WO2008042903A2 - Systems for sensing pressure/shear force - Google Patents

Systems for sensing pressure/shear force Download PDF

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Publication number
WO2008042903A2
WO2008042903A2 PCT/US2007/080197 US2007080197W WO2008042903A2 WO 2008042903 A2 WO2008042903 A2 WO 2008042903A2 US 2007080197 W US2007080197 W US 2007080197W WO 2008042903 A2 WO2008042903 A2 WO 2008042903A2
Authority
WO
WIPO (PCT)
Prior art keywords
diaphragm
sensor
polishing
cover
planarization
Prior art date
Application number
PCT/US2007/080197
Other languages
French (fr)
Other versions
WO2008042903A3 (en
Inventor
Wayne G. Renken
Mei H. Sun
Aron Abramowksi Mason
Lynn Karl Wiese
Original Assignee
Kla-Tencor Technologies Corporation
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Priority claimed from US11/861,207 external-priority patent/US7497134B2/en
Priority claimed from US11/861,119 external-priority patent/US7698952B2/en
Application filed by Kla-Tencor Technologies Corporation filed Critical Kla-Tencor Technologies Corporation
Priority to JP2009531559A priority Critical patent/JP2010506407A/en
Publication of WO2008042903A2 publication Critical patent/WO2008042903A2/en
Publication of WO2008042903A3 publication Critical patent/WO2008042903A3/en

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G01L5/0047Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes measuring forces due to residual stresses
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24BMACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B37/00Lapping machines or devices; Accessories
    • B24B37/04Lapping machines or devices; Accessories designed for working plane surfaces
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B24GRINDING; POLISHING
    • B24BMACHINES, DEVICES, OR PROCESSES FOR GRINDING OR POLISHING; DRESSING OR CONDITIONING OF ABRADING SURFACES; FEEDING OF GRINDING, POLISHING, OR LAPPING AGENTS
    • B24B49/00Measuring or gauging equipment for controlling the feed movement of the grinding tool or work; Arrangements of indicating or measuring equipment, e.g. for indicating the start of the grinding operation
    • B24B49/16Measuring or gauging equipment for controlling the feed movement of the grinding tool or work; Arrangements of indicating or measuring equipment, e.g. for indicating the start of the grinding operation taking regard of the load
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L1/00Measuring force or stress, in general
    • G01L1/14Measuring force or stress, in general by measuring variations in capacitance or inductance of electrical elements, e.g. by measuring variations of frequency of electrical oscillators
    • G01L1/142Measuring force or stress, in general by measuring variations in capacitance or inductance of electrical elements, e.g. by measuring variations of frequency of electrical oscillators using capacitors
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L5/00Apparatus for, or methods of, measuring force, work, mechanical power, or torque, specially adapted for specific purposes
    • G01L5/0061Force sensors associated with industrial machines or actuators
    • G01L5/0076Force sensors associated with manufacturing machines
    • G01L5/008Force sensors integrated in an article or a dummy workpiece
    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01LSEMICONDUCTOR DEVICES NOT COVERED BY CLASS H10
    • H01L21/00Processes or apparatus adapted for the manufacture or treatment of semiconductor or solid state devices or of parts thereof
    • H01L21/67Apparatus specially adapted for handling semiconductor or electric solid state devices during manufacture or treatment thereof; Apparatus specially adapted for handling wafers during manufacture or treatment of semiconductor or electric solid state devices or components ; Apparatus not specifically provided for elsewhere
    • H01L21/67005Apparatus not specifically provided for elsewhere
    • H01L21/67242Apparatus for monitoring, sorting or marking
    • H01L21/67253Process monitoring, e.g. flow or thickness monitoring

Definitions

  • CMP Chemical Mechanical Polishing
  • CMP generally leaves a planar surface, so that it is particularly suitable for applications where an uneven topology might cause problems, for example where additional layers are to be deposited over a surface formed by previous processing.
  • CMP allows successive layers to be formed while maintaining a reasonably flat surface for each successive layer.
  • CMP generally involves removing material from a wafer by a combination of physical abrasion and chemical action.
  • Figure 1 shows a cross-section of a wafer 101 that is undergoing a CMP process.
  • the wafer 101 is pressed down into a pad 103 by pressure applied to its upper surface. Pressure may be applied by a plate or pad.
  • pressure is applied to the upper surface of the wafer 101 by hydraulic or pneumatic systems. In this way the pressure may be controlled.
  • different pressure is provided at different locations on the upper surface of the wafer.
  • P E is provided near the edge, while Pc is provided at the center. Different pressures may be provided for a series of concentric zones with separate hydraulic, pneumatic or other systems to separately control pressure.
  • Some relative movement is created between the wafer 101 and the pad 103 by moving one or both of these components.
  • a retaining ring 105 keeps the wafer 101 in position with respect to structures providing pressure Pc and P E to the upper side of the wafer 101.
  • a slurry 107 extends over the pad 103, including the area under the wafer 101. Slurry 107 may be introduced through holes in pad 103. This slurry 107 contains abrasive particles as well as chemical components that may react with material on the wafer.
  • the pad 103 is generally formed of a soft material that deforms under the pressure exerted by a wafer. In general, CMP systems operate so that material is removed from the lower surface of the wafer.
  • a wafer is generally turned so that the side of the wafer to be processed (generally, the side that contains semiconductor devices and connections) is facing downwards.
  • the CMP head that is used to apply pressure may also need to be tuned in a tuning process, so that the pressures that are applied to the substrates of the type mentioned above are the desired pressures. Certain embodiments of the device proposed herein are also useful for the tuning process.
  • a member comprises a diaphragm to which pressure is applied, causing the diaphragm to deflect. At least one pair of capacitively coupled electrodes is used to sense the deflection of the diaphragm, wherein a capacitance of the at least one pair varies as a function of deflection of the diaphragm.
  • the member has a property that is substantially the same as that of the substrate.
  • a member is used, which member is suitable for undergoing a CMP process to simulate behavior of said substrate in the process.
  • At least one sensor is attached to the member.
  • the at least one sensor measures a parameter related to a shear force on a surface of the member when such surface is in contact with and pressed against a CMP surface and a lateral force is applied between the polishing or planarization surface and the surface of the member.
  • the surface of the member in contact with the CMP surface has a property that is substantially the same as a property of the surface of the substrate that the member simulates.
  • Figure 1 is a view of a cross-section of a semiconductor wafer undergoing a CMP process useful for illustrating the invention.
  • Figure 2 shows an example of a device or member such as one in the shape of a plate having a cavity that is covered by a diaphragm for measuring pressure or force to illustrate one embodiment of the invention.
  • FIGS 3A-3D are cross sectional views of capacitive pressure sensors that include a plate for measuring pressure or force to illustrate different embodiments of the invention.
  • a cavity is formed in a base or cover portion of the plate or a separation layer between the base and the cover.
  • Figure 4A shows a plan view of a base formed from a bare Silicon wafer.
  • Figure 4B shows a plan view of a cover formed from a thinned bare
  • Silicon wafer The cover is designed to be attached to the base of Figure 4A to form an instrumented wafer that includes a number of capacitive pressure sensors for measuring pressure or force to illustrate one embodiment of the invention.
  • Figure 5 A shows a plan view of a base of a device according to another embodiment of the invention.
  • Figure 5B shows a plan view of a cover designed to be attached to the base of Figure 5 A to form an instrumented wafer.
  • Figure 6 A shows a first example of a wafer for measuring pressure or force having sensor cavities with reservoirs illustrate one embodiment of the invention.
  • Figure 6B shows an alternative configuration to that of Figure 6 A.
  • Figure 7 shows an example of a device with a reservoir system that has an opening 706 to the exterior of the device and a valve controlling the opening to illustrate one embodiment of the invention.
  • Figure 8 A shows an example of a device that includes a flex circuit for measuring pressure or force.
  • Figure 8B is a side view of a plate with a base and a cover enclosing a cavity housing a pair of capacitively coupled electrodes not connected to the cover to sense a parasitic capacitance in the plate to illustrate another embodiment of the invention.
  • Figure 8C is a top plan view of two pairs of capacitively coupled electrodes adjacent to one another, one pair not connected to the cover to sense a parasitic capacitance in the plate, and the other pair connected to the cover to sense a deflection of the cover.
  • Figure 9 shows a device that includes a flex circuit and a plate having a cavity that is covered by a diaphragm for measuring pressure or force, where the circuit is at least partially located in the cavity to illustrate another embodiment of the invention.
  • Figure 10 shows another embodiment where a capacitive sensor is formed integrally with a flex circuit.
  • Figure 11 shows an example where a sensor cavity is formed within a base. Spacers are placed under a strain gauge so that the strain gauge can deflect downwards. A deflection augmenting element is placed between the upper surface of the strain gauge and the cover.
  • Figure 12A shows an alternative arrangement where a strain gauge is bonded to a cover so that the strain gauge deflects along with the cover.
  • Figure 12B shows an alternative embodiment to that of Figure 12 A.
  • Figure 13 shows an embodiment where pressure sensors are placed between a wafer and a CMP head.
  • Figure 14 shows a pressure calibration apparatus that may be used to calibrate a pressure sensing device.
  • Figure 15 shows a CMP head and an attached wafer moving with respect to a pad.
  • Figure 16A shows a first rigid body in contact with a surface and connected to a second rigid body by a portion of elastomeric material, where the .
  • Figure 16A first rigid body at rest with respect to the surface.
  • Figure 16B shows the first rigid body of Figure 16A in motion with respect to the surface and is moved by applying a force through the second rigid body.
  • a frictional force F is created, acting as a shear force causing portion of elastomeric material to deform.
  • Figure 17A shows a shear force sensor measuring deformation due to shear force on an elastomeric material through changes in the electrical properties of the elastomeric material as it is deformed.
  • Figure 17B shows an alternative shear force sensor where resistance is measured between two electrodes connected by a structure that varies in resistance as a result of shear induced deformation.
  • the structure is arranged so that it elongates and deforms under shear force. The resistance of the structure changes as a result of such elongation.
  • FIG. 18 Shown in Figure 18 is an alternative shear force sensor, where frictional force may be measured by allowing relative movement between two rigid bodies.
  • Figure 19A shows an example of a device where a base and a cover are separated by an elastomeric layer that deforms as the cover moves across a surface. In this case, a measurement is obtained for the entire device indicating the total frictional force experienced.
  • Figure 19B shows a plan view of a device having a lower surface consisting of concentric rigid bodies that are separated from a base by an elastomeric material.
  • the rigid bodies are physically separated from each other by small gaps so that they can move separately with respect to a base. Electrodes attached to the elastomeric material connecting the rigid bodies may be used to obtain separate resistance measurements to indicate the amount of frictional force experienced by different rigid bodies.
  • Figure 20 illustrates how a wafer may move with respect to a pad in one embodiment.
  • the pad is preferably a circular pad that rotates clockwise. The wafer rotates counter-clockwise and is moved laterally across the pad.
  • Figure 21 A shows a device that measures shear force at different radial and angular locations across a surface.
  • Figure 21 A shows the bottom (cover) side of a device similar to that of Figure 19B but with separate rigid bodies (separate shear force sensors) for different angular zones.
  • Figure 2 IB shows an alternative device for measuring shear force at different locations on a surface. Cut-outs are formed in a cover for shear force sensors with room to allow some displacement.
  • PCMDs Process Condition Measuring Devices
  • Instrumented wafers that have physical dimensions the same, or close to, those of a production wafer and that include sensors and electronics to measure at least one process condition.
  • Various PCMDs are described in US Patent Application Nos. 10/718,269, 10/837,359 and 11/381,992.
  • PCMDs may be wired or wireless.
  • a wired PCMD sends data to an external unit over wires (or optical fibers).
  • a wireless PCMD either stores data in a memory in the PCMD or may transmit the data to an external unit.
  • wireless PCMDs are more suitable for studying processes where a wafer is rotated such as CMP.
  • FIG. 2 shows an example of a wafer 211 having a cavity 213 that is covered by a diaphragm 215. Under pressure, the diaphragm 215 deflects by an amount ⁇ that depends on the external pressure. In general, ⁇ may be used as an indicator of pressure applied to the lower surface of the wafer 211.
  • a suitable sensor is used to sense deflection, and electronics are provided in the wafer 211 to store sensor data or transmit sensor data (or store and later transmit data)
  • such a PCMD may provide actual pressure data during a process such as CMP. Pressure on the lower surface of a substrate during CMP is generally less than five pounds per square inch (5psi), in addition to atmospheric pressure. In some cases, pressures may be up to 15psi, or even greater.
  • Various methods may be used to measure the deflection of a diaphragm such as diaphragm 215 of Figure 2.
  • One convenient method is to form a first capacitor electrode on the diaphragm, another electrode capacitively coupled to the first capacitor electrode fixed within the cavity and measure any change in capacitance.
  • a second convenient method is to use a strain gauge.
  • the deflection in a diaphragm used in this application should be small so that the surface being eroded behaves similarly to that of a production wafer that does not contain cavities and does not deflect in this way.
  • such a deflection is maintained at less than 10 microns, though in some cases deflections may exceed 10 microns. This may be achieved by choosing appropriate dimensions and material of the appropriate flexibility for the diaphragm and wafer of Figure 2.
  • FIGS 3A-3D show different embodiments where capacitance is used to measure deflection.
  • These capacitive pressure sensors use a cavity formed in a laminated wafer.
  • a laminated wafer or other sturcture is formed to include a base and a cover, the base generally being thicker than the cover.
  • the cover, or a portion of the cover, is sufficiently thin so that it deflects under pressure.
  • the base is generally formed by thinning a Silicon wafer and the cover is generally formed by thinning a Silicon wafer that has been processed up to a point where it is to be subjected to CMP processing. In this way, the lower surface of the cover closely resembles the lower surface of a production wafer including the same materials and topology.
  • the base and cover are attached to form a single unit.
  • the thickness of the unit (PCMD) formed is such that the pressures at the lower surface of the unit are close to those of a production wafer. This may require a thickness that is close to the thickness of a production wafer because a thicker PCMD would generally be stiffer and thus distribute pressure differently.
  • these capacitive pressure sensors simulate a real work piece or substrate that is undergoing a CMP process or a substrate to which a CMP head is to be applied (where the CMP head needs to be tuned).
  • the laminated wafer or structure it is preferable for the laminated wafer or structure to have properties (such as one or more of the following: dimensions, hardness, area and flexibility) that are substantially the same as those of a real substrate, such as a semiconductor wafer or flat panel display panel.
  • Figure 3A shows a cross section of a first capacitive pressure sensor where a cavity 321 is formed in a separation layer 323 that extends between a base 325 and a cover 327.
  • the separation layer 323 may be formed of a material such as Kapton® polyimide film that may be have cut-outs formed according to a predetermined pattern.
  • An electrical insulator 329a is formed on the cover 327 and a capacitor electrode 331a is formed on the insulator 329a. In one example, the insulator is between 5 microns and 50 microns thick.
  • the electrode 331a may be formed by attaching a metal foil or by depositing a metal layer.
  • An insulator 329b and electrode 331b are similarly formed on the base 325.
  • the base 325, cover 327 and separation layer 323 are aligned during assembly so that the electrodes 331a, 331b are in cavity 321.
  • no special topology is formed in opposing surfaces of either the base 325 or the cover 327. These surfaces of the base 325 and the cover 327 may be planar.
  • Figure 3B shows an alternative embodiment where a cavity 333 is formed into a base 335.
  • the cavity 333 may be machined, etched or otherwise formed in the base 335.
  • An insulator 337a is then formed in the cavity 333 and an electrode 339a is formed on the insulator 337a as before.
  • An electrode 339b and insulator 337b are similarly formed on the cover 341.
  • Figure 3C shows an alternative embodiment where a cavity 343 is formed into a cover 345. Insulators 347a, 347b and electrodes 349a, 349b are formed as before.
  • the cover 345 may be relatively thick in this example because it is reduced to a suitable thickness where cavities are formed.
  • the examples of Figures 3A-3D show three locations for the cavity: in a separation layer, in a base, and in a cover. A cavity may also be formed in a combination of these components, for example partially in the base and partially in the cover, or partially in a separation layer and partially elsewhere, either in the base or in the cover or in both.
  • a capacitive sensor includes a cavity having a diameter of 10 millimeters and an electrode of between 3 and 10 millimeters diameter, with a spacing between electrodes of 25-50 microns.
  • the diaphragm may have a thickness between 125 microns and 800 microns.
  • the insulators in this example have a thickness of 25 microns and the electrodes have a thickness of less than 25 microns. In other examples, different dimensions may be used.
  • Such a capacitive sensor may be able to resolve pressure to an accuracy of 0.01 pounds per square inch.
  • FIG. 3D shows another embodiment where instead of forming local insulators to isolate capacitor electrodes from the underlying surface, blanket insulating layers 351a, 351b are formed on both a base 353 and on a cover 355 respectively.
  • a blanket layer extends over all exposed surfaces on at least one side of a wafer.
  • the blanket layer is formed in such a way that the wafer is not warped and thus retains a substantially planar surface.
  • Such an insulating layer may be formed by deposition or may be grown, such as by growing a Silicon Dioxide layer on a Silicon surface. Where a cavity is formed in either the cover or the base, the insulating layer may be formed after the cavity is formed so that the insulating layer extends across surfaces of the cavity.
  • a blanket insulating layer may be used as an alternative to individual insulators in any of the above examples.
  • the base and cover may be electrically isolated from each other in some cases or may be electrically connected as described in US Patent Application No. 11/381,992.
  • the base and cover may be formed of either doped or undoped material and so may have different electrical conductivities according to requirements. Where the base and cover are undoped or have little doping so that the resistivity of the base and cover material is high, it may be possible to place electrodes directly on the surface of the base or cover (without an insulator or insulating layer). Where either the base or the cover is conductive, a parasitic capacitor may be formed between the conductive base (or cover) and an electrode that is separated from it by an insulator. In order to reduce the effects of such a parasitic capacitor, dimensions may be chosen so that the capacitive sensor has a greater capacitance than the parasitic capacitor.
  • Figure 4 A shows a plan view of a base 459 formed from a bare Silicon wafer.
  • the base contains a number of cavities, including cavity 461. Within these cavities insulators, such as insulator 463, are formed. Capacitive sensor electrodes, such as electrode 465, are formed on the insulators.
  • the base 459 of Figure 4A corresponds to the base 335 shown in Figure 3B.
  • Figure 4A also shows interconnects (pads), including interconnect 467 that form connections between the top capacitive sensor electrodes and the electronics in the base. Both electrodes are connected to electronic circuits (not shown) in the base to allow the capacitance to be measured.
  • the cavities and electrodes of this example are circular in shape, in other examples square, rectangular or other shaped cavities and electrodes may be used.
  • the shapes of the electrode or electrodes are not necessarily the same as the shapes of the cavities in which they are located.
  • Figure 4A shows sensor cavities extending along a diameter of the base. It may generally be assumed that the pressure distribution in a CMP process is radially symmetric (having the same pressure at all points along a given radius). However, in some cases sensor cavities may be distributed in a different manner so that pressures at are obtained at different angular locations.
  • Figure 4B shows a plan view of a cover 469 formed from a thinned bare Silicon wafer.
  • Cover 469 is designed to be attached to the base 459 of Figure 4A to form an instrumented wafer that includes a number of capacitive pressure sensors.
  • Insulators such as insulator 471 are formed on the cover 469 and capacitive sensor electrodes, such as electrode 473, are formed on the insulators.
  • interconnects to the base including interconnect 475. These interconnects are aligned with interconnects on the base to form an electrical connection between electrodes and the electronics.
  • Figure 5 A shows a plan view of a base 577 of a PCMD according to another embodiment.
  • no separate insulators are provided on the base 577 because the base 577 is formed from a Silicon wafer with an insulating layer (as shown in Figure 3D).
  • Capacitive sensor electrodes, including electrode 579, are placed directly on the insulating layer. Cavities, such as cavity 581, may either be formed in the base 577 or may be formed in a spacer layer that has holes located between electrodes of the base and cover.
  • some electronic circuits (not shown) are also located in or on such a base and such electronic circuits are connected to the electrodes on the base and the electrodes on the cover.
  • Figure 5B shows a plan view of a cover 583 designed to be attached to the base 577 of Figure 5A to form a PCMD (instrumented wafer).
  • Cover 583 has an insulating layer formed of Silicon dioxide or other suitable dielectric material and so does not require separate insulators under individual electrodes. Electrodes, such as electrode 585, are formed (by deposition or otherwise) directly on the insulating layer.
  • Figure 5B also shows interconnects, including interconnect 587 that connect the electrode of the cover to electronics in the base 577.
  • a groove (or trench) 579 is provided to allow connection between the electrode 585 and the interconnect 587.
  • An electrical connection between the interconnect and the electrode may be formed by the same deposition step that forms the electrode 585 or may be formed separately. In one example, electrodes and interconnects are formed by silk screening or similar thick film techniques.
  • a cavity is formed for a pressure sensor
  • slurry used in CMP could cause damage to electrodes and other components if it entered such a cavity.
  • an isolated cavity may experience a significant increase in pressure as a diaphragm is deflected. Even though the change in the volume of the cavity is small, if the cavity itself is small, the change in volume and hence the change in pressure may be significant. Such a pressure change is generally undesirable because it may cause a non-linear relationship between deflection and the external pressure.
  • One way to reduce the pressure change caused by a diaphragm deflecting into a cavity is to provide an additional volume in communication with the cavity.
  • This additional volume reduces the effect of volume change caused by diaphragm deflection on pressure in the sensor cavity.
  • the additional volume may be considered a reservoir.
  • Such a reservoir is generally formed so that its volume does not change as a result of external pressure. For example, support may be provided to ensure that significant deflection does not occur in a reservoir.
  • Figure 6A shows a first example of a wafer 689 having sensor cavities with reservoirs.
  • sensor cavity 691 connects with reservoir 693.
  • a reservoir may be formed as a cavity in the base (or cover, or separation layer, or a combination of these components) in the same manner as the cavity for the sensor.
  • a channel 695 connects the reservoir 693 to the sensor cavity 691.
  • supporting structures 697 extend across a reservoir to limit any deflection that might occur in the cover over this area.
  • Each sensor cavity of Figure 6A has a dedicated reservoir. In some cases, a reservoir may be deeper than a sensor cavity so that its volume is greater for a given cross sectional area.
  • Figure 6B shows an alternative configuration to that of Figure 6A.
  • sensor cavities 699a-i share a reservoir system that interconnects cavities 699a-i and reservoirs 602a, 602b.
  • a reservoir system may be formed by the same process used to form sensor cavities 699a-i.
  • a pattern of sensor cavities, reservoirs and interconnecting channels may be formed in the base (and/or other components) as shown.
  • the reservoir system is isolated from the exterior of the PCMD so that no foreign matter can enter the reservoir system and the pressure in the reservoir system remains stable.
  • the reservoir system may be desirable to have an opening from a reservoir system in a PCMD to the exterior of the wafer. For example, it may be desirable to equalize the pressure in the reservoir system with the ambient pressure. In some cases, equalization may be used to eliminate a pressure differential that might be caused by different atmospheric pressure resulting from use at different altitudes or in different weather conditions. It may also be desirable to bring the reservoir system to a predetermined condition before use. For example, the reservoir system may be brought to a desired pressure, either above atmospheric pressure or below atmospheric pressure (under vacuum). The reservoir system may also be filled with a particular gas or mixture of gases if desired.
  • FIG. 7 shows an example of a PCMD 704 with a reservoir system that has an opening 706 to the exterior of PCMD 704.
  • a valve is provided to selectively connect the opening 706 to the reservoir system.
  • MEMS Microelectromechanical Systems
  • a MEMS valve 708 may be formed in the base, or may be formed separately and attached to the base. The MEMS valve may be controlled by electronic circuits in PCMD 704. When PCMD 704 is in use, the MEMS valve will generally remain closed to prevent foreign matter entering the reservoir system.
  • the MEMS valve 708 may be opened by an electronic circuit in PCMD 704, generally in response to a signal provided from outside PCMD 704. This may occur during a calibration or initialization procedure.
  • An alternative to a MEMS valve is to provide a temporary blockage that covers the opening 706.
  • a suitable material for example a polymer such as Silicone, may be used to block the opening. The blockage formed may be removed to configure the reservoir system.
  • electronic circuits are provided in a PCMD to store data from the sensors. Circuits may alternatively transmit data to a receiver outside the PCMD. In some cases, data is first stored and then transmitted. Such circuits may be formed and connected in a number of ways.
  • electronic circuits include one or more integrated circuits that are placed in cavities in a base (or cover). The integrated circuits are bonded in place. Electrical connections between integrated circuits and sensors are provided by conductive traces formed on the surface of the base (or cover). Connection pads on the integrated circuits may be bonded to these traces. Integrated circuits used in this configuration may be used in the form of semiconductor dies so that they have small profiles and small thermal capacities.
  • insulated wires may extend between components including sensors and integrated circuits. Such wires may be bonded to the components and may run through trenches formed within a PCMD.
  • electronic circuits and connections between circuits are formed as a flex circuit assembly that is attached to a base. Generally, cavities and grooves are formed in the base so that such a flex circuit presents a surface that is flush with the surface of the base. A cover may then be attached. Descriptions of the use of such flex circuits and traces in PCMDs are provided in US Patent Application Nos. 10/837,359 and 11/381,992.
  • FIG. 8 A An example of a PCMD 810 that includes a flex circuit 812 is provided in Figure 8 A.
  • the flex circuit 812 includes at least one microprocessor 814 that is in communication with the sensors.
  • Microprocessor 814 may include a memory for storing data from the sensors, and/or transmitter circuits for transmitting such data to an external device, preferably by wireless transmission, such as radio waves.
  • the flex circuit 812 provides power connections between the battery 816, or batteries, and other components.
  • Figure 8A shows temperature sensors Tl, T2 and T3. Sensors Tl, T2, T3 are located close to capacitive pressure sensors 818a-c so that an individual temperature sensor may provide temperature for a specific capacitive sensor.
  • a temperature sensor is provided for each pressure sensor 818a-i. In this way, the temperature for a particular capacitive sensor may be used to compensate for any temperature variation that might affect the physical or electrical behavior of the capacitive sensor.
  • Temperature sensors Tl, T2, T3 may be formed as part of the flex circuit 812 or may be separately formed and attached to the flex circuit 812.
  • Figure 8B is a side view of a member such as a plate with a base 824 and a cover 822 enclosing a cavity housing a pair 826 of capacitively coupled electrodes 826a and 826b not connected to the cover to sense a parasitic capacitance in the plate to illustrate another embodiment of the invention. Electrodes 826a and 826b are separated by a dielectric layer 828.
  • Figure 8C is a top plan view of two pairs 826 and 836 of capacitively coupled electrodes adjacent to one another, one pair (826) not connected to the cover to sense a parasitic capacitance in the plate, and the other pair (836) connected (not shown in Figure 8B) to the cover to sense a deflection of the cover.
  • the capacitance of pair 826 is an indication of the parasitic capacitance experienced by pair 836.
  • the capacitance of pair 826 may be used to adjust the measurement of the deflection of cover 822 by pair 836, so as to reduce the effect of the parasitic capacitance experienced by pair 836 on the measurement. This may be performed by microprocessor 814 in Figure 8 A, after the microprocessor 814 receives data related to the capacitances of pairs 826 and 836 through flex circuit 812 in Figure 8A, and the change in capacitance of pair 836 caused by deflection of the cover 822.
  • Electrodes are formed on the base and cover, these electrodes are connected to the flex circuit so that electronic circuits within the flex circuit can detect any capacitance change. Similarly, temperature or other sensors that are not formed integrally with the flex circuit are connected to the flex circuit.
  • Figure 9 shows an example where an electrode 920 on a cover 922 is connected to a pad 924 on a flex circuit 926.
  • the electrode 920 is connected to an interconnect 928 that is outside the sensor cavity 930 (as shown in Figure 5B).
  • the interconnect 928 is isolated from the cover 922 by an insulating layer 932A on the cover 922.
  • Pad 924 on the flex circuit 926 overlies the interconnect 928 and this pad is electrically connected to one or more integrated circuits in the flex circuit 926.
  • the interconnect 928 is attached to the pad 924 by an electrically conductive epoxy 934.
  • a similar connection (not shown) may be made to the base electrode 936. Similar connections may be formed for temperature sensors.
  • Flex circuit 926 lies in trench 938 in this example. Thus, the electronics is partially in the cavity (the electrodes 920 and 936), and partially (flex circuit 926) in the trench 938 which can serve also as a reservoir to reduce the effect of deflection of the cover on the pressure measurement.
  • FIG. 10 shows another embodiment where a capacitive sensor is formed integrally with a flex circuit 1042.
  • the flex circuit includes two electrodes 1044a, 1044b that are separated by a dielectric layer 1046 to form a capacitor 1040.
  • the dielectric layer 1046 may be formed of a suitably compressible elastomeric material.
  • the portion of the flex circuit 1042 that contains the capacitor is bonded to both the base 1048 and the cover 1050 using thin layers 1052a, 1052b of adhesive. Flex circuit 1042 lies in trench 1056.
  • trenches are provided for the flex circuits 926, 1042. Trenches 938, 1056 connect to the sensor cavities 930, 1054 respectively.
  • a flex circuit does not fully occupy the flex circuit trench so that some unoccupied volume remains around the flex circuit. This extra volume allows for some gas flow through the trenches formed for the flex circuit. Also, some unoccupied volume generally remains around some integrated circuits of the flex circuit.
  • the unoccupied volumes within the trenches and cavities formed for the flex circuit may form a reservoir system that reduces pressure variation within sensor cavities. A controlled opening from such a reservoir system to the exterior of the PCMD may be provided as previously described.
  • a flex circuit includes one or more capacitive sensors, or is attached to one or more capacitive sensors, and also includes electrical connections from the one or more sensors to an integrated circuit that provides an output that is dependent on the capacitance of the capacitive sensor.
  • An example of an integrated circuit that may be used is an Analog Devices AD7746 capacitance to digital converter. This integrated circuit provides an output that may then be sent to a microprocessor for storage or transmission.
  • capacitors connect directly to a microprocessor that performs a capacitance to digital conversion internally.
  • a sensor cavity may be formed according to any of the examples described above so that a diaphragm is formed that will deflect under pressure. Instead of placing capacitor electrodes on either side of this cavity, a strain gauge is placed so that it will be deflected as the diaphragm is deflected.
  • Figure 11 shows a first example where a sensor cavity 1158 is formed within a base 1160 (note that this drawing shows the cover 1162 above the base 1160, the opposite orientation to that of previous drawings and the opposite to the orientation during CMP).
  • Spacers 1164a, 1164b are placed under a strain gauge 1166 so that the strain gauge 1166 can deflect downwards.
  • a deflection augmenting element 1168 (such as a small bead, tube, corrugated structure or some other small rigid body) is placed between the upper surface of the strain gauge 1166 and the cover 1162. Thus, any deflection in the cover 1162 will cause the strain gauge 1166 to deflect.
  • the deflection augmenting element 1168 causes a greater deflection in strain gauge 1166 than the deflection in cover 1162, thus augmenting the measurement obtained, which may increase resolution.
  • a deflection augmenting element is machined into either a cover or a base.
  • the strain gauge 1166 may be connected to electronic circuits in the base 1160 as previously described.
  • Figure 12A shows an alternative arrangement where a strain gauge
  • a suitable strain gauge may be a resistive strain gauge, a piezoresistive strain gauge, a piezoelectric strain gauge or a semiconductor strain gauge such as a bar gauge.
  • Figure 12B shows an alternative embodiment to that of Figure 12 A.
  • a cavity 1276 is formed in cover 1278 and a strain gauge 1280 is formed on cover 1278.
  • Base 1282 may be planar in this example.
  • FIG. 13 shows an embodiment where pressure sensors 1384a-d are placed between a wafer 1386 and a CMP head 1388.
  • a production wafer may be used for wafer 1386 or a PCMD may be used instead.
  • Pressure sensors may be capacitive sensors formed from two metal electrodes separated by a compressible dielectric.
  • sensors 1384a-d are attached to wafer 1386.
  • sensors 1384a-d are attached to the CMP head. In either case, sensors 1384a-d measure the pressure between the CMP head 1388 and wafer 1386 at various points on the wafer surface.
  • Sensors 1384a-d are connected to electronics module 1388, which is mounted to CMP head 1388.
  • Electronics module 1389 may store data from sensors 1384a-d, or may transmit the data in real time to another unit.
  • electronics module 1389 may include a Bluetooth or other wireless communication device to allow real time transmission of data.
  • a pressure measurement wafer (PCMD), either initially as part of a factory calibration or in the field.
  • the pressure readings from pressure sensors may change with use.
  • a PCMD is subject to CMP
  • the thickness of a diaphragm is reduced, thus affecting pressure measurements based on the deflection of the diaphragm.
  • a hard layer for example, Silicon Nitride
  • Such hard layer may have different characteristics to materials of production wafers.
  • Another option is to deposit additional material periodically to replace material removed by CMP. This may be done at relatively low temperatures for some materials (e.g. Copper) but may require high temperatures for other materials (e.g. Silicon).
  • Figure 14 shows a pressure calibration apparatus that may be used to calibrate a pressure sensing PCMD as previously described.
  • a PCMD 1490 is placed on a first surface 1492 with pressure sensors facing up.
  • a second surface 1494 is located at a fixed distance above first surface 1492 and an inflatable bladder 1496 is placed between the PCMD 1490 and second surface 1494.
  • Inflatable bladder 1496 is inflated to a predetermined pressure (or to a series of predetermined pressures) through pressure regulator 1498.
  • Sensor readings may be recorded for each sensor at each predetermined pressure applied, and this data may be used to calibrate the sensor readings.
  • a PCMD may be periodically calibrated in this manner to correct for removed material or other effects.
  • the pressure sensors are heated or cooled to predetermined temperatures by means of a temperature control instrument 1450.
  • a PCMD according to certain examples described above is used by placing it, with the cover side down, in a CMP processing system.
  • the PCMD undergoes the same process that a production wafer goes through.
  • the PCMD measures pressure at different locations across the lower surface.
  • the data generated from such measurements is stored in a memory.
  • the data is downloaded and analyzed to provide information about pressure across the PCMD as a function of time. Temperature data may be separately recorded. Temperature data may also be used to compensate pressure sensor reading for any temperature effects.
  • Various examples refer to CMP applications for a pressure sensing wafer or PCMD.
  • a pressure sensing wafer may be used in various other processes including processes that take place at pressures greater or less than atmospheric pressure.
  • One example of a process that may be studied using a pressure sensing wafer is an immersion photolithography process, where pressure caused by an air knife (used to contain a water puddle) may be measured.
  • Another process is CMP scrubbing or cleaning, a process that cleans a wafer after CMP. The pressure applied to the wafer during such a clean process may affect the cleanliness of the wafer.
  • Certain processes hold a wafer to a chuck by electrostatic force.
  • the force that such an electrostatic chuck (ESC) applies may vary over time and may be adjusted to prevent wafers from moving during processing.
  • a pressure measuring PCMD may be used to measure the pressure between a wafer and such a chuck to determine the appropriate adjustment (if any).
  • Substrates other than Silicon wafers may be instrumented to form a PCMD. For example, GaAs wafers or Flat Panel Display (FPD) substrates may be similarly provided with cavity based sensors.
  • FPD Flat Panel Display
  • a PCMD has the same diameter as a 200 millimeter or 300 millimeter wafer and the same (or similar thickness).
  • the PCMD includes at least one cavity that has a sensor to detect deflection into the cavity caused by external pressure.
  • the PCMD may further include at least one temperature sensor.
  • the PCMD may also include a flex circuit with at least one integrated circuit and conductors between the integrated circuit and sensors.
  • the PCMD may also include at least one battery.
  • a sensor to detect deflection in a cavity may be capacitance based or strain gauge based.
  • a cavity may be connected to a dedicated reservoir or to a shared reservoir.
  • a reservoir may be provided with an external opening.
  • Frictional force F generally depends on the coefficient of friction and also the normal force (pressure) between wafer 1503 and pad 1505.
  • pressure is not always uniform across a wafer surface during CMP.
  • the velocity of relative motion between a wafer and a pad is not always constant across a wafer.
  • a wafer may be rotated, resulting in a higher velocity for outer portions of the wafer than for inner portions.
  • the pad may rotate or otherwise move in a manner that does not provide uniform velocity across a wafer surface. It may be useful to measure frictional force at different locations across a wafer surface during CMP in order to estimate mechanical abrasion.
  • Figures 16A and 16B illustrate the effect of shear force on a structure
  • FIG. 1609 that is designed to deform under shear stress.
  • Figure 16A shows a first rigid body 1611 in contact with a surface 1613. First rigid body 1611 is connected to second rigid body 1615 by a portion of elastomeric material 1617.
  • Figure 16A shows structure 1609 at rest with respect to surface 1613.
  • Figure 16B shows structure 1609 in motion, having velocity V, with respect to surface 1613. Structure 1609 is moved by applying a force through second rigid body 1615.
  • Frictional force F acts as a shear force causing portion of elastomeric material 1617 to deform.
  • elastomeric material 1617 may comprise a silicone elastomer with conductive elements dispersed therein, such as small flakes, platelets, fibers or nanotubes.
  • the deformation causes an offset of d between first rigid body 1611 and second rigid body 1615 compared with their unloaded positions.
  • the magnitude of d is a function of F.
  • a shear force sensor may be formed from two rigid bodies that have a limited range of relative displacement under shear force and have some mechanism for measuring displacement.
  • structure or member 1609 simulates a real work piece or substrate that is undergoing a CMP process.
  • the surface in contact with surface 163 it is preferable for its surface in contact with surface 163 to have a coefficient of friction that is substantially the same as that of a real substrate, such as a semiconductor wafer or flat panel display panel. It is preferable for the structure 1609 to have dimensions that are substantially the same as those of a real substrate.
  • the shear force is applied in a direction so that the force has at least one component that is perpendicular to the surfaces of structure 1609 and surface 1613.
  • a shear force sensor 1718 measures deformation due to shear force on an elastomeric material through changes in the electrical properties of the elastomeric material as it is deformed.
  • the electrical resistance of such an elastomeric material may change as the material is deformed.
  • Electrodes may be provided to detect changes in the resistance of such an elastomeric material.
  • Figure 17A shows an example where electrodes 1719a, 1719b are embedded in an elastomeric layer 1720 and an electrical resistance measuring unit 1721 measures an electrical resistance (also referred to herein as simply "resistance", the two terms used interchangeably herein) between them.
  • Some elastomeric materials may be formed with anisotropic electrical characteristics.
  • a suitable elastomeric material with anisotropic electrical characteristics may comprise a silicone elastomer with conductive elements dispersed therein, such as small flakes, platelets, fibers or nanotubes.
  • conductive elements dispersed therein, such as small flakes, platelets, fibers or nanotubes.
  • such materials may be electrically conductive in one direction and nonconductive in another direction.
  • Such materials may be formed so that a resistance changes with a deformation caused by shear (horizontal) force but is not significantly affected by a compressive (vertical) force.
  • Electrodes for resistance measurement may be formed in the elastomeric material or on one or both surfaces on either side, for example as patterns of interdigitated fingers.
  • Figure 17B shows an alternative shear force sensor 1799 where resistance is measured by an electrical resistance measuring unit (not shown), such as unit 1721 of Figure 17A, between electrodes 1797a, 1797b, which are connected by a structure 1795 that varies in resistance as a result of shear induced deformation.
  • structure 1795 is arranged so that it runs diagonally through elastomeric layer 1793.
  • structure 1795 elongates as elastomeric layer 1793 deforms under shear force.
  • the resistance of structure 1795 changes as a result of such elongation.
  • Structure 1795 may be formed of metallic platelets (e.g. Aluminum), carbon fibers, carbon black particles or similar small conductive bodies that form a conductive pathway. As the conductive pathway is stretched, conduction diminishes because of poor contact between conductive bodies. Structure 1795 is generally not sensitive to downward pressure.
  • factional force may be measured by allowing relative movement between two rigid bodies.
  • a lower rigid body 1823 includes a protrusion 1825 that extends into a cavity 1827 in an upper rigid body 1829.
  • the location of protrusion 1825 within cavity 1827 is established by springs or some other mechanism that allows some lateral movement when force is applied (e.g. elastomeric material).
  • a frictional force F is generated that tends to cause lower rigid body 1823 to move with respect to upper rigid body 1829.
  • Such a relative movement may be observed as a change in distances dl, d2 between protrusion 1825 and walls of cavity 1827.
  • Distances dl and d2 may be measured by any suitable technique including capacitively or using piezoelectric material.
  • Shear force may occur in any lateral direction, so a shear force sensor may detect displacement from a static condition in more than one direction.
  • shear force sensor 1822 may also measure distances perpendicular the cross section shown. Thus, both the magnitude and direction of shear force may be measured.
  • Figure 18 shows upper rigid body 1829 in contact with surface 1831. In other examples, such an upper rigid body may not have any contact with a surface and only the lower rigid body is in contact.
  • Upper rigid body 1829 may be a base of a PCMD that includes electronic components that receive data from shear force sensor 1822.
  • a PCMD may measure frictional force using the structures described above.
  • Figure 19A shows a first example of a PCMD 1936 where a base 1933 and a cover 1935 are separated by an elastomeric layer 1937 that deforms as cover 1935 moves across a surface. In this case, a measurement is obtained for the entire PCMD 1936 indicating the total frictional force experienced. However, in some cases, it is desirable to obtain values for frictional force at different points on a wafer, or PCMD.
  • Figure 19B shows a plan view of a PCMD 1938 having a lower surface consisting of concentric rigid bodies 1939a-d that are separated from a base (not shown) by an elastomeric material.
  • Rigid bodies 1939a-d are physically separated from each other by small gaps so that rigid bodies 1939a-d can move separately with respect to a base.
  • PCMD 1938 rotates, frictional force is different for different rigid bodies 1939a-d.
  • Electrodes attached to the elastomeric material connecting rigid bodies 1939a-d may be used to obtain separate resistance measurements to indicate the amount of frictional force experienced by different rigid bodies. In this way, instead of a single measurement of frictional force experienced by a PCMD, four different measurements are obtained, representing shear force experienced by four concentric zones of a wafer.
  • PCMD 1938 may be considered to have four concentric shear force sensors.
  • Figure 20 illustrates how a wafer 2041 may move with respect to a pad 2043.
  • Pad 2043 is a circular pad that rotates clockwise in this example by an instrument 2050, such as a motor in a conventional manner.
  • Wafer 2041 rotates counter-clockwise and is moved laterally across pad 2043 by an instrument 2052 such as a motor and a gear mechanism in a conventional manner, which instrument may be one and the same as instrument 2050.
  • an instrument 2052 such as a motor and a gear mechanism in a conventional manner, which instrument may be one and the same as instrument 2050.
  • the right side of wafer 2041 experiences a higher speed with respect to the underlying portion of pad 2043 than the left side of wafer 2041.
  • shear force for a particular location on the wafer surface may oscillate from low to high.
  • the shear force changes as wafer 2041 moves laterally across pad 2043.
  • additional information may be obtained, such as maximum and minimum shear forces and patterns in changing shear force.
  • Figure 21 A shows a PCMD 2147 that measures shear force at different radial and angular locations across a surface.
  • Figure 21 A shows the bottom (cover) side of a PCMD 2147 similar to PCMD 1938 but with separate rigid bodies (separate shear force sensors) for different angular zones.
  • PCMD 2147 instead of measuring average frictional force for different radial zones, PCMD 2147 measures frictional force for four different portions of each radial zone. This may provide maximum and minimum shear force information that may be useful.
  • Figure 2 IB shows an alternative PCMD 2149 for measuring shear force at different locations on a surface.
  • the shear force sensors on the lower surface of a PCMD occupied the entire lower surface (or nearly the entire lower surface), here shear force sensors 2151 a-i occupy only a portion of the lower surface of PCMD 2149. Cut-outs are formed in a cover for shear force sensors 2151 a-i with room to allow some displacement.
  • PCMDs 1936, 1938, 2047 and 2149 may measure shear force using a shear force sensor such as sensors 1718 or 1799 that use elastomeric material, or a shear force sensor such as sensor 1822 that uses displacement, or using any other suitable shear force sensor.
  • one or more shear force sensors may be combined with other sensors in a PCMD.
  • a microprocessor (not shown) similar to microprocessor 814 in Figure 8 A may be used to receive the data from the shear force sensors such as sensors 1718 and 1799, and data from other sensors through flex circuits of the type described above.
  • such microprocessor includes a memory for storing data from the sensors, and/or transmitter circuits for transmitting such data to an external device, preferably by wireless transmission, such as radio waves.
  • sensors may collect acoustic input that is used to characterize a CMP process. For example, as a surface is eroded, a frequency of wafer vibration may change. This change may be detected by one or more acoustic sensors in the wafer or in a CMP head and used to obtain information regarding the amount of material removed. Thus, certain acoustic sensors may be considered removal rate sensors.

Abstract

At least one pair of capacitively coupled electrodes contained in a structure is used to sense the deflection of a diaphragm in a pressure or force sensor for measuring the pressure or force exerted on the diaphragm. Preferably the structure has properties (such as one or more of the following: dimensions, hardness, area and flexibility) that are substantially the same as those of a real substrate, such as a semiconductor wafer or flat panel display panel. For measuring shear force, at least one shear force sensor is used to measure the shear force on a member, when the member is in contact with and pressed against a polishing or planarization surface and a lateral force is applied between the two surfaces. Preferably the structure and the surface of the structure have properties (such as one or more of the following: dimensions and coefficient of friction) that are substantially the same as those of a real substrate, such as a semiconductor wafer or flat panel display panel.

Description

SYSTEMS FOR SENSING PRESSURE/SHEAR FORCE
BACKGROUND OF THE INVENTION
[0001] Semiconductor processing involves multiple steps to produce working integrated circuits on a semiconductor wafer. These steps may include deposition and removal of various materials to form devices and to form the electrical connections between devices. One process that removes material from a wafer is Chemical Mechanical Polishing or Planarization (CMP). CMP generally leaves a planar surface, so that it is particularly suitable for applications where an uneven topology might cause problems, for example where additional layers are to be deposited over a surface formed by previous processing. In particular, where multiple layers of metal interconnection are required in complex integrated circuits, CMP allows successive layers to be formed while maintaining a reasonably flat surface for each successive layer.
[0002] CMP generally involves removing material from a wafer by a combination of physical abrasion and chemical action. Figure 1 shows a cross-section of a wafer 101 that is undergoing a CMP process. The wafer 101 is pressed down into a pad 103 by pressure applied to its upper surface. Pressure may be applied by a plate or pad. In some cases, pressure is applied to the upper surface of the wafer 101 by hydraulic or pneumatic systems. In this way the pressure may be controlled. In some cases, different pressure is provided at different locations on the upper surface of the wafer. Here PE is provided near the edge, while Pc is provided at the center. Different pressures may be provided for a series of concentric zones with separate hydraulic, pneumatic or other systems to separately control pressure. Some relative movement is created between the wafer 101 and the pad 103 by moving one or both of these components. As the wafer 101 moves with respect to the pad 103 its lower surface is eroded. A retaining ring 105 keeps the wafer 101 in position with respect to structures providing pressure Pc and PE to the upper side of the wafer 101. A slurry 107 extends over the pad 103, including the area under the wafer 101. Slurry 107 may be introduced through holes in pad 103. This slurry 107 contains abrasive particles as well as chemical components that may react with material on the wafer. The pad 103 is generally formed of a soft material that deforms under the pressure exerted by a wafer. In general, CMP systems operate so that material is removed from the lower surface of the wafer. Thus, a wafer is generally turned so that the side of the wafer to be processed (generally, the side that contains semiconductor devices and connections) is facing downwards.
[0003] In general it is desirable to remove material uniformly across the surface of a wafer. Various parameters may vary across the wafer surface causing nonuniform removal rates. One parameter that may vary across the wafer is the pressure between the pad and the wafer. For example, in Figure 1, pressure Pl may not be equal to pressure P2. It is generally desirable to know the values of pressure Pl and P2 in order to adjust the CMP process to obtain high uniformity. While the pressures Pl and P2 between the wafer 101 and the pad 103 are affected by the pressures Pc, PE applied to the top surface of the wafer 101, these relationships may not be simple so that measuring Pc and PE may not provide sufficient information for process tuning. Therefore, it is generally desirable to directly measure pressure at points across a wafer surface during processing. CMP processes may also be applied to substrates other than semiconductor wafers, such as flat panel display panels and magnetic heads or still other types of work pieces.
SUMMARY OF THE INVENTION
[0004] Before or periodically during the CMP process, the CMP head that is used to apply pressure may also need to be tuned in a tuning process, so that the pressures that are applied to the substrates of the type mentioned above are the desired pressures. Certain embodiments of the device proposed herein are also useful for the tuning process.
[0005] In one embodiment, a member comprises a diaphragm to which pressure is applied, causing the diaphragm to deflect. At least one pair of capacitively coupled electrodes is used to sense the deflection of the diaphragm, wherein a capacitance of the at least one pair varies as a function of deflection of the diaphragm. Thus, by sensing the capacitance of the pair, it is possible to provide an indication of the deflection of the diaphragm, which in turn provides an indication of the pressure on the diaphragm. Preferably, the member has a property that is substantially the same as that of the substrate.
[0006] In general, removal of material in CMP is caused by two mechanisms: mechanical action and chemical action. Although these mechanisms are closely linked, it may be desirable to try to separately measure parameters associated with each. One measurement that may be of particular value in measuring mechanical action is the frictional force between a wafer and a pad as the wafer moves with respect to the pad. Generally, mechanical abrasion of material increases with increasing frictional force. Frictional force may be used to provide a shear force in a structure that deforms in a manner that indicates the magnitude of the shear force. In general, greater frictional force provides greater mechanical action in removing material during CMP.
[0007] In another embodiment, a member is used, which member is suitable for undergoing a CMP process to simulate behavior of said substrate in the process. At least one sensor is attached to the member. The at least one sensor measures a parameter related to a shear force on a surface of the member when such surface is in contact with and pressed against a CMP surface and a lateral force is applied between the polishing or planarization surface and the surface of the member. Preferably, the surface of the member in contact with the CMP surface has a property that is substantially the same as a property of the surface of the substrate that the member simulates.
BRIEF DESCRIPTION OF THE DRAWINGS
[0008] Figure 1 is a view of a cross-section of a semiconductor wafer undergoing a CMP process useful for illustrating the invention.
[0009] Figure 2 shows an example of a device or member such as one in the shape of a plate having a cavity that is covered by a diaphragm for measuring pressure or force to illustrate one embodiment of the invention.
[0010] Figures 3A-3D are cross sectional views of capacitive pressure sensors that include a plate for measuring pressure or force to illustrate different embodiments of the invention. A cavity is formed in a base or cover portion of the plate or a separation layer between the base and the cover.
[0011] Figure 4A shows a plan view of a base formed from a bare Silicon wafer.
[0012] Figure 4B shows a plan view of a cover formed from a thinned bare
Silicon wafer. The cover is designed to be attached to the base of Figure 4A to form an instrumented wafer that includes a number of capacitive pressure sensors for measuring pressure or force to illustrate one embodiment of the invention.
[0013] Figure 5 A shows a plan view of a base of a device according to another embodiment of the invention.
[0014] Figure 5B shows a plan view of a cover designed to be attached to the base of Figure 5 A to form an instrumented wafer.
[0015] Figure 6 A shows a first example of a wafer for measuring pressure or force having sensor cavities with reservoirs illustrate one embodiment of the invention.
[0016] Figure 6B shows an alternative configuration to that of Figure 6 A.
[0017] Figure 7 shows an example of a device with a reservoir system that has an opening 706 to the exterior of the device and a valve controlling the opening to illustrate one embodiment of the invention.
[0018] Figure 8 A shows an example of a device that includes a flex circuit for measuring pressure or force.
[0019] Figure 8B is a side view of a plate with a base and a cover enclosing a cavity housing a pair of capacitively coupled electrodes not connected to the cover to sense a parasitic capacitance in the plate to illustrate another embodiment of the invention. [0020] Figure 8C is a top plan view of two pairs of capacitively coupled electrodes adjacent to one another, one pair not connected to the cover to sense a parasitic capacitance in the plate, and the other pair connected to the cover to sense a deflection of the cover.
[0021] Figure 9 shows a device that includes a flex circuit and a plate having a cavity that is covered by a diaphragm for measuring pressure or force, where the circuit is at least partially located in the cavity to illustrate another embodiment of the invention.
[0022] Figure 10 shows another embodiment where a capacitive sensor is formed integrally with a flex circuit.
[0023] Figure 11 shows an example where a sensor cavity is formed within a base. Spacers are placed under a strain gauge so that the strain gauge can deflect downwards. A deflection augmenting element is placed between the upper surface of the strain gauge and the cover.
[0024] Figure 12A shows an alternative arrangement where a strain gauge is bonded to a cover so that the strain gauge deflects along with the cover.
[0025] Figure 12B shows an alternative embodiment to that of Figure 12 A.
[0026] Figure 13 shows an embodiment where pressure sensors are placed between a wafer and a CMP head.
[0027] Figure 14 shows a pressure calibration apparatus that may be used to calibrate a pressure sensing device.
[0028] Figure 15 shows a CMP head and an attached wafer moving with respect to a pad.
[0029] Figure 16A shows a first rigid body in contact with a surface and connected to a second rigid body by a portion of elastomeric material, where the . Figure 16A first rigid body at rest with respect to the surface. [0030] Figure 16B shows the first rigid body of Figure 16A in motion with respect to the surface and is moved by applying a force through the second rigid body. As a result of relative motion between first rigid body and the surface, a frictional force F is created, acting as a shear force causing portion of elastomeric material to deform.
[0031] Figure 17A shows a shear force sensor measuring deformation due to shear force on an elastomeric material through changes in the electrical properties of the elastomeric material as it is deformed.
[0032] Figure 17B shows an alternative shear force sensor where resistance is measured between two electrodes connected by a structure that varies in resistance as a result of shear induced deformation. In particular, the structure is arranged so that it elongates and deforms under shear force. The resistance of the structure changes as a result of such elongation.
[0033] Shown in Figure 18 is an alternative shear force sensor, where frictional force may be measured by allowing relative movement between two rigid bodies.
[0034] Figure 19A shows an example of a device where a base and a cover are separated by an elastomeric layer that deforms as the cover moves across a surface. In this case, a measurement is obtained for the entire device indicating the total frictional force experienced.
[0035] Figure 19B shows a plan view of a device having a lower surface consisting of concentric rigid bodies that are separated from a base by an elastomeric material. The rigid bodies are physically separated from each other by small gaps so that they can move separately with respect to a base. Electrodes attached to the elastomeric material connecting the rigid bodies may be used to obtain separate resistance measurements to indicate the amount of frictional force experienced by different rigid bodies. [0036] Figure 20 illustrates how a wafer may move with respect to a pad in one embodiment. The pad is preferably a circular pad that rotates clockwise. The wafer rotates counter-clockwise and is moved laterally across the pad.
[0037] Figure 21 A shows a device that measures shear force at different radial and angular locations across a surface. Figure 21 A shows the bottom (cover) side of a device similar to that of Figure 19B but with separate rigid bodies (separate shear force sensors) for different angular zones.
[0038] Figure 2 IB shows an alternative device for measuring shear force at different locations on a surface. Cut-outs are formed in a cover for shear force sensors with room to allow some displacement.
DETAILED DESCRIPTION OF EXEMPLARY EMBODIMENTS
[0039] Process Condition Measuring Devices (PCMDs) include instrumented wafers that have physical dimensions the same, or close to, those of a production wafer and that include sensors and electronics to measure at least one process condition. Various PCMDs are described in US Patent Application Nos. 10/718,269, 10/837,359 and 11/381,992. PCMDs may be wired or wireless. A wired PCMD sends data to an external unit over wires (or optical fibers). A wireless PCMD either stores data in a memory in the PCMD or may transmit the data to an external unit. Generally, wireless PCMDs are more suitable for studying processes where a wafer is rotated such as CMP.
[0040] One way to measure pressure on a wafer surface is to form a cavity within the wafer, leaving a thin layer over the cavity that acts as a diaphragm and deflects under pressure. Figure 2 shows an example of a wafer 211 having a cavity 213 that is covered by a diaphragm 215. Under pressure, the diaphragm 215 deflects by an amount δ that depends on the external pressure. In general, δ may be used as an indicator of pressure applied to the lower surface of the wafer 211. Where a suitable sensor is used to sense deflection, and electronics are provided in the wafer 211 to store sensor data or transmit sensor data (or store and later transmit data), such a PCMD may provide actual pressure data during a process such as CMP. Pressure on the lower surface of a substrate during CMP is generally less than five pounds per square inch (5psi), in addition to atmospheric pressure. In some cases, pressures may be up to 15psi, or even greater.
[0041] Various methods may be used to measure the deflection of a diaphragm such as diaphragm 215 of Figure 2. One convenient method is to form a first capacitor electrode on the diaphragm, another electrode capacitively coupled to the first capacitor electrode fixed within the cavity and measure any change in capacitance. A second convenient method is to use a strain gauge. In general, it is preferable that the deflection in a diaphragm used in this application should be small so that the surface being eroded behaves similarly to that of a production wafer that does not contain cavities and does not deflect in this way. Generally, such a deflection is maintained at less than 10 microns, though in some cases deflections may exceed 10 microns. This may be achieved by choosing appropriate dimensions and material of the appropriate flexibility for the diaphragm and wafer of Figure 2.
[0042] Figures 3A-3D show different embodiments where capacitance is used to measure deflection. These capacitive pressure sensors use a cavity formed in a laminated wafer. A laminated wafer or other sturcture is formed to include a base and a cover, the base generally being thicker than the cover. The cover, or a portion of the cover, is sufficiently thin so that it deflects under pressure. The base is generally formed by thinning a Silicon wafer and the cover is generally formed by thinning a Silicon wafer that has been processed up to a point where it is to be subjected to CMP processing. In this way, the lower surface of the cover closely resembles the lower surface of a production wafer including the same materials and topology. The base and cover are attached to form a single unit. In general, the thickness of the unit (PCMD) formed is such that the pressures at the lower surface of the unit are close to those of a production wafer. This may require a thickness that is close to the thickness of a production wafer because a thicker PCMD would generally be stiffer and thus distribute pressure differently. Preferably, these capacitive pressure sensors simulate a real work piece or substrate that is undergoing a CMP process or a substrate to which a CMP head is to be applied (where the CMP head needs to be tuned). For this purpose, it is preferable for the laminated wafer or structure to have properties (such as one or more of the following: dimensions, hardness, area and flexibility) that are substantially the same as those of a real substrate, such as a semiconductor wafer or flat panel display panel.
[0043] Figure 3A shows a cross section of a first capacitive pressure sensor where a cavity 321 is formed in a separation layer 323 that extends between a base 325 and a cover 327. The separation layer 323 may be formed of a material such as Kapton® polyimide film that may be have cut-outs formed according to a predetermined pattern. An electrical insulator 329a is formed on the cover 327 and a capacitor electrode 331a is formed on the insulator 329a. In one example, the insulator is between 5 microns and 50 microns thick. The electrode 331a may be formed by attaching a metal foil or by depositing a metal layer. An insulator 329b and electrode 331b are similarly formed on the base 325. The base 325, cover 327 and separation layer 323 are aligned during assembly so that the electrodes 331a, 331b are in cavity 321. In this embodiment, no special topology is formed in opposing surfaces of either the base 325 or the cover 327. These surfaces of the base 325 and the cover 327 may be planar.
[0044] Figure 3B shows an alternative embodiment where a cavity 333 is formed into a base 335. The cavity 333 may be machined, etched or otherwise formed in the base 335. An insulator 337a is then formed in the cavity 333 and an electrode 339a is formed on the insulator 337a as before. An electrode 339b and insulator 337b are similarly formed on the cover 341.
[0045] Figure 3C shows an alternative embodiment where a cavity 343 is formed into a cover 345. Insulators 347a, 347b and electrodes 349a, 349b are formed as before. The cover 345 may be relatively thick in this example because it is reduced to a suitable thickness where cavities are formed. The examples of Figures 3A-3D show three locations for the cavity: in a separation layer, in a base, and in a cover. A cavity may also be formed in a combination of these components, for example partially in the base and partially in the cover, or partially in a separation layer and partially elsewhere, either in the base or in the cover or in both. [0046] It should be noted that the drawings are not to scale and are not intended to accurately represent the relative proportions of the features shown. Certain dimensions are exaggerated to more clearly show the structures. In one example, a capacitive sensor includes a cavity having a diameter of 10 millimeters and an electrode of between 3 and 10 millimeters diameter, with a spacing between electrodes of 25-50 microns. The diaphragm may have a thickness between 125 microns and 800 microns. The insulators in this example have a thickness of 25 microns and the electrodes have a thickness of less than 25 microns. In other examples, different dimensions may be used. Such a capacitive sensor may be able to resolve pressure to an accuracy of 0.01 pounds per square inch.
[0047] Figure 3D shows another embodiment where instead of forming local insulators to isolate capacitor electrodes from the underlying surface, blanket insulating layers 351a, 351b are formed on both a base 353 and on a cover 355 respectively. A blanket layer extends over all exposed surfaces on at least one side of a wafer. The blanket layer is formed in such a way that the wafer is not warped and thus retains a substantially planar surface. Such an insulating layer may be formed by deposition or may be grown, such as by growing a Silicon Dioxide layer on a Silicon surface. Where a cavity is formed in either the cover or the base, the insulating layer may be formed after the cavity is formed so that the insulating layer extends across surfaces of the cavity. A blanket insulating layer may be used as an alternative to individual insulators in any of the above examples.
[0048] The base and cover may be electrically isolated from each other in some cases or may be electrically connected as described in US Patent Application No. 11/381,992. The base and cover may be formed of either doped or undoped material and so may have different electrical conductivities according to requirements. Where the base and cover are undoped or have little doping so that the resistivity of the base and cover material is high, it may be possible to place electrodes directly on the surface of the base or cover (without an insulator or insulating layer). Where either the base or the cover is conductive, a parasitic capacitor may be formed between the conductive base (or cover) and an electrode that is separated from it by an insulator. In order to reduce the effects of such a parasitic capacitor, dimensions may be chosen so that the capacitive sensor has a greater capacitance than the parasitic capacitor.
[0049] Figure 4 A shows a plan view of a base 459 formed from a bare Silicon wafer. The base contains a number of cavities, including cavity 461. Within these cavities insulators, such as insulator 463, are formed. Capacitive sensor electrodes, such as electrode 465, are formed on the insulators. Thus, the base 459 of Figure 4A corresponds to the base 335 shown in Figure 3B. Figure 4A also shows interconnects (pads), including interconnect 467 that form connections between the top capacitive sensor electrodes and the electronics in the base. Both electrodes are connected to electronic circuits (not shown) in the base to allow the capacitance to be measured. The cavities and electrodes of this example are circular in shape, in other examples square, rectangular or other shaped cavities and electrodes may be used. The shapes of the electrode or electrodes are not necessarily the same as the shapes of the cavities in which they are located. Figure 4A shows sensor cavities extending along a diameter of the base. It may generally be assumed that the pressure distribution in a CMP process is radially symmetric (having the same pressure at all points along a given radius). However, in some cases sensor cavities may be distributed in a different manner so that pressures at are obtained at different angular locations.
[0050] Figure 4B shows a plan view of a cover 469 formed from a thinned bare Silicon wafer. Cover 469 is designed to be attached to the base 459 of Figure 4A to form an instrumented wafer that includes a number of capacitive pressure sensors. Insulators, such as insulator 471, are formed on the cover 469 and capacitive sensor electrodes, such as electrode 473, are formed on the insulators. Also shown are interconnects to the base, including interconnect 475. These interconnects are aligned with interconnects on the base to form an electrical connection between electrodes and the electronics.
[0051] Figure 5 A shows a plan view of a base 577 of a PCMD according to another embodiment. In the example of Figure 5A, no separate insulators are provided on the base 577 because the base 577 is formed from a Silicon wafer with an insulating layer (as shown in Figure 3D). Capacitive sensor electrodes, including electrode 579, are placed directly on the insulating layer. Cavities, such as cavity 581, may either be formed in the base 577 or may be formed in a spacer layer that has holes located between electrodes of the base and cover. In general, some electronic circuits (not shown) are also located in or on such a base and such electronic circuits are connected to the electrodes on the base and the electrodes on the cover.
[0052] Figure 5B shows a plan view of a cover 583 designed to be attached to the base 577 of Figure 5A to form a PCMD (instrumented wafer). Cover 583 has an insulating layer formed of Silicon dioxide or other suitable dielectric material and so does not require separate insulators under individual electrodes. Electrodes, such as electrode 585, are formed (by deposition or otherwise) directly on the insulating layer. Figure 5B also shows interconnects, including interconnect 587 that connect the electrode of the cover to electronics in the base 577. A groove (or trench) 579 is provided to allow connection between the electrode 585 and the interconnect 587. An electrical connection between the interconnect and the electrode may be formed by the same deposition step that forms the electrode 585 or may be formed separately. In one example, electrodes and interconnects are formed by silk screening or similar thick film techniques.
[0053] In general, where a cavity is formed for a pressure sensor, it is desirable to isolate the cavity from the exterior environment. This prevents foreign material from entering the cavity, which could affect sensor performance. In particular, slurry used in CMP could cause damage to electrodes and other components if it entered such a cavity. However, an isolated cavity may experience a significant increase in pressure as a diaphragm is deflected. Even though the change in the volume of the cavity is small, if the cavity itself is small, the change in volume and hence the change in pressure may be significant. Such a pressure change is generally undesirable because it may cause a non-linear relationship between deflection and the external pressure.
[0054] One way to reduce the pressure change caused by a diaphragm deflecting into a cavity is to provide an additional volume in communication with the cavity. This additional volume reduces the effect of volume change caused by diaphragm deflection on pressure in the sensor cavity. The additional volume may be considered a reservoir. Such a reservoir is generally formed so that its volume does not change as a result of external pressure. For example, support may be provided to ensure that significant deflection does not occur in a reservoir.
[0055] Figure 6A shows a first example of a wafer 689 having sensor cavities with reservoirs. For example, sensor cavity 691 connects with reservoir 693. A reservoir may be formed as a cavity in the base (or cover, or separation layer, or a combination of these components) in the same manner as the cavity for the sensor. A channel 695 connects the reservoir 693 to the sensor cavity 691. To avoid significant volume change in a reservoir, supporting structures 697 extend across a reservoir to limit any deflection that might occur in the cover over this area. Each sensor cavity of Figure 6A has a dedicated reservoir. In some cases, a reservoir may be deeper than a sensor cavity so that its volume is greater for a given cross sectional area.
[0056] Figure 6B shows an alternative configuration to that of Figure 6A. In
Figure 6B, instead of dedicated reservoirs, sensor cavities 699a-i share a reservoir system that interconnects cavities 699a-i and reservoirs 602a, 602b. Such a reservoir system may be formed by the same process used to form sensor cavities 699a-i. A pattern of sensor cavities, reservoirs and interconnecting channels may be formed in the base (and/or other components) as shown. In this example, the reservoir system is isolated from the exterior of the PCMD so that no foreign matter can enter the reservoir system and the pressure in the reservoir system remains stable.
[0057] In some cases it may be desirable to have an opening from a reservoir system in a PCMD to the exterior of the wafer. For example, it may be desirable to equalize the pressure in the reservoir system with the ambient pressure. In some cases, equalization may be used to eliminate a pressure differential that might be caused by different atmospheric pressure resulting from use at different altitudes or in different weather conditions. It may also be desirable to bring the reservoir system to a predetermined condition before use. For example, the reservoir system may be brought to a desired pressure, either above atmospheric pressure or below atmospheric pressure (under vacuum). The reservoir system may also be filled with a particular gas or mixture of gases if desired.
[0058] Figure 7 shows an example of a PCMD 704 with a reservoir system that has an opening 706 to the exterior of PCMD 704. A valve is provided to selectively connect the opening 706 to the reservoir system. Microelectromechanical Systems (MEMS) technology enables valves and other components to be formed on an extremely small scale. A MEMS valve 708 may be formed in the base, or may be formed separately and attached to the base. The MEMS valve may be controlled by electronic circuits in PCMD 704. When PCMD 704 is in use, the MEMS valve will generally remain closed to prevent foreign matter entering the reservoir system. The MEMS valve 708 may be opened by an electronic circuit in PCMD 704, generally in response to a signal provided from outside PCMD 704. This may occur during a calibration or initialization procedure. An alternative to a MEMS valve is to provide a temporary blockage that covers the opening 706. A suitable material, for example a polymer such as Silicone, may be used to block the opening. The blockage formed may be removed to configure the reservoir system.
[0059] In general, electronic circuits are provided in a PCMD to store data from the sensors. Circuits may alternatively transmit data to a receiver outside the PCMD. In some cases, data is first stored and then transmitted. Such circuits may be formed and connected in a number of ways. In one arrangement, electronic circuits include one or more integrated circuits that are placed in cavities in a base (or cover). The integrated circuits are bonded in place. Electrical connections between integrated circuits and sensors are provided by conductive traces formed on the surface of the base (or cover). Connection pads on the integrated circuits may be bonded to these traces. Integrated circuits used in this configuration may be used in the form of semiconductor dies so that they have small profiles and small thermal capacities. Instead of using traces on a surface, insulated wires may extend between components including sensors and integrated circuits. Such wires may be bonded to the components and may run through trenches formed within a PCMD. [0060] In another arrangement, electronic circuits and connections between circuits are formed as a flex circuit assembly that is attached to a base. Generally, cavities and grooves are formed in the base so that such a flex circuit presents a surface that is flush with the surface of the base. A cover may then be attached. Descriptions of the use of such flex circuits and traces in PCMDs are provided in US Patent Application Nos. 10/837,359 and 11/381,992.
[0061] An example of a PCMD 810 that includes a flex circuit 812 is provided in Figure 8 A. The flex circuit 812 includes at least one microprocessor 814 that is in communication with the sensors. Microprocessor 814 may include a memory for storing data from the sensors, and/or transmitter circuits for transmitting such data to an external device, preferably by wireless transmission, such as radio waves. In addition, the flex circuit 812 provides power connections between the battery 816, or batteries, and other components. In addition to capacitive sensors 818a-i, Figure 8A shows temperature sensors Tl, T2 and T3. Sensors Tl, T2, T3 are located close to capacitive pressure sensors 818a-c so that an individual temperature sensor may provide temperature for a specific capacitive sensor. In some examples a temperature sensor is provided for each pressure sensor 818a-i. In this way, the temperature for a particular capacitive sensor may be used to compensate for any temperature variation that might affect the physical or electrical behavior of the capacitive sensor. Temperature sensors Tl, T2, T3 may be formed as part of the flex circuit 812 or may be separately formed and attached to the flex circuit 812.
[0062] Figure 8B is a side view of a member such as a plate with a base 824 and a cover 822 enclosing a cavity housing a pair 826 of capacitively coupled electrodes 826a and 826b not connected to the cover to sense a parasitic capacitance in the plate to illustrate another embodiment of the invention. Electrodes 826a and 826b are separated by a dielectric layer 828. Figure 8C is a top plan view of two pairs 826 and 836 of capacitively coupled electrodes adjacent to one another, one pair (826) not connected to the cover to sense a parasitic capacitance in the plate, and the other pair (836) connected (not shown in Figure 8B) to the cover to sense a deflection of the cover. The capacitance of pair 826 is an indication of the parasitic capacitance experienced by pair 836. Thus, the capacitance of pair 826 may be used to adjust the measurement of the deflection of cover 822 by pair 836, so as to reduce the effect of the parasitic capacitance experienced by pair 836 on the measurement. This may be performed by microprocessor 814 in Figure 8 A, after the microprocessor 814 receives data related to the capacitances of pairs 826 and 836 through flex circuit 812 in Figure 8A, and the change in capacitance of pair 836 caused by deflection of the cover 822.
[0063] Where electrodes are formed on the base and cover, these electrodes are connected to the flex circuit so that electronic circuits within the flex circuit can detect any capacitance change. Similarly, temperature or other sensors that are not formed integrally with the flex circuit are connected to the flex circuit. Figure 9 shows an example where an electrode 920 on a cover 922 is connected to a pad 924 on a flex circuit 926. The electrode 920 is connected to an interconnect 928 that is outside the sensor cavity 930 (as shown in Figure 5B). The interconnect 928 is isolated from the cover 922 by an insulating layer 932A on the cover 922. Pad 924 on the flex circuit 926 overlies the interconnect 928 and this pad is electrically connected to one or more integrated circuits in the flex circuit 926. The interconnect 928 is attached to the pad 924 by an electrically conductive epoxy 934. A similar connection (not shown) may be made to the base electrode 936. Similar connections may be formed for temperature sensors. Flex circuit 926 lies in trench 938 in this example. Thus, the electronics is partially in the cavity (the electrodes 920 and 936), and partially (flex circuit 926) in the trench 938 which can serve also as a reservoir to reduce the effect of deflection of the cover on the pressure measurement.
[0064] Figure 10 shows another embodiment where a capacitive sensor is formed integrally with a flex circuit 1042. The flex circuit includes two electrodes 1044a, 1044b that are separated by a dielectric layer 1046 to form a capacitor 1040. The dielectric layer 1046 may be formed of a suitably compressible elastomeric material. The portion of the flex circuit 1042 that contains the capacitor is bonded to both the base 1048 and the cover 1050 using thin layers 1052a, 1052b of adhesive. Flex circuit 1042 lies in trench 1056.
[0065] In the examples of both Figures 9 and 10, trenches are provided for the flex circuits 926, 1042. Trenches 938, 1056 connect to the sensor cavities 930, 1054 respectively. Generally, a flex circuit does not fully occupy the flex circuit trench so that some unoccupied volume remains around the flex circuit. This extra volume allows for some gas flow through the trenches formed for the flex circuit. Also, some unoccupied volume generally remains around some integrated circuits of the flex circuit. Thus, the unoccupied volumes within the trenches and cavities formed for the flex circuit may form a reservoir system that reduces pressure variation within sensor cavities. A controlled opening from such a reservoir system to the exterior of the PCMD may be provided as previously described.
[0066] In one example, a flex circuit includes one or more capacitive sensors, or is attached to one or more capacitive sensors, and also includes electrical connections from the one or more sensors to an integrated circuit that provides an output that is dependent on the capacitance of the capacitive sensor. An example of an integrated circuit that may be used is an Analog Devices AD7746 capacitance to digital converter. This integrated circuit provides an output that may then be sent to a microprocessor for storage or transmission. In an alternative embodiment, capacitors connect directly to a microprocessor that performs a capacitance to digital conversion internally.
[0067] An alternative to using a capacitive sensor to measure pressure is to use a strain gauge. A sensor cavity may be formed according to any of the examples described above so that a diaphragm is formed that will deflect under pressure. Instead of placing capacitor electrodes on either side of this cavity, a strain gauge is placed so that it will be deflected as the diaphragm is deflected.
[0068] Figure 11 shows a first example where a sensor cavity 1158 is formed within a base 1160 (note that this drawing shows the cover 1162 above the base 1160, the opposite orientation to that of previous drawings and the opposite to the orientation during CMP). Spacers 1164a, 1164b are placed under a strain gauge 1166 so that the strain gauge 1166 can deflect downwards. A deflection augmenting element 1168 (such as a small bead, tube, corrugated structure or some other small rigid body) is placed between the upper surface of the strain gauge 1166 and the cover 1162. Thus, any deflection in the cover 1162 will cause the strain gauge 1166 to deflect. The deflection augmenting element 1168 causes a greater deflection in strain gauge 1166 than the deflection in cover 1162, thus augmenting the measurement obtained, which may increase resolution. In one example, a deflection augmenting element is machined into either a cover or a base. The strain gauge 1166 may be connected to electronic circuits in the base 1160 as previously described.
[0069] Figure 12A shows an alternative arrangement where a strain gauge
1272 is bonded to a cover 1274 so that the strain gauge 1272 deflects along with the cover 1274. A suitable strain gauge may be a resistive strain gauge, a piezoresistive strain gauge, a piezoelectric strain gauge or a semiconductor strain gauge such as a bar gauge.
[0070] Figure 12B shows an alternative embodiment to that of Figure 12 A.
Here a cavity 1276 is formed in cover 1278 and a strain gauge 1280 is formed on cover 1278. Base 1282 may be planar in this example.
[0071] Figure 13 shows an embodiment where pressure sensors 1384a-d are placed between a wafer 1386 and a CMP head 1388. A production wafer may be used for wafer 1386 or a PCMD may be used instead. Pressure sensors may be capacitive sensors formed from two metal electrodes separated by a compressible dielectric. In one example, sensors 1384a-d are attached to wafer 1386. In another example, sensors 1384a-d are attached to the CMP head. In either case, sensors 1384a-d measure the pressure between the CMP head 1388 and wafer 1386 at various points on the wafer surface. Sensors 1384a-d are connected to electronics module 1388, which is mounted to CMP head 1388. Electronics module 1389 may store data from sensors 1384a-d, or may transmit the data in real time to another unit. For example, electronics module 1389 may include a Bluetooth or other wireless communication device to allow real time transmission of data.
[0072] In some cases, it may be desirable to calibrate a pressure measurement wafer (PCMD), either initially as part of a factory calibration or in the field. In some cases, the pressure readings from pressure sensors may change with use. For example, as a PCMD is subject to CMP, the thickness of a diaphragm is reduced, thus affecting pressure measurements based on the deflection of the diaphragm. One option is to coat a surface with a hard layer (for example, Silicon Nitride) to reduce erosion. However, such hard layer may have different characteristics to materials of production wafers. Another option is to deposit additional material periodically to replace material removed by CMP. This may be done at relatively low temperatures for some materials (e.g. Copper) but may require high temperatures for other materials (e.g. Silicon).
[0073] Figure 14 shows a pressure calibration apparatus that may be used to calibrate a pressure sensing PCMD as previously described. A PCMD 1490 is placed on a first surface 1492 with pressure sensors facing up. A second surface 1494 is located at a fixed distance above first surface 1492 and an inflatable bladder 1496 is placed between the PCMD 1490 and second surface 1494. Inflatable bladder 1496 is inflated to a predetermined pressure (or to a series of predetermined pressures) through pressure regulator 1498. Sensor readings may be recorded for each sensor at each predetermined pressure applied, and this data may be used to calibrate the sensor readings. A PCMD may be periodically calibrated in this manner to correct for removed material or other effects. Preferably, the pressure sensors are heated or cooled to predetermined temperatures by means of a temperature control instrument 1450.
[0074] Generally, a PCMD according to certain examples described above is used by placing it, with the cover side down, in a CMP processing system. The PCMD undergoes the same process that a production wafer goes through. During the process, the PCMD measures pressure at different locations across the lower surface. The data generated from such measurements is stored in a memory. After processing, the data is downloaded and analyzed to provide information about pressure across the PCMD as a function of time. Temperature data may be separately recorded. Temperature data may also be used to compensate pressure sensor reading for any temperature effects.
[0075] Various examples refer to CMP applications for a pressure sensing wafer or PCMD. However, such a pressure sensing wafer may be used in various other processes including processes that take place at pressures greater or less than atmospheric pressure. One example of a process that may be studied using a pressure sensing wafer is an immersion photolithography process, where pressure caused by an air knife (used to contain a water puddle) may be measured. Another process is CMP scrubbing or cleaning, a process that cleans a wafer after CMP. The pressure applied to the wafer during such a clean process may affect the cleanliness of the wafer. Certain processes hold a wafer to a chuck by electrostatic force. The force that such an electrostatic chuck (ESC) applies may vary over time and may be adjusted to prevent wafers from moving during processing. A pressure measuring PCMD may be used to measure the pressure between a wafer and such a chuck to determine the appropriate adjustment (if any). Substrates other than Silicon wafers may be instrumented to form a PCMD. For example, GaAs wafers or Flat Panel Display (FPD) substrates may be similarly provided with cavity based sensors.
[0076] In one embodiment, a PCMD has the same diameter as a 200 millimeter or 300 millimeter wafer and the same (or similar thickness). The PCMD includes at least one cavity that has a sensor to detect deflection into the cavity caused by external pressure. The PCMD may further include at least one temperature sensor. The PCMD may also include a flex circuit with at least one integrated circuit and conductors between the integrated circuit and sensors. The PCMD may also include at least one battery. A sensor to detect deflection in a cavity may be capacitance based or strain gauge based. A cavity may be connected to a dedicated reservoir or to a shared reservoir. A reservoir may be provided with an external opening.
[0077] In general, removal of material in CMP is caused by two mechanisms: mechanical action and chemical action. Although these mechanisms are closely linked, it may be desirable to try to separately measure parameters associated with each. One measurement that may be of particular value in measuring mechanical action is the frictional force between a wafer and a pad as the wafer moves with respect to the pad. Generally, mechanical abrasion of material increases with increasing frictional force. Frictional force may be used to provide a shear force in a structure that deforms in a manner that indicates the magnitude of the shear force. In general, greater frictional force provides greater mechanical action in removing material during CMP. [0078] Figure 15 shows a CMP head 1501 and an attached wafer 1503 moving with velocity V with respect to a pad 1505. A layer of slurry 1507 extends across pad 1505. As wafer 1503 moves horizontally, it is pressed into pad 1505 so that there is some pressure between wafer 1503 and pad 1505. As wafer 1503 moves to the right in Figure 15, it experiences a frictional force opposing its motion, indicated by force F. Frictional force F generally depends on the coefficient of friction and also the normal force (pressure) between wafer 1503 and pad 1505. However, as discussed above, pressure is not always uniform across a wafer surface during CMP. Also, the velocity of relative motion between a wafer and a pad is not always constant across a wafer. A wafer may be rotated, resulting in a higher velocity for outer portions of the wafer than for inner portions. Also, the pad may rotate or otherwise move in a manner that does not provide uniform velocity across a wafer surface. It may be useful to measure frictional force at different locations across a wafer surface during CMP in order to estimate mechanical abrasion.
[0079] Figures 16A and 16B illustrate the effect of shear force on a structure
1609 that is designed to deform under shear stress. Figure 16A shows a first rigid body 1611 in contact with a surface 1613. First rigid body 1611 is connected to second rigid body 1615 by a portion of elastomeric material 1617. Figure 16A shows structure 1609 at rest with respect to surface 1613. Figure 16B shows structure 1609 in motion, having velocity V, with respect to surface 1613. Structure 1609 is moved by applying a force through second rigid body 1615. As a result of relative motion between first rigid body 1611 and surface 1613, a frictional force F is created. Frictional force F acts as a shear force causing portion of elastomeric material 1617 to deform. For example, elastomeric material 1617 may comprise a silicone elastomer with conductive elements dispersed therein, such as small flakes, platelets, fibers or nanotubes. In this case, the deformation causes an offset of d between first rigid body 1611 and second rigid body 1615 compared with their unloaded positions. The magnitude of d is a function of F. A shear force sensor may be formed from two rigid bodies that have a limited range of relative displacement under shear force and have some mechanism for measuring displacement. Preferably structure or member 1609 simulates a real work piece or substrate that is undergoing a CMP process. For this purpose, it is preferable for its surface in contact with surface 163 to have a coefficient of friction that is substantially the same as that of a real substrate, such as a semiconductor wafer or flat panel display panel. It is preferable for the structure 1609 to have dimensions that are substantially the same as those of a real substrate. The shear force is applied in a direction so that the force has at least one component that is perpendicular to the surfaces of structure 1609 and surface 1613.
[0080] In one example, shown in Figure 17A, a shear force sensor 1718 measures deformation due to shear force on an elastomeric material through changes in the electrical properties of the elastomeric material as it is deformed. In particular, the electrical resistance of such an elastomeric material may change as the material is deformed. Electrodes may be provided to detect changes in the resistance of such an elastomeric material. Figure 17A shows an example where electrodes 1719a, 1719b are embedded in an elastomeric layer 1720 and an electrical resistance measuring unit 1721 measures an electrical resistance (also referred to herein as simply "resistance", the two terms used interchangeably herein) between them. Some elastomeric materials may be formed with anisotropic electrical characteristics. A suitable elastomeric material with anisotropic electrical characteristics may comprise a silicone elastomer with conductive elements dispersed therein, such as small flakes, platelets, fibers or nanotubes. For example, such materials may be electrically conductive in one direction and nonconductive in another direction. Such materials may be formed so that a resistance changes with a deformation caused by shear (horizontal) force but is not significantly affected by a compressive (vertical) force. Electrodes for resistance measurement may be formed in the elastomeric material or on one or both surfaces on either side, for example as patterns of interdigitated fingers.
[0081] Figure 17B shows an alternative shear force sensor 1799 where resistance is measured by an electrical resistance measuring unit (not shown), such as unit 1721 of Figure 17A, between electrodes 1797a, 1797b, which are connected by a structure 1795 that varies in resistance as a result of shear induced deformation. In particular, structure 1795 is arranged so that it runs diagonally through elastomeric layer 1793. Thus, structure 1795 elongates as elastomeric layer 1793 deforms under shear force. The resistance of structure 1795 changes as a result of such elongation. Structure 1795 may be formed of metallic platelets (e.g. Aluminum), carbon fibers, carbon black particles or similar small conductive bodies that form a conductive pathway. As the conductive pathway is stretched, conduction diminishes because of poor contact between conductive bodies. Structure 1795 is generally not sensitive to downward pressure.
[0082] In an alternative shear force sensor 1822, shown in Figure 18, factional force may be measured by allowing relative movement between two rigid bodies. A lower rigid body 1823 includes a protrusion 1825 that extends into a cavity 1827 in an upper rigid body 1829. The location of protrusion 1825 within cavity 1827 is established by springs or some other mechanism that allows some lateral movement when force is applied (e.g. elastomeric material). As lower rigid body 1823 moves across a surface 1831, a frictional force F is generated that tends to cause lower rigid body 1823 to move with respect to upper rigid body 1829. Such a relative movement may be observed as a change in distances dl, d2 between protrusion 1825 and walls of cavity 1827. Distances dl and d2 may be measured by any suitable technique including capacitively or using piezoelectric material. Shear force may occur in any lateral direction, so a shear force sensor may detect displacement from a static condition in more than one direction. For example, shear force sensor 1822 may also measure distances perpendicular the cross section shown. Thus, both the magnitude and direction of shear force may be measured. Figure 18 shows upper rigid body 1829 in contact with surface 1831. In other examples, such an upper rigid body may not have any contact with a surface and only the lower rigid body is in contact. Upper rigid body 1829 may be a base of a PCMD that includes electronic components that receive data from shear force sensor 1822.
[0083] A PCMD may measure frictional force using the structures described above. Figure 19A shows a first example of a PCMD 1936 where a base 1933 and a cover 1935 are separated by an elastomeric layer 1937 that deforms as cover 1935 moves across a surface. In this case, a measurement is obtained for the entire PCMD 1936 indicating the total frictional force experienced. However, in some cases, it is desirable to obtain values for frictional force at different points on a wafer, or PCMD. [0084] Figure 19B shows a plan view of a PCMD 1938 having a lower surface consisting of concentric rigid bodies 1939a-d that are separated from a base (not shown) by an elastomeric material. Rigid bodies 1939a-d are physically separated from each other by small gaps so that rigid bodies 1939a-d can move separately with respect to a base. As PCMD 1938 rotates, frictional force is different for different rigid bodies 1939a-d. Electrodes attached to the elastomeric material connecting rigid bodies 1939a-d may be used to obtain separate resistance measurements to indicate the amount of frictional force experienced by different rigid bodies. In this way, instead of a single measurement of frictional force experienced by a PCMD, four different measurements are obtained, representing shear force experienced by four concentric zones of a wafer. Thus, PCMD 1938 may be considered to have four concentric shear force sensors.
[0085] In some cases, it may be desirable to obtain shear force measurements for zones having different angular displacements as well as different radial displacements. Figure 20 illustrates how a wafer 2041 may move with respect to a pad 2043. Pad 2043 is a circular pad that rotates clockwise in this example by an instrument 2050, such as a motor in a conventional manner. Wafer 2041 rotates counter-clockwise and is moved laterally across pad 2043 by an instrument 2052 such as a motor and a gear mechanism in a conventional manner, which instrument may be one and the same as instrument 2050. The result of these different movements is that the speed with which a point on the wafer surface moves with respect to the pad beneath it changes as the wafer rotates. For example, as shown in Figure 20 the right side of wafer 2041 experiences a higher speed with respect to the underlying portion of pad 2043 than the left side of wafer 2041. Thus, shear force for a particular location on the wafer surface may oscillate from low to high. Also, the shear force changes as wafer 2041 moves laterally across pad 2043. By measuring localized shear forces, additional information may be obtained, such as maximum and minimum shear forces and patterns in changing shear force.
[0086] Figure 21 A shows a PCMD 2147 that measures shear force at different radial and angular locations across a surface. Figure 21 A shows the bottom (cover) side of a PCMD 2147 similar to PCMD 1938 but with separate rigid bodies (separate shear force sensors) for different angular zones. Thus, instead of measuring average frictional force for different radial zones, PCMD 2147 measures frictional force for four different portions of each radial zone. This may provide maximum and minimum shear force information that may be useful.
[0087] Figure 2 IB shows an alternative PCMD 2149 for measuring shear force at different locations on a surface. Whereas in earlier figures the shear force sensors on the lower surface of a PCMD occupied the entire lower surface (or nearly the entire lower surface), here shear force sensors 2151 a-i occupy only a portion of the lower surface of PCMD 2149. Cut-outs are formed in a cover for shear force sensors 2151 a-i with room to allow some displacement. PCMDs 1936, 1938, 2047 and 2149 may measure shear force using a shear force sensor such as sensors 1718 or 1799 that use elastomeric material, or a shear force sensor such as sensor 1822 that uses displacement, or using any other suitable shear force sensor. In general, one or more shear force sensors may be combined with other sensors in a PCMD. In particular, it may be desirable to include pressure sensors to measure compressive force, temperature sensors and material removal rate sensors for CMP applications. A microprocessor (not shown) similar to microprocessor 814 in Figure 8 A may be used to receive the data from the shear force sensors such as sensors 1718 and 1799, and data from other sensors through flex circuits of the type described above. Preferably such microprocessor includes a memory for storing data from the sensors, and/or transmitter circuits for transmitting such data to an external device, preferably by wireless transmission, such as radio waves.
[0088] In some PCMDs, sensors may collect acoustic input that is used to characterize a CMP process. For example, as a surface is eroded, a frequency of wafer vibration may change. This change may be detected by one or more acoustic sensors in the wafer or in a CMP head and used to obtain information regarding the amount of material removed. Thus, certain acoustic sensors may be considered removal rate sensors.
[0089] All patents, patent applications, articles, books, specifications, other publications, documents and things referenced herein are hereby incorporated herein by this reference in their entirety for all purposes. To the extent of any inconsistency or conflict in the definition or use of a term between any of the incorporated publications, documents or things and the text of the present document, the definition or use of the term in the present document shall prevail.
[0090] Although the various aspects of the present invention have been described with respect to certain preferred embodiments, it is understood that the invention is entitled to protection within the full scope of the appended claims.

Claims

CLAIMS:
1. A process condition measuring device for measuring pressure or force on a surface of a substrate undergoing a process, said device comprising: a member having a property that is substantially the same as a property of the substrate, said member comprising a diaphragm; and sensor means physically connected to the diaphragm, wherein said sensor means is for measuring deflection of the diaphragm when the diaphragm is in contact with and pressed against a surface employed in said process, said sensor means comprising at least one pair of capacitively coupled electrodes, wherein a capacitance of the at least one pair varies as a function of deflection of the diaphragm.
2. The device of claim 1 , wherein said diaphragm is of such flexibility that deflection of said diaphragm is not more than about 10 microns when the diaphragm is in contact with and pressed against the surface employed in the process.
3. The device of claim 1 , said member comprising a plate, wherein said property includes one or more of the following: flexibility, area, hardness and physical dimensions of the plate.
4. The device of claim 1, said member comprising a base and a cover defining at least one cavity between the base and cover for housing said sensor means, said cover comprising said diaphragm.
5. The device of claim 4, wherein said at least one cavity is formed on a surface of the base facing the cover, or on a surface of the cover facing the base.
6. The device of claim 4, said member further comprising a separation layer between the base and cover, said at least one cavity being formed in said separation layer.
7. The device of claim 4, said member defines therein at least one reservoir in communication with said at least one cavity to reduce effect of deflection of the diaphragm on pressure within the at least one cavity.
8. The device of claim 7, further comprising an opening through which the at least one reservoir communicates with an external environment, and a valve controlling such communication.
9. The device of claim 4, further comprising an electronic circuit, wherein at least a portion of said electronic circuit is in said at least one cavity, the electronic circuit comprising a memory or a wireless transmission component, the electronic circuit receiving data from the sensor means and storing the data in the memory or transmitting the data using the wireless transmission component.
10. The device of claim 9, wherein said member defines therein at least one reservoir in communication with said at least one cavity to reduce effect of deflection of the diaphragm on pressure within the at least one cavity, and at least a portion of said electronic circuit is located in said at least one reservoir.
11. The device of claim 4, said member comprising a semiconductor wafer that has dimensions and thickness that are substantially the same as those of a production semiconductor wafer.
12. The device of claim 1 , said process being a polishing or planarization process, said diaphragm comprising one or more of the following: a wear resistant coating to reduce erosion by said polishing or planarization process, and additional deposited material to replace material eroded by said process.
13. The device of claim 1, said member comprising a plate, said sensor means including a plurality of pairs of capacitively coupled electrodes distributed across the areal extent of said plate, said device further comprising a plurality of temperature sensors, wherein each of the temperature sensors is located in proximity to a corresponding pair of capacitively coupled electrodes for measuring temperature of said corresponding pair of capacitively coupled electrodes, said temperature sensors providing outputs.
14. The device of claim 13, further comprising an electronic circuit responsive to said sensor means and the outputs of the temperature sensors for adjusting measurements of each of the corresponding pairs of capacitively coupled electrodes using the output of the temperature sensor located in proximity to each of the corresponding pairs.
15. The device of claim 1, further comprising at least one reference pair of capacitively coupled electrodes that is not connected to said diaphragm for sensing a parasitic capacitance in said member.
16. The device of claim 15, further comprising an electronic circuit responsive to an output of said reference pair of capacitively coupled electrodes for adjusting measurements of said sensor means to reduce effect of the parasitic capacitance on such measurements.
17. The device of claim 15, further comprising a plurality of reference pairs of capacitively coupled electrodes that are not connected to said diaphragm for sensing a parasitic capacitance in said member, each of the plurality of reference pairs located in proximity to a corresponding pair of capacitively coupled electrodes for reducing effect of the parasitic capacitance on measurements by such corresponding pair.
18. The device of claim 1 , said process being a polishing or planarization process, and said member is suitable for undergoing said process to simulate behavior of said substrate in the process.
19. The device of claim 1 , said process being a process for tuning a polishing or planarization head.
20. A method for measuring pressure or force on a surface of a substrate that is undergoing a process, said method comprising: providing a device having a plate with a property that is substantially the same as a property of the substrate, said plate comprising a diaphragm and at least one pair of capacitively coupled electrodes, said at least one pair having a capacitance; and sensing deflection of the diaphragm when the diaphragm is in contact with and pressed against a polishing or planarization surface, said sensing comprising detecting a change in the capacitance of the at least one pair of capacitively coupled electrodes.
21. The method of claim 20, wherein said property includes one or more of the following: flexibility, area, hardness and physical dimensions of the plate, wherein said device comprises a memory or a wireless transmission component, said method further comprising storing data related to the change in the capacitance of the at least one pair of capacitively coupled electrodes in the memory or transmitting the data using the wireless transmission component.
22. The method of claim 20, further comprising measuring a parasitic capacitance in said plate and reducing effect of the parasitic capacitance on said sensing.
23. The method of claim 20, further comprising inflating an inflatable member to predetermined pressures, sensing deflection of the diaphragm caused by inflation of the member, and using heating elements to heat the plate to predetermined temperatures during the inflating and sensing.
24. The method of claim 20, said process being a polishing or planarization process, and said plate is suitable for undergoing said process to simulate behavior of said substrate in the process.
25. The method device of claim 20, said process being a process for tuning a polishing or planarization head.
26. A process condition measuring device for measuring shear force on a surface of a substrate that undergoes a polishing or planarization process, said device comprising: a member having a surface that has a property that is substantially the same as a property of the surface of the substrate, said member suitable for undergoing said process to simulate behavior of said substrate in the process; and at least one sensor attached to the member, wherein said at least one sensor measures a parameter related to a shear force on the surface of the member when such surface is in contact with and pressed against a polishing or planarization surface and a lateral force is applied between the polishing or planarization surface and the surface of the member.
27. The device of claim 26, wherein said property relates to a coefficient of friction of the surface of the member.
28. The device of claim 26, wherein said member has dimensions that are substantially similar to those of the substrate.
29. The device of claim 26, wherein said at least one sensor comprises a deformable body that deforms in response to the shear force on the surface of the member, said sensor measuring amount of deformation of the body.
30. The device of claim 29, wherein said at least one sensor further comprises a circuit that measures a change in an electrical parameter.
31. The device of claim 30, wherein said circuit measures a change in electrical resistance between two locations in said body.
32. The device of claim 30, wherein said circuit comprises a structure that varies in length and electrical resistance when said body is deformed, said circuit measuring a change in electrical resistance of said structure.
33. The device of claim 26, at least one sensor comprising two rigid bodies, wherein said lateral force causes displacement between the two rigid bodies and said at least one sensor measures said displacement.
34. The device of claim 26, wherein said member comprises a plurality of rigid bodies, each of plurality of rigid bodies having a surface that simulates a portion of the surface of the substrate in said polishing or planarization process, said at least one sensor comprises an elastomeric material with portions that separate corresponding ones of said plurality of rigid bodies from one another, and a plurality of circuits, each of said plurality of circuits measuring a change in a parameter related to deformation of one of said portions of said elastomeric material.
35. The device of claim 34, wherein said circuit measures a change in electrical resistance between two locations in said body.
36. The device of claim 34, said plurality of rigid bodies comprising a plurality of concentric rigid bodies.
37. The device of claim 36, wherein cross-sections of at least some of said plurality of rigid bodies have angular zones.
38. The device of claim 26, said member comprising a cover and a base, said base defining therein a plurality of cut-outs therein, said cut-outs distributed across a surface of said cover, said device further comprising a plurality of sensors in the cut-outs for sensing shear forces on said sensors when the surface of said cover is in contact with and pressed against said polishing or planarization surface and said lateral force is applied between the polishing or planarization surface and the surface of the cover.
39. The device of claim 26, wherein said process causes a first motion of said polishing or planarization surface, said device further comprising an instrument causing a second motion of the surface of the member, said first and second motions being in different directions.
40. The device of claim 39, wherein said first and second motions are rotational motions.
41. A method for measuring shear force on a surface of a substrate that undergoes a polishing or planarization process; said method comprising: providing a member having a surface that has a property that is substantially the same as a property of the surface of the substrate, said member suitable for undergoing said process to simulate behavior of said substrate in the process; pressing the surface of the member against a polishing or planarization surface; applying a lateral force between the polishing or planarization surface and the surface of the member; and measuring a parameter related to a shear force on the surface of the member.
42. The method of claim 41, wherein said measuring measures said parameter at a plurality of different locations across the surface of said member substantially simultaneously.
43. The method of claim 41, said process causing a first motion of said polishing or planarization surface, said method further comprising causing a second motion of the surface of the member, said first and second motions being different.
44. The method of claim 43, said first and second motions being in different directions.
45. The method of claim 43, wherein said first and second motions are rotational motions.
46. A process condition measuring device comprising: a member; at least one shear force sensor attached to the member; and an electronic circuit attached to the member, the electronic circuit comprising a memory or a wireless transmission component, the electronic circuit receiving data from the shear force or pressure sensor and storing the data in the memory or transmitting the data using the wireless transmission component.
PCT/US2007/080197 2006-10-03 2007-10-02 Systems for sensing pressure/shear force WO2008042903A2 (en)

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US11/861,207 2007-09-25
US11/861,119 2007-09-25
US11/861,207 US7497134B2 (en) 2006-10-03 2007-09-25 Process condition measuring device and method for measuring shear force on a surface of a substrate that undergoes a polishing or planarization process
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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010037218A1 (en) * 2008-09-30 2010-04-08 Research In Motion Limited Mobile wireless communications device having touch activated near field communications (nfc) circuit
WO2010124807A1 (en) * 2009-04-29 2010-11-04 Siltronic Ag Device for gauging forces impacting a semiconductor disk
US8351854B2 (en) 2008-09-30 2013-01-08 Research In Motion Limited Mobile wireless communications device having touch activated near field communications (NFC) circuit
US8681493B2 (en) 2011-05-10 2014-03-25 Kla-Tencor Corporation Heat shield module for substrate-like metrology device
WO2014068269A1 (en) * 2012-10-31 2014-05-08 University Of Southampton Apparatus for sensing and measuring pressure and/or shear components of a force at an interface between two surfaces
US9836118B2 (en) 2015-06-16 2017-12-05 Wilson Steele Method and system for analyzing a movement of a person
WO2020020779A3 (en) * 2018-07-23 2020-03-12 Abb Schweiz Ag A pressure sensor for a pipe
CN113340507A (en) * 2021-04-15 2021-09-03 安徽大学 Full-flexible three-dimensional force flexible touch sensor based on hourglass-shaped structure

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2011047893A (en) * 2009-08-28 2011-03-10 Nissha Printing Co Ltd Pressure detection unit
US8635919B2 (en) * 2009-08-28 2014-01-28 Nissha Printing Co., Ltd. Pressure detection unit and pressure detection device
KR101310012B1 (en) 2011-12-19 2013-09-24 성균관대학교산학협력단 Hybrid type multi-axis sensor
TWI470197B (en) 2012-12-20 2015-01-21 Ind Tech Res Inst Capacitive shear force sensor and method for fabricating thereof
DE102015119272A1 (en) * 2015-11-09 2017-05-11 Endress+Hauser Gmbh+Co. Kg Capacitive pressure sensor and method for its manufacture
CN108701581B (en) * 2015-12-10 2023-12-19 艾尼尔有限公司 Device and method for determining parameters of a machining operation
JP6500764B2 (en) * 2015-12-10 2019-04-17 信越半導体株式会社 Method of evaluating polishing head and method of polishing wafer
US11660722B2 (en) * 2018-08-31 2023-05-30 Applied Materials, Inc. Polishing system with capacitive shear sensor
JP2022138845A (en) * 2021-03-11 2022-09-26 株式会社荏原製作所 Wafer for measurement comprising sensor and method of using the same
WO2022196131A1 (en) * 2021-03-17 2022-09-22 株式会社村田製作所 Pressure sensor device

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3815566A1 (en) * 1988-05-06 1989-11-16 Siemens Ag Method for determining mechanical stress conditions in electrical or electronic components to be coated, or already coated, with moulding compound
WO1990013425A1 (en) * 1989-05-08 1990-11-15 American Composite Technology Inc. System and method for monitoring pressure during the production of fiber reinforced polymers
DE4413442A1 (en) * 1994-04-18 1994-09-08 Fm Automation Elektronik Gmbh Assembly platform with a process-observing function
WO2000028277A2 (en) * 1998-11-06 2000-05-18 Wisconsin Alumni Research Foundation Micromachined strain sensor
US6129613A (en) * 1998-01-30 2000-10-10 Philips Electronics North America Corp. Semiconductor manufacturing apparatus and method for measuring in-situ pressure across a wafer
US20030022595A1 (en) * 2001-07-24 2003-01-30 Chien-Hsin Lai Wafer pressure regulation system for polishing machine
US20040023606A1 (en) * 2002-01-17 2004-02-05 Yuchun Wang Advanced chemical mechanical polishing system with smart endpoint detection
US20040098216A1 (en) * 2002-11-04 2004-05-20 Jun Ye Method and apparatus for monitoring integrated circuit fabrication
US20050239371A1 (en) * 2003-09-09 2005-10-27 Tetsuji Togawa Pressure control system and polishing apparatus
US20050263760A1 (en) * 2004-05-28 2005-12-01 Eckhard Langer Semiconductor structure comprising a stress sensitive element and method of measuring a stress in a semiconductor structure

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1563894A (en) * 1976-03-12 1980-04-02 Kavlico Corp Capacitive pressure transducer and method for making same
JPH0465645A (en) * 1990-07-05 1992-03-02 Toshiba Corp Pressure sensor array
JP2000258272A (en) * 1999-01-04 2000-09-22 Fuji Electric Co Ltd Capacitive pressure sensor
US6691068B1 (en) * 2000-08-22 2004-02-10 Onwafer Technologies, Inc. Methods and apparatus for obtaining data for process operation, optimization, monitoring, and control
JP2003014564A (en) * 2001-06-28 2003-01-15 Fujitsu Ten Ltd Sheet sensor and sitting person sensing system
US6770505B1 (en) * 2001-09-21 2004-08-03 Lsi Logic Corporation Arrangement for measuring pressure on a semiconductor wafer and an associated method for fabricating a semiconductor wafer
WO2003074228A1 (en) * 2002-01-17 2003-09-12 Nutool, Inc. Advanced chemical mechanical polishing system with smart endpoint detection
US6892563B2 (en) * 2002-11-26 2005-05-17 Stowe Woodward Llc Calibration apparatus and method for roll covers with embedded sensors
US7151366B2 (en) * 2002-12-03 2006-12-19 Sensarray Corporation Integrated process condition sensing wafer and data analysis system
US7135852B2 (en) * 2002-12-03 2006-11-14 Sensarray Corporation Integrated process condition sensing wafer and data analysis system
JP2005331327A (en) * 2004-05-19 2005-12-02 Alps Electric Co Ltd Contact pressure sensor and its manufacturing method
GB2430306B (en) * 2004-05-28 2009-10-21 Advanced Micro Devices Inc Semiconductor structure comprising a stress sensitive element and method of measuring a stress in a semiconductor structure
JP2006112842A (en) * 2004-10-13 2006-04-27 Alps Electric Co Ltd Surface pressure distribution sensor
JP4516445B2 (en) * 2005-02-18 2010-08-04 パナソニック株式会社 Manufacturing method of semiconductor device

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3815566A1 (en) * 1988-05-06 1989-11-16 Siemens Ag Method for determining mechanical stress conditions in electrical or electronic components to be coated, or already coated, with moulding compound
WO1990013425A1 (en) * 1989-05-08 1990-11-15 American Composite Technology Inc. System and method for monitoring pressure during the production of fiber reinforced polymers
DE4413442A1 (en) * 1994-04-18 1994-09-08 Fm Automation Elektronik Gmbh Assembly platform with a process-observing function
US6129613A (en) * 1998-01-30 2000-10-10 Philips Electronics North America Corp. Semiconductor manufacturing apparatus and method for measuring in-situ pressure across a wafer
WO2000028277A2 (en) * 1998-11-06 2000-05-18 Wisconsin Alumni Research Foundation Micromachined strain sensor
US20030022595A1 (en) * 2001-07-24 2003-01-30 Chien-Hsin Lai Wafer pressure regulation system for polishing machine
US20040023606A1 (en) * 2002-01-17 2004-02-05 Yuchun Wang Advanced chemical mechanical polishing system with smart endpoint detection
US20040098216A1 (en) * 2002-11-04 2004-05-20 Jun Ye Method and apparatus for monitoring integrated circuit fabrication
US20050239371A1 (en) * 2003-09-09 2005-10-27 Tetsuji Togawa Pressure control system and polishing apparatus
US20050263760A1 (en) * 2004-05-28 2005-12-01 Eckhard Langer Semiconductor structure comprising a stress sensitive element and method of measuring a stress in a semiconductor structure

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2010037218A1 (en) * 2008-09-30 2010-04-08 Research In Motion Limited Mobile wireless communications device having touch activated near field communications (nfc) circuit
US8351854B2 (en) 2008-09-30 2013-01-08 Research In Motion Limited Mobile wireless communications device having touch activated near field communications (NFC) circuit
KR101243574B1 (en) 2008-09-30 2013-03-20 리서치 인 모션 리미티드 Mobile wireless communications device having touch activated near field communications (nfc) circuit
US8615195B2 (en) 2008-09-30 2013-12-24 Blackberry Limited Mobile wireless communications device having touch activated near field communications (NFC) circuit
WO2010124807A1 (en) * 2009-04-29 2010-11-04 Siltronic Ag Device for gauging forces impacting a semiconductor disk
US8681493B2 (en) 2011-05-10 2014-03-25 Kla-Tencor Corporation Heat shield module for substrate-like metrology device
WO2014068269A1 (en) * 2012-10-31 2014-05-08 University Of Southampton Apparatus for sensing and measuring pressure and/or shear components of a force at an interface between two surfaces
GB2521975A (en) * 2012-10-31 2015-07-08 Univ Southampton Apparatus for sensing and measuring pressure and/or shear components of a force at an interface between two surfaces
US9700258B2 (en) 2012-10-31 2017-07-11 University Of Southampton Apparatus for sensing and measuring pressure and shear components of a force at an interface between two surfaces
GB2521975B (en) * 2012-10-31 2018-07-11 Univ Southampton Apparatus for sensing and measuring pressure and shear components of a force at an interface between two surfaces
US9836118B2 (en) 2015-06-16 2017-12-05 Wilson Steele Method and system for analyzing a movement of a person
WO2020020779A3 (en) * 2018-07-23 2020-03-12 Abb Schweiz Ag A pressure sensor for a pipe
US11566956B2 (en) 2018-07-23 2023-01-31 Abb Schweiz Ag Pressure sensor for a pipe
CN113340507A (en) * 2021-04-15 2021-09-03 安徽大学 Full-flexible three-dimensional force flexible touch sensor based on hourglass-shaped structure

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