CN203930072U - A kind of device for searching for the unmanned plane that falls - Google Patents
A kind of device for searching for the unmanned plane that falls Download PDFInfo
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- CN203930072U CN203930072U CN201420357181.9U CN201420357181U CN203930072U CN 203930072 U CN203930072 U CN 203930072U CN 201420357181 U CN201420357181 U CN 201420357181U CN 203930072 U CN203930072 U CN 203930072U
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Abstract
The utility model relates to device for searching, a kind of device for searching for the unmanned plane that falls is disclosed, comprise the primary module that is fixedly located on unmanned plane and from module, also comprise the mobile earth station that ground reseaching staff carries, primary module comprises remote-wireless communication module, satellite positioning module and near radio transceiver module, from module, comprise higher source luminance, high-decibel generator, near radio transceiver module and wireless location beacon, mobile earth station is provided with remote-wireless communication module.The utility model provides a kind of device for searching for the unmanned plane that falls, adopt wireless communication module and satellite positioning module on unmanned plane and mobile earth station, location, light, the sound one prompting search personnel unmanned plane position of falling via satellite, make search personnel can search out in time the unmanned plane that falls, and unmanned plane diverse location place arranges wireless communication module and satellite positioning module, effectively reduced the incidence that wireless telecommunications are broken down.
Description
Technical field
The utility model relates to device for searching, relates in particular to a kind of device for searching for the unmanned plane that falls.
Background technology
Unmanned plane, in flight course, due to the impact of various uncertain factors, is difficult to avoid falling accident can occur.Once after unmanned plane falls, if cannot give in time unmanned plane for change, probably cause the loss of data, equipment.Therefore, after unmanned plane generation falling accident, how locating fast the position of falling, how to allow search personnel find the most most effectively the unmanned plane falling, is a problem in the urgent need to address.
At present, unmanned plane is generally all with global position system, and in trouble-proof situation, this system can be stood earthward and be sent the position of unmanned plane by wireless station.If there is unmanned plane, fall, if this system can also be worked and wireless station can also keep being connected with land station, search personnel and can search according to this signal; If this system breaks down and unavailable, effective satellite positioning information that search personnel can finally beam back according to aircraft dwindles search area.
But the global position system of existing this dependence unmanned plane self-driving has very large risk, after unmanned plane falls, various device on the unmanned plane possibility that particularly electronic equipment breaks down is quite high, cannot guarantee that positioning system normally works, make to be difficult to look for unmanned plane in time and incur loss through delay follow-up work.
Summary of the invention
The utility model easily causes after falling for unmanned plane in prior art that global position system breaks down, power-fail and cause being difficult to look in time the shortcoming of unmanned plane, the device for searching for the unmanned plane that falls that provides a kind of satellite positioning module of the global position system that is independent of unmanned plane self-driving and wireless communication module, collection satnav, light, sound one prompting search personnel to fall position.
In order to solve the problems of the technologies described above, the utility model is solved by following technical proposals:
A kind of device for searching for the unmanned plane that falls, comprise the primary module that is fixedly located on unmanned plane and from module, also comprise the mobile earth station that ground reseaching staff carries, primary module comprises remote-wireless communication module, satellite positioning module and near radio transceiver module, from module, comprise higher source luminance, high-decibel generator, near radio transceiver module and wireless location beacon, mobile earth station is provided with remote-wireless communication module.
By remote-wireless communication module, primary module and mobile earth station carry out radio communication, by satellite positioning module, locating information are sent to mobile earth station, and the search personnel of guiding mobile earth station carry out search work.The search personnel of mobile earth station can send instructions to primary module by remote-wireless communication module, primary module again by near radio transceiver module with from module, carry out radio communication, thereby the luminous and sounding of controlling higher source luminance and high-decibel generator, makes search personnel to locate rapidly and to find the unmanned plane falling by passage of scintillation light and sound.
Primary module transmits a signal to from module by Fixed Time Interval, identifies the integrity of self.From module, in Fixed Time Interval, receive signal, higher source luminance, high-decibel generator, wireless location beacon, all in silent status, are saved electric quantity of lithium battery.
As preferably, unmanned plane comprises head, the fuselage being connected with head, the wing being connected with fuselage, the tail being connected with fuselage and the empennage being connected with tail, and wing comprises the wing tip in outside; Primary module is fixedly located in the case body of tail, is fixedly located in the case body of head and/or wing tip and/or tail and/or empennage from module.Primary module need be placed on the safe location of unmanned plane, because unmanned plane falls in process, because tail is comparatively safe position, therefore primary module is installed in tail case body by vibroshock.Head, wing tip, tail, empennage diverse location place at unmanned plane install from module, damage allly from module while avoiding unmanned plane to fall, and can guarantee to greatest extent that light, sound are not blocked.
As preferably, primary module and be equipped with the lithium battery that power supply is provided from module.
As preferably, mobile earth station is provided with location direction-finder antenna.
The utility model is owing to having adopted above technical scheme, there is significant technique effect: adopt wireless communication module and satellite positioning module on unmanned plane and mobile earth station, location, light, the sound one prompting search personnel unmanned plane position of falling via satellite, make search personnel can search out in time the unmanned plane that falls, and unmanned plane diverse location place arranges wireless communication module and satellite positioning module, effectively reduced the incidence that wireless telecommunications are broken down.
Accompanying drawing explanation
Fig. 1 is the control principle block diagram of the utility model device for searching embodiment.
Fig. 2 is the utility model primary module and is installed in the structural representation of embodiment unmanned plane from module.
The toponym that in accompanying drawing, each number designation refers to is as follows: 1-unmanned plane, 2-primary module, 3-and from module, 4-mobile earth station, 5-lithium battery, 11-head, 12-fuselage, 13-wing, 14-tail, 15-empennage, 21-remote-wireless communication module, 22-satellite positioning module, 23-near radio transceiver module, 31-higher source luminance, 32-high-decibel generator, 33-wireless location beacon, 40-location direction-finder antenna, 130-wing tip.
Embodiment
Below in conjunction with accompanying drawing and embodiment, the utility model is described in further detail.
Embodiment 1
A kind of device for searching for the unmanned plane that falls, as shown in Figure 1-2, comprise the primary module 2 that is fixedly located on unmanned plane 1 and from module 3, also comprise the mobile earth station 4 that ground reseaching staff carries, primary module 2 comprises remote-wireless communication module 21, satellite positioning module 22 and near radio transceiver module 23, from module 3, comprise higher source luminance 31, high-decibel generator 32, near radio transceiver module 23 and wireless location beacon 33, mobile earth station 4 is provided with remote-wireless communication module 21, primary module 2 and be equipped with the lithium battery of power supply 5 is provided from module 3, unmanned plane 1 comprises head 11, the fuselage 12 being connected with head 11, the wing 13 being connected with fuselage 12, the tail 14 being connected with fuselage 12 and the empennage 15 being connected with tail 14, and wing 13 comprises the wing tip 130 in outside, primary module 2 is fixedly located in the case body of tail 14, is fixedly located in the case body of head 11, wing tip 130, tail 14 and empennage 15 from module 3.
By remote-wireless communication module 21, primary module 2 carries out radio communication with mobile earth station 4, by satellite positioning module 22, the positional information of the unmanned plane falling 1 is sent to mobile earth station 4, and the search personnel of guiding mobile earth station 4 carry out search work.The search personnel of mobile earth station 4 can send instructions to primary module 2 by remote-wireless communication module 21, primary module 2 again by near radio transceiver module 23 with from module 3, carry out radio communication, thereby the luminous and sounding of controlling higher source luminance 31 and high-decibel generator 32, makes search personnel to locate rapidly and to find the unmanned plane 1 falling by passage of scintillation light and sound.
Primary module 2 transmits a signal to from module 3 by Fixed Time Interval, identifies the integrity of self.From module 3, receive signal in Fixed Time Interval, higher source luminance 31, high-decibel generator 32, wireless location beacon 33, all in silent status, are saved lithium battery 5 electric weight.If primary module 2 breaks down and cannot normally work after unmanned plane 1 falls, from higher source luminance 31 high-decibel generators 32 and wireless location beacon 33 automatically startings of module 3, and send wireless signals to mobile earth station 4.Mobile earth station 4 receives by location direction-finder antenna 40 wireless signal that wireless location beacon 33 sends.
Primary module 2 need be placed on the safe location of unmanned plane 1, because unmanned plane 1 falls in process, because tail 14 is comparatively safe positions, therefore primary module 2 is installed in tail 14 case bodies by vibroshock.Head 11, wing tip 130, tail 14, empennage 15 diverse location places at unmanned plane 1 install from module 3, damage allly from module 3 while avoiding unmanned plane 1 to fall, and can guarantee to greatest extent that light, sound are not blocked.
In a word, the foregoing is only preferred embodiment of the present utility model, all equalizations of doing according to the utility model claim change and modify, and all should belong to the covering scope of the utility model patent.
Claims (4)
1. the device for searching for the unmanned plane that falls, it is characterized in that: comprise the primary module (2) that is fixedly located on unmanned plane (1) and from module (3), also comprise the mobile earth station (4) that ground reseaching staff carries, primary module (2) comprises remote-wireless communication module (21), satellite positioning module (22) and near radio transceiver module (23), from module (3), comprise higher source luminance (31), high-decibel generator (32), near radio transceiver module (23) and wireless location beacon (33), mobile earth station (4) is provided with remote-wireless communication module (21).
2. a kind of device for searching for the unmanned plane that falls according to claim 1, it is characterized in that: unmanned plane (1) comprises head (11), the fuselage (12) being connected with head (11), the wing (13) being connected with fuselage (12), the tail (14) being connected with fuselage (12) and the empennage (15) being connected with tail (14), wing (13) comprises the wing tip (130) in outside; Primary module (2) is fixedly located in the case body of tail (14), is fixedly located in the case body of head (11) and/or wing tip (130) and/or tail (14) and/or empennage (15) from module (3).
3. a kind of device for searching for the unmanned plane that falls according to claim 1 and 2, is characterized in that: primary module (2) and be equipped with the lithium battery of power supply (5) is provided from module (3).
4. a kind of device for searching for the unmanned plane that falls according to claim 1, is characterized in that: mobile earth station (4) is provided with location direction-finder antenna (40).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420357181.9U CN203930072U (en) | 2014-06-30 | 2014-06-30 | A kind of device for searching for the unmanned plane that falls |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420357181.9U CN203930072U (en) | 2014-06-30 | 2014-06-30 | A kind of device for searching for the unmanned plane that falls |
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| CN203930072U true CN203930072U (en) | 2014-11-05 |
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| CN201420357181.9U Expired - Fee Related CN203930072U (en) | 2014-06-30 | 2014-06-30 | A kind of device for searching for the unmanned plane that falls |
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Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105487093A (en) * | 2015-12-29 | 2016-04-13 | 湖南云顶智能科技有限公司 | Device and method for searching fallen unmanned plane |
| CN107229290A (en) * | 2016-03-24 | 2017-10-03 | 深圳市创翼睿翔天空科技有限公司 | Unmanned plane search and rescue system and method |
| CN107462908A (en) * | 2017-07-01 | 2017-12-12 | 湖南翼航无人机科技有限公司 | A kind of earth station is used for the alignment system and its method of unmanned plane |
| CN107632617A (en) * | 2017-09-28 | 2018-01-26 | 深圳市道通科技股份有限公司 | The control method and device of a kind of unmanned vehicle |
| WO2018076467A1 (en) * | 2016-10-31 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and alarm system thereof |
| CN108112004A (en) * | 2018-02-11 | 2018-06-01 | 深圳市道通智能航空技术有限公司 | Communicator |
| CN109283943A (en) * | 2018-11-20 | 2019-01-29 | 深圳市道通智能航空技术有限公司 | Method for searching and search device when a kind of unmanned plane lost contact |
| CN109573028A (en) * | 2018-12-12 | 2019-04-05 | 深圳市道通智能航空技术有限公司 | A kind of auxiliary unmanned plane method for retrieving, device and unmanned plane |
| CN112666589A (en) * | 2020-12-25 | 2021-04-16 | 广东电网有限责任公司 | Unmanned aerial vehicle searching instrument, unmanned aerial vehicle searching method and power inspection unmanned aerial vehicle |
| CN112666577A (en) * | 2020-11-24 | 2021-04-16 | 青岛欧森系统技术有限公司 | Searching device of accident-losing unmanned aerial vehicle |
-
2014
- 2014-06-30 CN CN201420357181.9U patent/CN203930072U/en not_active Expired - Fee Related
Cited By (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105487093A (en) * | 2015-12-29 | 2016-04-13 | 湖南云顶智能科技有限公司 | Device and method for searching fallen unmanned plane |
| CN107229290A (en) * | 2016-03-24 | 2017-10-03 | 深圳市创翼睿翔天空科技有限公司 | Unmanned plane search and rescue system and method |
| CN107229290B (en) * | 2016-03-24 | 2024-02-20 | 广东泰一高新技术发展有限公司 | Unmanned aerial vehicle search and rescue system and method |
| WO2018076467A1 (en) * | 2016-10-31 | 2018-05-03 | 深圳市大疆创新科技有限公司 | Unmanned aerial vehicle and alarm system thereof |
| CN107462908A (en) * | 2017-07-01 | 2017-12-12 | 湖南翼航无人机科技有限公司 | A kind of earth station is used for the alignment system and its method of unmanned plane |
| CN107632617A (en) * | 2017-09-28 | 2018-01-26 | 深圳市道通科技股份有限公司 | The control method and device of a kind of unmanned vehicle |
| CN107632617B (en) * | 2017-09-28 | 2020-02-14 | 深圳市道通智能航空技术有限公司 | Control method and device for unmanned aerial vehicle |
| CN108112004A (en) * | 2018-02-11 | 2018-06-01 | 深圳市道通智能航空技术有限公司 | Communicator |
| CN109283943A (en) * | 2018-11-20 | 2019-01-29 | 深圳市道通智能航空技术有限公司 | Method for searching and search device when a kind of unmanned plane lost contact |
| CN109573028A (en) * | 2018-12-12 | 2019-04-05 | 深圳市道通智能航空技术有限公司 | A kind of auxiliary unmanned plane method for retrieving, device and unmanned plane |
| CN112666577A (en) * | 2020-11-24 | 2021-04-16 | 青岛欧森系统技术有限公司 | Searching device of accident-losing unmanned aerial vehicle |
| CN112666589A (en) * | 2020-12-25 | 2021-04-16 | 广东电网有限责任公司 | Unmanned aerial vehicle searching instrument, unmanned aerial vehicle searching method and power inspection unmanned aerial vehicle |
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| C14 | Grant of patent or utility model | ||
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| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141105 Termination date: 20190630 |
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| CF01 | Termination of patent right due to non-payment of annual fee |