CN104155654A - Airborne radar - Google Patents
Airborne radar Download PDFInfo
- Publication number
- CN104155654A CN104155654A CN201410396130.1A CN201410396130A CN104155654A CN 104155654 A CN104155654 A CN 104155654A CN 201410396130 A CN201410396130 A CN 201410396130A CN 104155654 A CN104155654 A CN 104155654A
- Authority
- CN
- China
- Prior art keywords
- unit
- alarm
- processor
- display
- information
- 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.)
- Withdrawn
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Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S13/00—Systems using the reflection or reradiation of radio waves, e.g. radar systems; Analogous systems using reflection or reradiation of waves whose nature or wavelength is irrelevant or unspecified
- G01S13/88—Radar or analogous systems specially adapted for specific applications
- G01S13/93—Radar or analogous systems specially adapted for specific applications for anti-collision purposes
- G01S13/933—Radar or analogous systems specially adapted for specific applications for anti-collision purposes of aircraft or spacecraft
Landscapes
- Engineering & Computer Science (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Electromagnetism (AREA)
- Computer Networks & Wireless Communication (AREA)
- General Physics & Mathematics (AREA)
- Alarm Systems (AREA)
Abstract
An airborne radar disclosed by the present invention comprises a sending unit, a processor and a receiving unit. An object position determining unit is connected between the receiving unit and the processor, and is used to detect the position of a target. The processor is connected with an alarm unit and is also connected with a pressure sensor and a temperature sensor, and the pressure and temperature signals are transmitted to a display screen via the processor, at the same time, are transmitted to a satellite or a ground radar via a sending unit. The alarm unit comprises a display alarm sub-unit and a sound alarm sub-unit, the display alarm sub-unit is used to send the display information of an alarm, and the sound alarm sub-unit is used to send the sound information of the alarm. According to the technical scheme, the alarm unit comprises the display alarm sub-unit and the sound alarm sub-unit, so that the form is diverse, and the users are convenient to receive the information via multiple paths rapidly and process the information timely. The signals which are processed by the processor and are transmitted by the pressure sensor and the temperature sensor can be known via the display screen, thereby improving the safety performance.
Description
Technical field
The present invention relates to communication technical field, relate in particular to a kind of airborne radar.
Background technology
In the apparatus field of the radar of present generation aircraft, the back unit that known use is decided to be on airframe and extends along the longitudinal direction of aircraft.Back unit comprises along a plurality of sideward-looking antenna elements of the longitudinal direction location of back unit, for side-looking purposes.Airborne radar under prior art cannot be recognized the ambiguous barriers of aircraft periphery and the speed of a ship or plane of flying object and distance accurately, and warning device is also more single, and information can not be transmitted in time efficiently, and safety coefficient is lower.
Summary of the invention
For the deficiencies in the prior art, the invention provides a kind of airborne radar.
To achieve these goals, the technical solution used in the present invention is:
A kind of airborne radar, comprise transmitting element, processor and receiving element, between receiving element and processor, be connected with object's position determining unit, for detection of the position to described target, processor is connected with alarm unit, and alarm unit is according to the distance of the periphery barrier of calculating place of described computing unit and rapidly remind, and processor is connected with pressure transducer and temperature sensor, through processor, display screen be will be transported to, by transmitting element, satellite or ground radar passed to simultaneously.
Described alarm unit comprises display alarm subelement and audible alarm subelement, described display alarm subelement is for sending the demonstration information of warning, described audible alarm subelement is for sending the acoustic information of warning, alarm unit can be more comprehensive, be conducive to the situation that people grasp aircraft in time, improved security performance.
Described display screen adopts the true color screen of TFT, is conducive to watching of people.
Beneficial effect of the present invention: the present invention processes by processor with respect to prior art, then exports, and has facilitated people's use; Alarm unit comprises display alarm subelement and audible alarm subelement, various informative, and person easy to use can be quick, and the multipath information that receives, deals with in time; By display screen, can recognize that the pressure and temperature sensor that inner treated device was processed passes the signal of coming, and has improved security performance.
Accompanying drawing explanation
Fig. 1 is schematic diagram of the present invention.
Embodiment
As shown in Figure 1, a kind of airborne radar, comprise transmitting element, processor and receiving element, between receiving element and processor, be connected with object's position determining unit, for detection of the position to described target, processor is connected with alarm unit, alarm unit is according to the distance of the periphery barrier of calculating place of described computing unit and rapidly remind, processor is connected with pressure transducer and temperature sensor, through processor, will be transported to display screen, by transmitting element, pass to satellite or ground radar simultaneously, described alarm unit comprises display alarm subelement and audible alarm subelement, described display alarm subelement is for sending the demonstration information of warning, described audible alarm subelement is for sending the acoustic information of warning, alarm unit can be more comprehensive, be conducive to the situation that people grasp aircraft in time, improved security performance, described display screen adopts the true color screen of TFT, be conducive to watching of people.
Beneficial effect of the present invention: the present invention processes by processor with respect to prior art, then exports, and has facilitated people's use; Alarm unit comprises display alarm subelement and audible alarm subelement, various informative, and person easy to use can be quick, and the multipath information that receives, deals with in time; By display screen, can recognize that the pressure and temperature sensor that inner treated device was processed passes the signal of coming, and has improved security performance.
Claims (3)
1. an airborne radar, comprise transmitting element, processor and receiving element, it is characterized in that, between receiving element and processor, be connected with object's position determining unit, for detection of the position to described target, processor is connected with alarm unit, alarm unit is according to the distance of the periphery barrier of calculating place of described computing unit and rapidly remind, processor is connected with pressure transducer and temperature sensor, through processor, display screen be will be transported to, by transmitting element, satellite or ground radar passed to simultaneously.
2. airborne radar as claimed in claim 1, it is characterized in that, described alarm unit comprises display alarm subelement and audible alarm subelement, and described display alarm subelement is for sending the demonstration information of warning, and described audible alarm subelement is for sending the acoustic information of warning.
3. airborne radar as claimed in claim 1, is characterized in that, described display screen adopts the true color screen of TFT.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410396130.1A CN104155654A (en) | 2014-08-13 | 2014-08-13 | Airborne radar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410396130.1A CN104155654A (en) | 2014-08-13 | 2014-08-13 | Airborne radar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104155654A true CN104155654A (en) | 2014-11-19 |
Family
ID=51881204
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410396130.1A Withdrawn CN104155654A (en) | 2014-08-13 | 2014-08-13 | Airborne radar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104155654A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5223285A (en) * | 1975-08-15 | 1977-02-22 | Toyo Commun Equip Co Ltd | Range measuring system for aircraft collision prevention |
| US20050024256A1 (en) * | 2003-07-29 | 2005-02-03 | Navaero Ab | Passive Airborne Collision Warning Device and Method |
| US20070252760A1 (en) * | 1999-03-05 | 2007-11-01 | Smith Alexander E | Method and apparatus for ADS-B validation, active and passive multilateration, and elliptical surviellance |
| US20080055149A1 (en) * | 2004-11-03 | 2008-03-06 | Flight Safety Technologies, Inc. | Ground-based collision alerting and avoidance system |
| CN101584083A (en) * | 2006-12-18 | 2009-11-18 | 艾利森电话股份有限公司 | Fore/aft looking airborne radar |
| CN102627149A (en) * | 2011-02-04 | 2012-08-08 | 霍尼韦尔国际公司 | Passive bird-strike avoidance systems and methods |
| CN102679951A (en) * | 2011-03-11 | 2012-09-19 | 尤洛考普特公司 | Method for measuring height and detecting obstacles, radio altimeter and aircraft |
| US8570211B1 (en) * | 2009-01-22 | 2013-10-29 | Gregory Hubert Piesinger | Aircraft bird strike avoidance method and apparatus |
-
2014
- 2014-08-13 CN CN201410396130.1A patent/CN104155654A/en not_active Withdrawn
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS5223285A (en) * | 1975-08-15 | 1977-02-22 | Toyo Commun Equip Co Ltd | Range measuring system for aircraft collision prevention |
| US20070252760A1 (en) * | 1999-03-05 | 2007-11-01 | Smith Alexander E | Method and apparatus for ADS-B validation, active and passive multilateration, and elliptical surviellance |
| US20050024256A1 (en) * | 2003-07-29 | 2005-02-03 | Navaero Ab | Passive Airborne Collision Warning Device and Method |
| US20080055149A1 (en) * | 2004-11-03 | 2008-03-06 | Flight Safety Technologies, Inc. | Ground-based collision alerting and avoidance system |
| CN101584083A (en) * | 2006-12-18 | 2009-11-18 | 艾利森电话股份有限公司 | Fore/aft looking airborne radar |
| US8570211B1 (en) * | 2009-01-22 | 2013-10-29 | Gregory Hubert Piesinger | Aircraft bird strike avoidance method and apparatus |
| CN102627149A (en) * | 2011-02-04 | 2012-08-08 | 霍尼韦尔国际公司 | Passive bird-strike avoidance systems and methods |
| CN102679951A (en) * | 2011-03-11 | 2012-09-19 | 尤洛考普特公司 | Method for measuring height and detecting obstacles, radio altimeter and aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| WW01 | Invention patent application withdrawn after publication | ||
| WW01 | Invention patent application withdrawn after publication |
Application publication date: 20141119 |