CN100424540C - Large-bore optical periscope type radar 3-D Scanner - Google Patents
Large-bore optical periscope type radar 3-D Scanner Download PDFInfo
- Publication number
- CN100424540C CN100424540C CNB2004100646602A CN200410064660A CN100424540C CN 100424540 C CN100424540 C CN 100424540C CN B2004100646602 A CNB2004100646602 A CN B2004100646602A CN 200410064660 A CN200410064660 A CN 200410064660A CN 100424540 C CN100424540 C CN 100424540C
- Authority
- CN
- China
- Prior art keywords
- ring
- vertical
- vertical rotation
- casing
- horizontally
- Prior art date
- Legal status (The legal status 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 status listed.)
- Expired - Fee Related
Links
Images
Classifications
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02A—TECHNOLOGIES FOR ADAPTATION TO CLIMATE CHANGE
- Y02A90/00—Technologies having an indirect contribution to adaptation to climate change
- Y02A90/10—Information and communication technologies [ICT] supporting adaptation to climate change, e.g. for weather forecasting or climate simulation
Abstract
The present invention discloses a large-bore optical periscope type radar 3-D Scanner which comprises a plane reflection mirror, a horizontal rotation mechanism and a vertical rotation mechanism, wherein the plane reflection mirror is arranged on the horizontal rotation mechanism and the vertical rotation mechanism at a 45 DEG angle. The vertical rotation mechanism and the horizontal rotation mechanism are rotationally connected. The lower end of the vertical rotation mechanism is provided with a rotary disk, and both the horizontal rotation mechanism and the vertical rotation mechanism are driven through a worm wheel and worm rod driving mechanism. The present invention has the advantages of high scanning accuracy, high system stability, simple control and convenient installation, and can be butted with a reception system in a long distance.
Description
Technical field
The present invention relates to a kind of three-dimensional scanner of laser radar.
Background technology
In optical instrument, often use optical scanning, especially at atmospheric exploration, laser radar scanning, aerial camera is in laser marking or the like system.The most frequently used in the scanning system is exactly the scan mode of monolithic level crossing, as: Landsat polishing wax scanner MSS scanning mirror be exactly a major axis be 33cm, minor axis is the elliptic plane mirror of the surface coating of 23cm, its optical system with ground and back respectively becomes 45 degree, with the warble of 13.65Hz, realize scanning; The level and vertical rotation of simple reflector have been utilized, realized taking a picture at the middle 3D laser scanning and the shooting at close range of shipbuilding, scanning system is often used rotary reflection mirror drum, refracting prisms post, rotation refraction wedge, rotation V-type catoptron, biplane catoptron rotation sweep in addition.The rotation body tubes that adopt scan more in the laser radar monitoring system.
Summary of the invention
The purpose of this invention is to provide a kind of large-bore optical periscope type radar 3-D Scanner, can be widely applied in laser radar system and the scanning imaging system, especially some scanning accuracies are required than in the higher system.
A kind of large-bore optical periscope type radar 3-D Scanner, include plane mirror, horizontal rotary mechanism, with vertical rotating mechanism, it is characterized in that being equipped with on the vertical rotating box 45 degree plane mirrors, on the outer ring, side of vertical casing is installed in and encircles in the vertical rotation, the ring outer ring is fixed with turbine in the vertical rotation, be with vertical rotation outer shroud outside the ring in the vertical rotation, vertical rotation outer shroud is equipped with radial bearing between encircling with vertical rotation is interior, vertical rotation outer shroud with horizontally rotate casing and fixedly connected, horizontally rotate and be fixed with bearing on the casing, be installed with vertical revolving wormgear scroll bar gear train on the bearing, with the turbine cooperation on the ring in the vertical rotation; Horizontally rotate 45 degree plane mirrors are installed on the casing, parallel with the plane mirror of installing in the vertical rotating box, the below that horizontally rotates casing is installed with and horizontally rotates interior ring, the outer turbine that is equipped with of ring in horizontally rotating, ring is fixed on the rotating disk of hollow in horizontally rotating, and the rotating disk below is the substrate of fixing, and circumferential groove is all arranged on substrate and the rotating disk, difference fixed pan support ring has steel ball between two circumferential grooves up and down in the circumferential groove.
Described three-dimensional scanner is characterized in that described plane mirror is fixed on the microscope base, and microscope base is fixed on and horizontally rotates on casing or the vertical rotating box.
Described three-dimensional scanner is characterized in that described rotating disk below is fixedly connected on ring in the location, and the substrate below is connected with the location outer shroud, between ring and the location outer shroud radial bearing is installed in the location.
Described three-dimensional scanner is characterized in that the described casing outside that horizontally rotates is equipped with balancing weight.
Precision index of the present invention is as follows:
(1) periscopic scanning mirror:
Horizontal scanning angular region :-180 °-180 °;
Angular velocity:＞5 °/second;
Vertical scanning angular region :-5 °-95 °;
Angular velocity:＞5 °/second;
When (2) two scanning mirrors rotate, optical axis swing＜5 ';
(3) two plane mirror parallel deviation＜5 ';
(4) horizontal scanning of periscopic scanning mirror and vertical scanning have the zero degree identification device respectively.
Advantage of the present invention is as follows: 1, under the control of computing machine, utilize the turbine and worm transmission principle to realize the rotation of plane mirror, thereby make sweep test become one independently parts be widely applied in the laser radar system, avoided the rotation inconvenience that telescopic system brought.2, because itself is an independently system, thereby very big surplus has been arranged on the infield, can separate, reduced the restriction on the installing space greatly with the telescope of laser radar.3, whole scanning system has had certain guarantee by computer control on the control accuracy, has avoided manually-operated inconvenience and deficiency etc.4, scanning accuracy is very high, the good stability of system, and control is simple, convenient.Because system by mounting means independently, does not have the restriction of distance on the space of installing, can dock at a distance with receiving system, it is quite convenient to install.Adopt the control technology of computing machine, avoided manually-operated inconvenience; Owing to increased stop means in the system, thereby improved system's maintainability.
Description of drawings
Fig. 1 is a structural representation of the present invention.
Fig. 2 is a scanning theory synoptic diagram of the present invention.
Fig. 3 is the scanning space synoptic diagram of 3-D scanning of the present invention mechanism.
Fig. 4 turbine and worm gear train.
Fig. 5 is the principle schematic of increment type displacement coder.
Fig. 6 is a planar support loops composition.
Fig. 7 is plane reflection mirror-seat structure figure.
Fig. 8 is vertical rotating box cut-open view.
Fig. 9 is vertical rotating box three-dimensional structure diagram.
Figure 10 horizontally rotates the casing cut-open view.
Figure 11 horizontally rotates the casing three-dimensional structure diagram.
Figure 12 is the plane mirror structural drawing.
Embodiment
Referring to Fig. 1 ~ Figure 10.Each label among the figure: 1, plane mirror, 2, the plane reflection microscope base, 3, vertical rotating box, 4, ring in the vertical rotation, 5, vertical rotation outer shroud, 6, radial bearing, 7, horizontally rotate casing, 8, horizontal counterweight, 9, vertical counterweight, 10, Worm and worm-wheel gearing, 11, fixed pedestal, 12, the location outer shroud, 13, ring in the location, 14, radial bearing, 15, the planar support ring, 16, steel ball, 17, bearing, 18, the horizontal protective cover, 19, horizontally rotate interior ring, 20, rotating disk, 21, substrate, 22, worm screw, 23, motor, 24, the increment type displacement coder, 25, power lead, 26, control line, 27, computing machine, 28 turbines.
A kind of large-bore optical periscope type radar 3-D Scanner, plane mirror 1 is fixed on the microscope base 2, totally two groups, wherein an arrangement of mirrors seat 2 is fixed on the vertical rotating box 3 again, 1 one-tenth 45 degree of plane mirror is installed, the outer ring, side of vertical rotating box 3 is installed in to be encircled on 4 in the vertical rotation, ring 4 outer rings are fixed with turbine in the vertical rotation, be with vertical rotation outer shroud 5 outside the ring 4 in the vertical rotation, vertical rotation outer shroud 5 is equipped with radial bearing 6 between encircling 4 with vertical rotation is interior, vertical rotation outer shroud 5 with horizontally rotate casing 7 and fixedly connected, horizontally rotate and be fixed with bearing 17 on the casing, be installed with vertical revolving wormgear scroll bar gear train 10 on the bearing 17, with the turbine cooperation on the ring 4 in the vertical rotation; Another group plane mirror 1 is installed in microscope base 2 and horizontally rotates on the casing 7, plane mirror 1 also becomes 45 degree to install, parallel with the plane mirror of installing in the vertical rotating box 31, ring 19 in the below that horizontally rotates casing 7 is installed with and horizontally rotates, the ring 19 outer turbines that are equipped with in horizontally rotating, ring 29 is fixed on the rotating disk 20 of hollow in horizontally rotating, rotating disk 20 belows are fixing substrates 21 of hollow, substrate 21 all has circumferential groove with rotating disk 20, the planar support ring 15 that fixedly the Pingdu precision is very high respectively in the groove, steel ball 16 is rolling around central shaft between the planar support ring 15 up and down, plays and supports and the power effect of reducing friction.Substrate 21 is fixedly mounted on the fixed pedestal 11.
Rotating disk 20 belows are fixedly connected on ring 13 in the location, and substrate 21 belows are connected with location outer shroud 12, between ring 13 and the location outer shroud 12 radial bearing 14 are installed in the location.
Shown in Figure 1 is the optical-mechanical system diagrammatic cross-section of the periscopic scanning of clear aperture Φ 300mm.The present invention has adopted the biplane mirror structure of periscopic on optical system, two plane mirrors become the parallel placement of 45 degree with chief ray, and catoptron has plated highly reflecting films according to the operating position of reality.Because catoptron 45 degree are placed, the clear aperature on the catoptron is oval; In clear aperture Φ 300mm scanning system, the actual bore of catoptron is major axis a=424mm, and the ellipse of minor axis c=300mm is considered processing and clamping, and two actual plane mirrors are made octagon.Periscopic laser radar three bit scans rotate principle as shown in Figure 2, and its rotary system horizontally rotates and vertical rotation constitutes, when horizontally rotating, and two whole rotations of catoptron; During vertical the rotation, have only the catoptron of vertical sense of rotation to rotate, its scanning space synoptic diagram as shown in Figure 3.
1. the realization of vertical rotation
As can be seen from Figure 1, plane mirror 1 adopts suspension type to be fixed on the microscope base 2, microscope base 2 changes casing 3 by screw and heavy direct rotary and connects as one, and casing positions with the interior ring of vertical rotation 4 usefulness register pins and is connected, and has improved bearing accuracy and stability of rotation.Ring 4 is connected with worm gear in the vertical rotation, and the oscillating quantity of optical axis has been installed two major diameter radial bearings 6 between interior ring 4 and outer shroud 5 when controlling rotation; Vertical rotating part by outer shroud 5 with horizontally rotate casing 7 and be connected.Like this, when motor-driven turbine and worm gear train 10, vertical rotating box and on plane mirror realize vertical rotation.And outer shroud 5 and casing 7 can keep stationary state.
2. the realization that horizontally rotates
Horizontally rotate factors such as the installation that needs taking into account system and weight thereof, so it is comparatively complicated to horizontally rotate structure.What horizontally rotate transfers from one department to another as shown in Figure 1, the plane mirror 1 same suspension type that adopts is fixed on the microscope base 2, microscope base 2 is fixed on the casing 7, whole rotatable parts finally are connected with ring 13 in the rotation, be two major diameter radial bearings 14 between ring 13 and the rotation outer shroud 12 in the rotation, bear the weight of total system.Drive by turbine and worm gear train 10 has realized horizontally rotating of whole rotating system, in order to reduce friction and optical axis rolling momentum, adopted steel ball 16 to support, and steel ball 16 is rolled on the support ring 15 of two high flatnesses, be used to bear the gravity of whole scanning mechanism, avoided radial bearing to bear excessive axial force.
In fact the design of steel ball is exactly to calculate the required minimum diameter of steel ball, and its formula is:
The load intensity allowable of C in the formula---steel ball material is about 780～980N/cm
2
Q
k---assumed (specified) load, its computing formula is
Q
k＝Q
0·a
1·a
2·a
3 (2)
A wherein
1---consider the coefficient that seat ring rotates, get 1.4 herein;
a
2---consider the coefficient of load condition, get 1.8 herein;
a
3---consider the coefficient of working time, get 2 herein;
Q
0---when bearing axial load, the peak load that steel ball is subjected to, computing formula is
Wherein Q---axial gross load is about Q=210kg according to all load;
The steel ball number of z---use, the steel ball number that native system uses is 60;
α---steel ball is subjected to the angle of force direction and axis, and α is zero in the native system.
With the data substitution, can obtain:
Q
k＝Q
0·a
1·a
2·a
3＝4.79×1.4×1.8×2＝24.15kg＝236.7N；
So using diameter in the native system is enough as the steel ball intensity of 10mm.
3. turbine and worm gear train
The turbine and worm gear train as shown in Figure 4, turbine 28 and worm screw 22 are driven by motor 23, the motor back connects increment type displacement coder 24, motor links to each other with control system and computing machine 27 with control line 26 by power lead 25 with scrambler.Stepper motor is a kind of topworks that electric pulse is converted into angular displacement.When step actuator receives a pulse signal, it rotates a fixing angle (being step angle) with regard to drive stepping motor by the direction of setting.Can come the pilot angle displacement by the gating pulse number, thereby reach the purpose of accurate location, can control speed and the acceleration that motor rotates by the gating pulse frequency simultaneously, thereby reach the purpose of speed governing.The stepper motor that the present invention selects for use is a two-phase hybrid, and step angle is 1.8 ° (through being 0.36 ° after the driver segmentation).Because the moment of inertia of scanning mechanism is very big, stepper motor might be to the also response fully of a gating pulse when starting to walk and stopping, and another pulse has arrived, and this step-out phenomenon will influence control accuracy greatly.The way that solves is exactly to add zero-bit angle identification device and increment type displacement coder 24 in system.The increment type displacement coder is a kind of pulse disc type digital sensor of angle.Its principle schematic as shown in Figure 5.On the edge of disk, be carved with the radial slit (being divided into printing opacity and lightproof part) that equates angular distance.Both sides at the disk that cracks are installed light source and light activated element respectively.When disk rotated with working shaft, revolution was crossed the variation that a bright and dark light just takes place in a slit.Produce the variation of an electric signal by light activated element.Amplify through shaping again, get final product the electric pulse output signal of certain amplitude and power.The slit number that umber of pulse equals to turn over.The pulse signal of output is delivered to and gone in the counter to count, then just can obtain the disc rotation value by the count value that obtains.
The stepper motor two ends are furnished with projecting shaft, a termination worm screw, and another termination displacement coder is used for monitoring the corner of axle.The least error of this method of counting is the angular resolution of displacement coder, the angle that pulse rotating shaft of promptly every generation is turned over.Therefore method of counting can be expressed from the next to the influence of control accuracy:
Δ θ in the formula
2---the angular resolution of displacement coder to the influence of control accuracy (°);
The umber of pulse that N---grating in the displacement coder spirals and circles and produce;
I---overall ratio.
The groove of grating dish is general closeer, so the N value is very big, and through 1/168 segmentation, so adopted after the displacement coder, the angle gauge counting method is also just very little to the influence of control accuracy again.Utilize computer programming to realize increment type displacement coder and motor rotational synchronization, under the strictness control of photoswitc and travel switch, realized that scanning mechanism carries out three-dimensional scanning by given angle.
For being calculated as follows of turbine and worm in the scanning mechanism of Φ 300mm bore:
(1) number of threads Z
1, the worm gear tooth number Z
2And the calculating of ratio of gear i:
According to actual optics and mechanical dimension, determined the physical dimension of worm and gear, roughly as follows:
Worm gear: external diameter Φ 430mm, internal diameter Φ 336mm, thickness 35mm;
Worm screw: diameter of phi 35mm
Delivery is counted m=2,5, and the reference circle of wormwheel diameter is d2=420mm, and then the worm gear number of teeth is:
Z
2＝d
2/m＝420/2.5＝168
Because the ratio of gear in this example is bigger, can get number of threads Z1=1, ratio of gear is: i=Z
2/ Z
1=168
So can determine: number of threads Z
1=1, the worm gear tooth number Z
2=168, ratio of gear i=168.
(2) select material and definite its permissible stress:
The material of worm gear pair not only requires enough intensity, and the more important thing is to have good properties of antifriction and wear resistance, therefore adopts ZQSn10-1 to make the material of worm gear, and its anti-bonding and anti-wear performance is good, the sliding speed height of permission, and be easy to cut; The material that worm screw is selected for use is 40Cr, and surface hardening has very high hardness to HRC40～45.
When estimating operate as normal the relative sliding velocity of worm gear and worm screw be no more than 0,5m/s, the allowable contact stress of worm gear is [σ
H]=180N/mm
2
(3) calculating of modulus m, diameter quotient q and physical dimension:
Got m=2,5 in the first step, getting reference diameter of worm is d1=30mm, and then diameter quotient is q=d
1/ m=30/2.5=12
The computing formula of other physical dimensions and the results are shown in Table 1
4, the design of balancing weight
For system is operated steadily, also respectively level has been carried out counterbalance design with vertical rotating mechanism.This part content is finished by PRO/E software.Under Assembly (assembling) pattern, earlier the roughly modelling of scanning mechanism is come out, import the density value of part then according to the material of each part, can carry out the analysis of qualitative attribute whole model.
Counterweight is carried out in two sub-sections.At first will carry out counterweight to vertical rotating mechanism, then to the horizontal rotary mechanism counterweight, two process approachs are the same, only introduce the counterweight process of horizontal rotary mechanism here.
Because the horizontal rotary mechanism running time drives vertical rotating mechanism and rotates together, to analyze together so will add vertical rotating mechanism during to the horizontal rotary mechanism counterweight, this also is must the first reason that carry out counterweight to vertical mechanism.
The general assembly (TW) of system is about the G=173 kilogram before the counterweight.This is the key parameter that counterweight will be used.For reducing the side-play amount of center of gravity, need add balancing weight in the opposite direction with respect to horizontal rotating shaft.Should use the bigger and cheap material of density, as cast iron etc.During design balancing weight is installed in from rotating shaft position far away slightly, like this can be under the situation that obtains same counterweight effect the general assembly (TW) of mitigation system.Needn't accurately calculate to add how much weight when adding balancing weight, can after adding certain counterweight, carry out the qualitative attribute analysis at once, analyze once more if be unsatisfied with the volume (weight) that can change counterweight easily, till satisfaction.
The weight that goes out counterweight 8 and 9 according to the PRO/E computed in software is 37 kilograms, adds gross weight and be 20 kilograms substrate 11 and protective cover 18, and the 3 D scanning system general assembly (TW) is about 230 kilograms.
Claims (4)
1. large-bore optical periscope type radar 3-D Scanner, include plane mirror, horizontally rotate casing, with vertical rotating box, it is characterized in that being equipped with on the vertical rotating box 45 degree plane mirrors, on the outer ring, side of vertical rotating box is installed in and encircles in the vertical rotation, the ring outer ring is fixed with turbine in the vertical rotation, be with vertical rotation outer shroud outside the ring in the vertical rotation, vertical rotation outer shroud is equipped with radial bearing between encircling with vertical rotation is interior, vertical rotation outer shroud with horizontally rotate casing and fixedly connected, horizontally rotate and be fixed with bearing on the casing, be installed with vertical revolving wormgear scroll bar gear train on the bearing, with the turbine cooperation on the ring in the vertical rotation; Horizontally rotate 45 degree plane mirrors are installed on the casing, parallel with the plane mirror of installing in the vertical rotating box, the below that horizontally rotates casing is installed with and horizontally rotates interior ring, the outer turbine that is equipped with of ring in horizontally rotating, ring is fixed on the rotating disk of hollow in horizontally rotating, and the rotating disk below is the substrate of fixing, and circumferential groove is all arranged on substrate and the rotating disk, difference fixed pan support ring has steel ball between two circumferential grooves up and down in the circumferential groove.
2. device according to claim 1 is characterized in that described plane mirror is fixed on the microscope base, and microscope base is fixed on and horizontally rotates on casing and the vertical rotating box.
3. device according to claim 1 is characterized in that described rotating disk below is fixedly connected on ring in the location, and the substrate below is connected with the location outer shroud, between ring and the location outer shroud radial bearing is installed in the location.
4. device according to claim 1 is characterized in that the described casing outside that horizontally rotates is equipped with balancing weight.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100646602A CN100424540C (en) | 2004-09-14 | 2004-09-14 | Large-bore optical periscope type radar 3-D Scanner |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNB2004100646602A CN100424540C (en) | 2004-09-14 | 2004-09-14 | Large-bore optical periscope type radar 3-D Scanner |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN1601324A CN1601324A (en) | 2005-03-30 |
| CN100424540C true CN100424540C (en) | 2008-10-08 |
Family
ID=34666413
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNB2004100646602A Expired - Fee Related CN100424540C (en) | 2004-09-14 | 2004-09-14 | Large-bore optical periscope type radar 3-D Scanner |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN100424540C (en) |
Families Citing this family (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN100487433C (en) * | 2005-06-07 | 2009-05-13 | 中国科学院安徽光学精密机械研究所 | Vehicular pollution-motoring lidar device based on Raman light source |
| CN1936617B (en) * | 2006-10-12 | 2010-04-21 | 中国地震局地震研究所 | Comprehensive low-noise constant-temperature laser receiving system |
| CN1952687B (en) * | 2006-11-02 | 2010-12-01 | 中国科学院安徽光学精密机械研究所 | Automatic collimating method and collimator set for light path of colidar |
| CN101576620B (en) * | 2009-06-08 | 2011-06-15 | 北京理工大学 | Large-caliber optical periscopic non-coaxial laser radar three-dimensional scanning device |
| CN101614861B (en) * | 2009-08-12 | 2013-01-02 | 中国航空工业第一集团公司北京长城计量测试技术研究所 | Fixing support body for fixing reflector in injection-molded mirror canal |
| CN101697037B (en) * | 2009-09-29 | 2011-08-24 | 陈自明 | Stereoscopic mirror |
| CN102063125A (en) * | 2009-11-17 | 2011-05-18 | 陈继文 | Automatic tracing, aiming and positioning device |
| CN101900806B (en) * | 2010-05-18 | 2013-03-27 | 北京航空航天大学 | Method and device for real-time compensation of roll angle deviation of airborne laser radar |
| CN106600966B (en) * | 2016-11-17 | 2019-07-16 | 武汉万集信息技术有限公司 | A kind of vehicle axles identifying system and method based on laser radar |
| CN107643516A (en) * | 2017-09-27 | 2018-01-30 | 北京因泰立科技有限公司 | A kind of 3-D scanning laser radar based on MEMS micromirror |
| CN108693088B (en) * | 2018-05-17 | 2021-07-13 | 吉林省洪科光电技术有限公司 | Atmospheric particulate monitoring scanning polarization laser radar system |
| CN111587382A (en) * | 2018-12-18 | 2020-08-25 | 深圳市大疆创新科技有限公司 | Laser measuring device and unmanned vehicles |
| JP2021524015A (en) * | 2019-04-23 | 2021-09-09 | ハンズ レーザー テクノロジー インダストリー グループ カンパニー リミテッド | Lattice disk and feedback system |
| CN110031863A (en) * | 2019-05-21 | 2019-07-19 | 安徽蓝科信息科技有限公司 | A kind of scanning means based on two wavelength aerosol radars |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5268554A (en) * | 1992-06-29 | 1993-12-07 | General Electric Co. | Apparatus and system for positioning a laser beam |
| US5546214A (en) * | 1995-09-13 | 1996-08-13 | Reliant Technologies, Inc. | Method and apparatus for treating a surface with a scanning laser beam having an improved intensity cross-section |
| CN1205453A (en) * | 1998-06-08 | 1999-01-20 | 北京大学 | Three-dimensional laser scanner |
| CN1240970A (en) * | 1998-07-02 | 2000-01-12 | 全友电脑股份有限公司 | Optical path changer for multi-lens scanner |
| CN2481095Y (en) * | 2001-05-26 | 2002-03-06 | 陈业明 | Optical signal vertical horizontal deflection controller |
-
2004
- 2004-09-14 CN CNB2004100646602A patent/CN100424540C/en not_active Expired - Fee Related
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5268554A (en) * | 1992-06-29 | 1993-12-07 | General Electric Co. | Apparatus and system for positioning a laser beam |
| US5546214A (en) * | 1995-09-13 | 1996-08-13 | Reliant Technologies, Inc. | Method and apparatus for treating a surface with a scanning laser beam having an improved intensity cross-section |
| CN1205453A (en) * | 1998-06-08 | 1999-01-20 | 北京大学 | Three-dimensional laser scanner |
| CN1240970A (en) * | 1998-07-02 | 2000-01-12 | 全友电脑股份有限公司 | Optical path changer for multi-lens scanner |
| CN2481095Y (en) * | 2001-05-26 | 2002-03-06 | 陈业明 | Optical signal vertical horizontal deflection controller |
Non-Patent Citations (1)
| Title |
|---|
| 一种改进激光雷达性能的方法. 仲思东等.仪器仪表学报，第25卷第4期. 2004 * |
Also Published As
| Publication number | Publication date |
|---|---|
| CN1601324A (en) | 2005-03-30 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN100424540C (en) | Large-bore optical periscope type radar 3-D Scanner | |
| CN201016713Y (en) | Optical centering instrument with air bearing rotating platform | |
| CN100410625C (en) | Shedding profilogram measuring apparatus | |
| CN102338165B (en) | Reflection type control method for monitoring angular displacement of turnable bearing | |
| CN108681024A (en) | A kind of moving-target face focus adjusting mechanism and its target surface tilt quantity and optical axis glitch detection method | |
| CN107101712A (en) | Multi-direction wide-angle based on single-point laser vialog continuously scans vibration measuring auxiliary machine | |
| CN109186502B (en) | Full-circumference high-precision positioning rotary worktable based on photoelectric autocollimator and method | |
| CN109724636A (en) | One-dimensional turntable | |
| KR100723757B1 (en) | apparatus and method for measuring roundness | |
| US4646566A (en) | Apparatus for testing gear wheel tooth flank profile and tooth flank lines (toot angle) and a method for positioning this apparatus for the measurement apparatus | |
| CN113324514B (en) | Rotating shaft debugging method and debugging assembly | |
| CN102352889B (en) | Control method for improving angular-displacement accuracy of rotary-table bearing | |
| US5031443A (en) | Apparatus for measuring bearing torque | |
| CN102672537A (en) | Precise shafting circular grating optical indexing method | |
| CN112729172A (en) | Encoder code wheel eccentricity detection device and eccentricity adjustment method | |
| CN208270833U (en) | A kind of moving-target face focus adjusting mechanism | |
| CN113847878A (en) | Surface difference measuring equipment and surface difference measuring method for excavator appearance piece | |
| JP3444800B2 (en) | Tilt stage | |
| McIlraith et al. | A radial grating dividing engine of high accuracy | |
| CN112698206A (en) | Rotating motor eccentric fault simulation mechanism and method | |
| Korhonen et al. | Polishing and testing of the 3.5 m SiC M1 mirror of the Herschel space observatory of ESA | |
| US20230375438A1 (en) | Dual-dial measurement device and measurement method for viewing angle measurement of optical component | |
| JP4072265B2 (en) | Rotation axis tilt measurement method | |
| JPS63128219A (en) | Aspherical shape measuring machine | |
| CN213041502U (en) | Bevel gear detection device |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20081008 Termination date: 20091014 |