CN203094457U - Parachute recovering and fail-safe device of small-size unmanned plane - Google Patents
Parachute recovering and fail-safe device of small-size unmanned plane Download PDFInfo
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- CN203094457U CN203094457U CN 201220728428 CN201220728428U CN203094457U CN 203094457 U CN203094457 U CN 203094457U CN 201220728428 CN201220728428 CN 201220728428 CN 201220728428 U CN201220728428 U CN 201220728428U CN 203094457 U CN203094457 U CN 203094457U
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Abstract
The utility model discloses a parachute recovering and fail-safe device of a small-size unmanned plane. The parachute recovering and fail-safe device of the small-size unmanned plane comprises a ground recovering control system and a control device connected with the ground recovering control system through wireless signals, the control device is further respectively connected with a parachate-opening mechanism and a photoelectric sensor, and the photoelectric sensor is connected with a receiver signal lamp. The parachute recovering and fail-safe device of the small-size unmanned plane not only has a parachute recovering function, but also has a fail safe function, when out of control suddenly in a flying process, the small-size unmanned plane can be protected for safe landing, and loss to personnel and properties on the ground due to incontrollable crash of the small-size unmanned plane is effectively avoided.
Description
Technical field
The utility model relates to a kind of parachuting recovery and lost-control protection device, is specifically related to a kind of SUAV (small unmanned aerial vehicle) parachuting recovery and lost-control protection device.
Background technology
The function that existing SUAV (small unmanned aerial vehicle) has only parachuting to reclaim is sent the parachuting instruction by the ground staff to the parachuting recovery system after SUAV (small unmanned aerial vehicle) arrives the target spatial domain, parachute is opened, and drops to ground until SUAV (small unmanned aerial vehicle) safety; The function that does not have lost-control protection when SUAV (small unmanned aerial vehicle) ground that drops to suddenly out of control in flight course, so not only can be lost SUAV (small unmanned aerial vehicle), and can bring loss to ground staff and property.
Summary of the invention
The purpose of this utility model provides a kind of SUAV (small unmanned aerial vehicle) parachuting recovery and lost-control protection device, has solved that existing SUAV (small unmanned aerial vehicle) does not have the lost-control protection function and brings the problem of loss for ground staff and property.
The technical scheme that the utility model adopted is; SUAV (small unmanned aerial vehicle) parachuting recovery and lost-control protection device; comprise the ground recovery control system and by wireless signal and ground recovery control system bonded assembly control setup; control setup also is connected with opto-electronic pickup with parachute deployment means respectively, and opto-electronic pickup is connected with the receiver signal lamp.
The beneficial effects of the utility model are; parachuting recovery of the utility model SUAV (small unmanned aerial vehicle) and lost-control protection device; not only has the function that parachuting is reclaimed; the function that also has lost-control protection simultaneously; when SUAV (small unmanned aerial vehicle) unexpected when out of control in flight course; can protect the SUAV (small unmanned aerial vehicle) safe falling, avoid effectively that SUAV (small unmanned aerial vehicle) is out of control falls to the loss of ground staff and property.
Description of drawings
Fig. 1 is the structural representation of parachuting recovery of the utility model SUAV (small unmanned aerial vehicle) and lost-control protection device.
Among the figure, 1. ground recovery control system, 2. control setup, 3. parachute deployment means, 4. opto-electronic pickup, 5. receiver signal lamp.
The specific embodiment
Below in conjunction with the drawings and specific embodiments the utility model is elaborated.
Parachuting recovery of the utility model SUAV (small unmanned aerial vehicle) and lost-control protection device; referring to accompanying drawing 1; comprise ground recovery control system 1 and by wireless signal and ground recovery control system 1 bonded assembly control setup 2; control setup 2 also is connected with opto-electronic pickup 4 with parachute deployment means 3 respectively, and opto-electronic pickup 4 is connected with receiver signal lamp 5.
Parachuting recovery of the utility model SUAV (small unmanned aerial vehicle) and lost-control protection device mainly contain three functions: function, automatic protection functions out of control and manual defencive function out of control are reclaimed in parachuting.
Function is reclaimed in parachuting, and when SUAV (small unmanned aerial vehicle) arrives the target spatial domain, the ground staff sends instruction to ground recovery control system 1 and passes to control setup 2 by wireless signal, and then control parachute deployment means 3 releases a parachute, and makes the SUAV (small unmanned aerial vehicle) safe falling to ground.
Automatic protection functions out of control; the signal power of utilizing opto-electronic pickup 4 to detect receiver signal lamp 5 judges whether SUAV (small unmanned aerial vehicle) is in runaway condition; and detection signal reached control setup 2; control setup 2 processing controls parachute deployment means 3 by analysis releases a parachute, and makes the SUAV (small unmanned aerial vehicle) safe falling to ground.
Manual defencive function out of control; the signal power of utilizing opto-electronic pickup 4 to detect receiver signal lamp 5 judges whether SUAV (small unmanned aerial vehicle) is in runaway condition; but unmanned plane hardware damage this moment; lose automatic protection functions and feed back to ground recovery control system 1; just send instruction by ground recovery control system 1 and pass to control setup 2 by wireless signal by the ground staff; and then control parachute deployment means 3 release a parachute, make the SUAV (small unmanned aerial vehicle) safe falling to ground.
Parachuting recovery of the utility model SUAV (small unmanned aerial vehicle) and lost-control protection device; not only has the function that parachuting is reclaimed; the function that also has lost-control protection simultaneously; when SUAV (small unmanned aerial vehicle) unexpected when out of control in flight course; can protect the SUAV (small unmanned aerial vehicle) safe falling, avoid effectively that SUAV (small unmanned aerial vehicle) is out of control falls to the loss of ground staff and property.
Claims (1)
1. SUAV (small unmanned aerial vehicle) parachuting recovery and lost-control protection device; it is characterized in that: comprise ground recovery control system (1) and by wireless signal and described ground recovery control system (1) bonded assembly control setup (2); described control setup (2) also is connected with opto-electronic pickup (4) with parachute deployment means (3) respectively, and described opto-electronic pickup (4) is connected with receiver signal lamp (5).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220728428 CN203094457U (en) | 2012-12-26 | 2012-12-26 | Parachute recovering and fail-safe device of small-size unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201220728428 CN203094457U (en) | 2012-12-26 | 2012-12-26 | Parachute recovering and fail-safe device of small-size unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203094457U true CN203094457U (en) | 2013-07-31 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201220728428 Expired - Fee Related CN203094457U (en) | 2012-12-26 | 2012-12-26 | Parachute recovering and fail-safe device of small-size unmanned plane |
Country Status (1)
| Country | Link |
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| CN (1) | CN203094457U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103625644A (en) * | 2013-12-16 | 2014-03-12 | 鲍业全 | Engine-power-free landing assisting device of airplane |
| CN103693202A (en) * | 2013-08-30 | 2014-04-02 | 北京空间机电研究所 | Recovery system of helicopter |
| CN104058095A (en) * | 2014-06-12 | 2014-09-24 | 深圳市哈博森科技有限公司 | Aircraft parachute control system and method |
| CN104417759A (en) * | 2013-08-28 | 2015-03-18 | 无锡慧思顿科技有限公司 | Multi-parameter multi-sensor intelligent parachute |
| CN106227083A (en) * | 2016-07-20 | 2016-12-14 | 广东容祺智能科技有限公司 | A kind of unmanned plane motor phase failure monitoring and protecting device |
| CN107108038A (en) * | 2016-12-01 | 2017-08-29 | 深圳市大疆创新科技有限公司 | A kind of device for controlling forced landing, method, equipment |
-
2012
- 2012-12-26 CN CN 201220728428 patent/CN203094457U/en not_active Expired - Fee Related
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104417759A (en) * | 2013-08-28 | 2015-03-18 | 无锡慧思顿科技有限公司 | Multi-parameter multi-sensor intelligent parachute |
| CN104417759B (en) * | 2013-08-28 | 2016-06-01 | 武汉飞恩微电子有限公司 | A kind of Intelligent parachute based on the many sensings of multiparameter |
| CN103693202A (en) * | 2013-08-30 | 2014-04-02 | 北京空间机电研究所 | Recovery system of helicopter |
| CN103693202B (en) * | 2013-08-30 | 2015-11-11 | 北京空间机电研究所 | A kind of recovery system of helicopter |
| CN103625644A (en) * | 2013-12-16 | 2014-03-12 | 鲍业全 | Engine-power-free landing assisting device of airplane |
| CN104058095A (en) * | 2014-06-12 | 2014-09-24 | 深圳市哈博森科技有限公司 | Aircraft parachute control system and method |
| CN106227083A (en) * | 2016-07-20 | 2016-12-14 | 广东容祺智能科技有限公司 | A kind of unmanned plane motor phase failure monitoring and protecting device |
| CN107108038A (en) * | 2016-12-01 | 2017-08-29 | 深圳市大疆创新科技有限公司 | A kind of device for controlling forced landing, method, equipment |
| WO2018098774A1 (en) * | 2016-12-01 | 2018-06-07 | 深圳市大疆创新科技有限公司 | Apparatus, method and device for controlling forced landing |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| 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: 20130731 Termination date: 20131226 |