CN206171828U - Unmanned aerial vehicle safety arrangement that falls - Google Patents
Unmanned aerial vehicle safety arrangement that falls Download PDFInfo
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- CN206171828U CN206171828U CN201621155874.5U CN201621155874U CN206171828U CN 206171828 U CN206171828 U CN 206171828U CN 201621155874 U CN201621155874 U CN 201621155874U CN 206171828 U CN206171828 U CN 206171828U
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Abstract
The utility model belongs to the technical field of unmanned aerial vehicle, concretely relates to unmanned aerial vehicle safety arrangement that falls, the problem of the technique is solved for: the utility model provides an utilize air bag to fall to unmanned aerial vehicle and carry out the unmanned aerial vehicle safety arrangement that falls that protects, can effectively prevent unmanned aerial vehicle from to fall the aircraft self that causes damages, ground personnel injury and loss of property, the technical scheme who adopts does: an unmanned aerial vehicle safety arrangement that falls, includes the unmanned aerial vehicle body, be provided with radio signal recepition ware, flight controller, video monitoring device, image display ware, safety arrangement and power supply on the unmanned aerial vehicle body, the output of radio signal recepition ware links to each other with flight controller's input, flight controller's output is continuous with video monitoring device and safety arrangement's input respectively, the output of video monitoring device links to each other with the input of image display ware, power supply is the power supply of whole device.
Description
Technical field
This utility model belongs to the technical field of unmanned plane, and in particular to a kind of unmanned plane fall safety protection device.
Background technology
At present, unmanned plane is widely used to the industry-by-industries such as industry, agricultural, military affairs, for example：Unmanned plane can be applicable to plant
Guarantor field, by the use of unmanned plane as flying platform carry medicine-chest, spray appliance either monitoring device farmland is sprayed or
Data acquisition；Unmanned plane can be applicable to streetscape shooting, is carried out using the unmanned plane for carrying camera system and is taken photo by plane on a large scale, realize
The effect looked down in the air；Unmanned plane can be applicable to electric inspection process, using being equipped with high-definition digital video camera and photographing unit and GPS
The unmanned plane of alignment system can carry out positioning autonomous cruise along electrical network, and filmed image is transmitted in real time, and monitoring personnel can be on computers
Synchronously watch and manipulation；Unmanned plane can be applicable to field of environment protection, and environment is carried out with the unmanned plane of collecting device using analysis is carried
Monitoring, environmental law enforcement and environmental improvement：Observation air, soil, vegetation and water quality condition, the waste gas of factory of monitoring enterprise and waste water
Discharge is found polluter, is sprayed in the air using carrying the soft wing unmanned plane that catalyst and meteorological detection set, Ke Yi
Certain area internal diabetes remove haze；Unmanned plane can be applicable to Post disaster relief field, using the unmanned plane for being equipped with high-definition shooting device
Disaster area is taken photo by plane, there is provided newest image information.
But, unmanned plane is highly susceptible in the air the interference of several factors in flight course causes unmanned plane to run out of steam
Or disequilibrium and fall, cause aircraft itself to damage and ground staff's injury and the phenomenon of property loss happen occasionally.One
A little expensive unmanned plane prices are all first in tens of thousands of or even hundreds of thousands, and falling loss in the event of failure will be incomparable heavy.Existing skill
Art is mainly protected using parachute to unmanned plane, but the opening speed of parachute is slow, if unmanned plane is in low latitude
Break down, then can cause very big loss because parachute is not opened in time.
Utility model content
This utility model overcomes the shortcomings of that prior art is present, and technical problem to be solved is：There is provided a kind of using peace
Full air bag falls the unmanned plane fall safety protection device protected to unmanned plane, can effectively prevent unmanned plane from falling and cause
Aircraft itself damage, ground staff injury and property loss.
In order to solve above-mentioned technical problem, the technical solution adopted in the utility model is：A kind of unmanned plane fall safety is protected
Protection unit, including unmanned plane body, are provided with wireless signal receiver, flight controller, video prison on the unmanned plane body
Control device, image display, safety guard and power supply, outfan and the flight control of the wireless signal receiver
The input of device is connected, the outfan of the flight controller respectively with video monitoring apparatus and the input of safety guard
It is connected, the outfan of the video monitoring apparatus is connected with the input of image display, the power supply is whole device
Power supply；
The safety guard includes air spring control, triggering device and airbag apparatus, the air spring control output
End is connected respectively with the input of flight controller and the input of triggering device, and outfan and the air bag of the triggering device are filled
Put connected.
The video monitoring apparatus include photographic head head, video superimpose unit and the image for controlling photographic head work
Transmitter, the photographic head is electrically connected with video superimpose unit, outfan and the picture transmitter of the video superimpose unit
Input is connected, and described image transmitter is connected by wireless module with image display.
The air spring control includes gyroscope and acceleration transducer.
The speed regulator for controlling motor speed on propeller is additionally provided with the unmanned plane body.
The triggering device includes attitude sensing triggering, acceleration rate threshold triggering and manually triggers.
The air bag that the airbag apparatus are ejected adopts semi-circular structure.
The unmanned plane includes multi-rotor aerocraft, Fixed Wing AirVehicle and depopulated helicopter.
Model MPU-6000 of the gyroscope.
This utility model has the advantages that compared with prior art：
In a kind of unmanned plane fall safety protection device of this utility model, including unmanned plane body, the unmanned plane body
It is provided with wireless signal receiver, flight controller, video monitoring apparatus, image display, safety guard and power supply electricity
Source, safety guard includes air spring control, triggering device and airbag apparatus；During unmanned plane during flying, air spring control is real-time
The angle of inclination of monitoring unmanned plane and self-acceleration, when the angle of inclination for detecting unmanned plane is close to more than threshold value or acceleration
During freely falling body, air spring control starts triggering device and ejects the air bag in airbag apparatus, and air bag will after opening
Unmanned plane is all wrapped up, and is prevented unmanned plane from falling and is caused unnecessary property loss, meanwhile, air spring control sends out fault-signal
Give flight controller, flight controller controlled motor quits work, and propeller stops operating, and prevents propeller from beating in air bag
It is broken；Compared with traditional parachute protection device, a kind of safety of unmanned plane fall safety protection device described in the utility model
The airbag-releasing time is 0.03s, is caused because parachute opening speed is relatively slow when can effectively prevent unmanned plane low latitude from falling
Property loss and personnel injure.
Description of the drawings
Below in conjunction with the accompanying drawings the utility model is described in more detail；
Fig. 1 is structural representation of the present utility model；
Fig. 2 is the structural representation of this utility model video monitoring apparatus；
Fig. 3 is the structural representation of this utility model unmanned plane；
Fig. 4 is the sectional stereogram that this utility model airbag apparatus are ejected；
Fig. 5 is the structural representation that this utility model airbag apparatus are ejected；
In figure：1 is unmanned plane body, and 2 is wireless signal receiver, and 3 is flight controller, and 4 is video monitoring apparatus,
401 are control photographic head, and 402 is photographic head head, and 403 is video superimpose unit, and 404 is picture transmitter, and 5 show for image
Device, 6 is safety guard, and 601 is air spring control, and 602 is triggering device, and 603 is airbag apparatus, and 7 is power supply, 8
For motor, 9 is speed regulator.
Specific embodiment
To make purpose, technical scheme and the advantage of this utility model embodiment clearer, below will be to this utility model
Technical scheme in embodiment is clearly and completely described, it is clear that described embodiment is a part of the present utility model
Embodiment, rather than the embodiment of whole；Based on the embodiment in this utility model, those of ordinary skill in the art are without work
Go out the every other embodiment obtained under the premise of creative work, belong to the scope of this utility model protection.
As shown in Figure 1, Figure 3, a kind of unmanned plane fall safety protection device, including unmanned plane body 1, the unmanned plane sheet
Wireless signal receiver 2, flight controller 3, video monitoring apparatus 4, image display 5, safety guard are provided with body 1
6 and power supply 7, the outfan of the wireless signal receiver 2 is connected with the input of flight controller 3, the flight control
The outfan of device processed 3 is connected respectively with the input of video monitoring apparatus 4 and safety guard 6, the video monitoring apparatus 4
Outfan be connected with the input of image display 5, the power supply 7 is powered for whole device；
The safety guard 6 includes air spring control 601, triggering device 602 and airbag apparatus 603, the air bag
The outfan of controller 601 is connected respectively with the input of flight controller 3 and the input of triggering device 602, the triggering dress
The outfan for putting 602 is connected with airbag apparatus 603, and the air bag that the airbag apparatus 603 are ejected adopts semi-circular structure.
As shown in Fig. 2 the video monitoring apparatus 4 include for control photographic head 401 work photographic head head 402,
Video superimpose unit 403 and picture transmitter 404, the photographic head 401 is electrically connected with video superimpose unit 403, the video
The outfan of superpositing unit 403 is connected with the input of picture transmitter 404, and described image transmitter 404 passes through wireless module
It is connected with image display 5；Video monitoring apparatus 4 are used for the aircraft such as Aerial Images, the aircraft speed of a ship or plane, course, height letter
Breath is sent to image display 5, and image display 5 is shown above- mentioned information；The photographic head head 402 controls photographic head
401 rotate, and the information such as the image information that video superimpose unit 403 obtains photographic head 401 and flight parameter of unmanned plane is carried out
Picture transmitter 404 is superimposed and is sent to, information is transferred to image display 5 by picture transmitter 404 by wireless module.
The speed regulator 9 for controlling the rotating speed of motor 8 on propeller is additionally provided with the unmanned plane body 1.
The air spring control 601 includes the gyroscope and acceleration transducer of model MPU-6000, and gyroscope is real-time
The change at detection unmanned plane angle of inclination, acceleration transducer is used to monitor the whether close freely falling body of acceleration of unmanned plane；
The triggering device 602 includes attitude sensing triggering, acceleration rate threshold triggering and manually triggering etc.；The triggering device
602 using the safety in the ignition lead and extender triggering airbag apparatus 603 in the carbon fiber foot rest connecting tube being connected with fuselage
Air bag is ejected, and the opening time of airbag apparatus 603 is 30ms, and speed is very fast, when can effectively prevent unmanned plane low latitude from falling
The personnel's property loss caused because parachute opening speed is relatively slow.
Unmanned aerial vehicle body top and bottom are respectively provided with an airbag apparatus 603, airbag fold in this utility model
In being positioned over airbag apparatus 603, when aircraft breaks down, air spring control 601 starts triggering device 602 by airbag apparatus
Air bag in 603 is ejected, and unmanned plane be all surrounded can effectively be prevented aircraft from falling the personnel for causing by air bag
Property loss.
The unmanned plane includes multi-rotor aerocraft, Fixed Wing AirVehicle and depopulated helicopter, and this utility model revolving more
Illustrate as a example by rotor aircraft.
Specifically, flight orders and cradle head control order are sent to wireless signal receiver 2 by ground remote control signal, wirelessly
Signal receiver 2 transmits a signal to flight controller 3, and flight controller 3 is by the speed of a ship or plane of unmanned plane during flying, course, height etc.
Flight parameter information is sent to the video superimpose unit 403 in video monitoring apparatus 4, and flight controller 3 is real by speed regulator 10
The control of the existing rotating speed of motor 9, so as to the rotating speed of propeller on the axle of controlled motor 9, be finally reached the flight speed to aircraft and
The control of heading, video monitoring apparatus 4 are used to send out the aircraft information such as Aerial Images, the aircraft speed of a ship or plane, course, height
Image display 5 is given, image display 5 is shown above- mentioned information.
As shown in Figure 4, Figure 5, when air spring control 601 detects the angle of inclination of unmanned plane or acceleration is close to freely to fall
During body, air spring control 601 starts triggering device 602, the air bag triggering in airbag apparatus 603 is opened, air bag
Unmanned plane is all wrapped up after opening, is prevented unmanned plane from falling and is caused unnecessary property loss, meanwhile, air spring control 601
Fault-signal is sent to into flight controller 5, the controlled motor 8 of flight controller 5 quits work, and propeller stops operating, prevent
Only propeller breaks in air bag；Compared with traditional parachute protection device, a kind of unmanned plane described in the utility model falls peace
The air bag opening time of full protection device is 0.03s, because parachute is opened when can effectively prevent unmanned plane low latitude from falling
Speed is relatively slow and causes property loss and personnel's injury.
Finally it should be noted that：Various embodiments above is only illustrating the technical solution of the utility model, rather than it is limited
System；Although being described in detail to this utility model with reference to foregoing embodiments, one of ordinary skill in the art should
Understand：It still can modify to the technical scheme described in foregoing embodiments, either to which part or whole
Technical characteristic carries out equivalent；And these are changed or are replaced, the essence for not making appropriate technical solution departs from this practicality newly
The scope of each embodiment technical scheme of type.
Claims (8)
1. a kind of unmanned plane fall safety protection device, including unmanned plane body（1）, it is characterised in that：The unmanned plane body
（1）On be provided with wireless signal receiver（2）, flight controller（3）, video monitoring apparatus（4）, image display（5）, safety
Protection device（6）And power supply（7）, the wireless signal receiver（2）Outfan and flight controller（3）Input
It is connected, the flight controller（3）Outfan respectively with video monitoring apparatus（4）And safety guard（6）Input
It is connected, the video monitoring apparatus（4）Outfan and image display（5）Input be connected, the power supply（7）For
Whole device is powered；
The safety guard（6）Including air spring control（601）, triggering device（602）And airbag apparatus（603）, it is described
Air spring control（601）Outfan respectively with flight controller（3）Input and triggering device（602）Input be connected,
The triggering device（602）Outfan and airbag apparatus（603）It is connected.
2. a kind of unmanned plane fall safety protection device according to claim 1, it is characterised in that：The video monitoring dress
Put（4）Including for controlling photographic head（401）The photographic head head of work（402）, video superimpose unit（403）With image transmitting
Machine（404）, the photographic head（401）With video superimpose unit（403）Electrical connection, the video superimpose unit（403）Output
End and picture transmitter（404）Input be connected, described image transmitter（404）By wireless module and image display
（5）It is connected.
3. a kind of unmanned plane fall safety protection device according to claim 1, it is characterised in that：The air spring control
（601）Including gyroscope and acceleration transducer.
4. a kind of unmanned plane fall safety protection device according to claim 1, it is characterised in that：The unmanned plane body
（1）On be additionally provided with for controlling motor on propeller（8）The speed regulator of rotating speed（9）.
5. a kind of unmanned plane fall safety protection device according to claim 1, it is characterised in that：The triggering device
（602）Trigger including attitude sensing triggering, acceleration rate threshold triggering and manually.
6. a kind of unmanned plane fall safety protection device according to claim 1, it is characterised in that：The airbag apparatus
（603）The air bag of ejection adopts semi-circular structure.
7. a kind of unmanned plane fall safety protection device according to claim 1, it is characterised in that：The unmanned plane includes
Multi-rotor aerocraft, Fixed Wing AirVehicle and depopulated helicopter.
8. a kind of unmanned plane fall safety protection device according to claim 3, it is characterised in that：The type of the gyroscope
Number be MPU-6000.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621155874.5U CN206171828U (en) | 2016-10-31 | 2016-10-31 | Unmanned aerial vehicle safety arrangement that falls |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621155874.5U CN206171828U (en) | 2016-10-31 | 2016-10-31 | Unmanned aerial vehicle safety arrangement that falls |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206171828U true CN206171828U (en) | 2017-05-17 |
Family
ID=58679392
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| CN201621155874.5U Active CN206171828U (en) | 2016-10-31 | 2016-10-31 | Unmanned aerial vehicle safety arrangement that falls |
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Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106995061A (en) * | 2017-05-20 | 2017-08-01 | 林永勤 | A kind of battery protecting apparatus of unmanned plane |
| CN107521694A (en) * | 2017-08-29 | 2017-12-29 | 西安冰果智能航空科技有限公司 | A kind of Small and micro-satellite recovery air bag controlled mechanism |
| CN108617620A (en) * | 2017-11-24 | 2018-10-09 | 吴李海 | A kind of pulsed spraying machine |
| CN108891587A (en) * | 2018-07-23 | 2018-11-27 | 河南机电职业学院 | A kind of unmanned plane with air bag |
| CN109110127A (en) * | 2018-07-25 | 2019-01-01 | 国网山东省电力公司枣庄供电公司 | A kind of patrolling transmission line unmanned plane failure drop protection device |
| CN110152219A (en) * | 2019-04-19 | 2019-08-23 | 宁波大学科学技术学院 | Infant breathing chamber and method of using the same |
| CN110562470A (en) * | 2019-10-11 | 2019-12-13 | 复旦大学 | Unmanned aerial vehicle protection device that falls |
| CN110979645A (en) * | 2019-12-18 | 2020-04-10 | 新疆联海创智信息科技有限公司 | Post-fault emergency control device and method for unmanned aerial vehicle |
| CN111038709A (en) * | 2019-10-11 | 2020-04-21 | 湖北航天化学技术研究所 | Helicopter safety airbag triggering method and device |
| CN111038718A (en) * | 2020-01-07 | 2020-04-21 | 中铁第五勘察设计院集团有限公司 | Unmanned aerial vehicle |
| CN113104222A (en) * | 2021-05-06 | 2021-07-13 | 北京理工大学 | A kind of autonomous safety anti-fall device for unmanned aerial vehicle and its control method |
| CN113753246A (en) * | 2021-05-11 | 2021-12-07 | 南京壮大智能科技研究院有限公司 | Small unmanned aerial vehicle falling protection device and working method thereof |
| CN113799993A (en) * | 2021-11-02 | 2021-12-17 | 广东电网有限责任公司 | Micro unmanned aerial vehicle buffering gasbag system that falls |
-
2016
- 2016-10-31 CN CN201621155874.5U patent/CN206171828U/en active Active
Cited By (14)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106995061A (en) * | 2017-05-20 | 2017-08-01 | 林永勤 | A kind of battery protecting apparatus of unmanned plane |
| CN107521694A (en) * | 2017-08-29 | 2017-12-29 | 西安冰果智能航空科技有限公司 | A kind of Small and micro-satellite recovery air bag controlled mechanism |
| CN108617620A (en) * | 2017-11-24 | 2018-10-09 | 吴李海 | A kind of pulsed spraying machine |
| CN108891587A (en) * | 2018-07-23 | 2018-11-27 | 河南机电职业学院 | A kind of unmanned plane with air bag |
| CN109110127A (en) * | 2018-07-25 | 2019-01-01 | 国网山东省电力公司枣庄供电公司 | A kind of patrolling transmission line unmanned plane failure drop protection device |
| CN110152219A (en) * | 2019-04-19 | 2019-08-23 | 宁波大学科学技术学院 | Infant breathing chamber and method of using the same |
| CN110562470A (en) * | 2019-10-11 | 2019-12-13 | 复旦大学 | Unmanned aerial vehicle protection device that falls |
| CN111038709A (en) * | 2019-10-11 | 2020-04-21 | 湖北航天化学技术研究所 | Helicopter safety airbag triggering method and device |
| CN110979645A (en) * | 2019-12-18 | 2020-04-10 | 新疆联海创智信息科技有限公司 | Post-fault emergency control device and method for unmanned aerial vehicle |
| CN111038718A (en) * | 2020-01-07 | 2020-04-21 | 中铁第五勘察设计院集团有限公司 | Unmanned aerial vehicle |
| CN113104222A (en) * | 2021-05-06 | 2021-07-13 | 北京理工大学 | A kind of autonomous safety anti-fall device for unmanned aerial vehicle and its control method |
| CN113104222B (en) * | 2021-05-06 | 2022-04-29 | 北京理工大学 | Autonomous safety anti-falling device for unmanned aerial vehicle and control method thereof |
| CN113753246A (en) * | 2021-05-11 | 2021-12-07 | 南京壮大智能科技研究院有限公司 | Small unmanned aerial vehicle falling protection device and working method thereof |
| CN113799993A (en) * | 2021-11-02 | 2021-12-17 | 广东电网有限责任公司 | Micro unmanned aerial vehicle buffering gasbag system that falls |
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