CN202609087U - Downward dropping type flexible-connection cabin cover parachute-opening device of push-back type mini-sized pilotless plane - Google Patents
Downward dropping type flexible-connection cabin cover parachute-opening device of push-back type mini-sized pilotless plane Download PDFInfo
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- CN202609087U CN202609087U CN 201220195447 CN201220195447U CN202609087U CN 202609087 U CN202609087 U CN 202609087U CN 201220195447 CN201220195447 CN 201220195447 CN 201220195447 U CN201220195447 U CN 201220195447U CN 202609087 U CN202609087 U CN 202609087U
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- parachute
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- cabin cover
- pilotless plane
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Abstract
The utility model relates to a downward dropping type flexible-connection cabin cover parachute-opening device of a push-back type mini-sized pilotless plane. The downwards dropping type flexible-connection cabin cover parachute-opening device of the push-back type mini-sized pilotless plane comprises a parachute cabin, parachutes and a parachute cabin cover, wherein one end of the parachute cabin cover of the push-back type mini-sized pilotless plane is provided with a plug connected with a pilotless plane body; one end of the parachute cabin of the push-back type mini-sized pilotless plane is provided with a groove which corresponds to the plug; the plug is inserted into the parachute cabin groove; the other end of the parachute cabin is provided with a steering engine clamping groove; a steering engine rocker arm is clamped into a clamping groove; one end of a parachute cabin soft cloth is connected with the parachute cabin cover, and the other end is bonded with the parachute cabin of the push-back type mini-sized pilotless plane; and the parachute cabin cover and the pilotless plane body are provided with magnets. According to the utility model, when the push-back type mini-sized pilotless plane encounters an emergency situation by flying in any flight state, the parachutes need to be opened, the parachute cabin cover can be safely and fast opened, and the parachutes of the push-back type mini-sized pilotless plane can be safely popped out; and the downward dropping type flexible-connection cabin cover parachute-opening device disclosed by the utility model has the advantages of simple structure, safety, stability and high reliability.
Description
Technical field
The utility model relates to the micro-unmanned aircraft down-throwing of a kind of back-pushed hatchcover parachute opener that is flexible coupling.
Background technology
At present, known unmanned plane parachute parachute-opening mode is divided into two kinds: parachute-opening of upthrow formula and down-throwing parachute-opening, the hatchcover in umbrella cabin are generally connected by the metal hinge; And this metal hinge wants cube little, and is in light weight, and the utmost point is not easy to seek on market; Traditional down-throwing parachute-opening umbrella hatchcover is at the flight attitude mal or receive to be difficult for opening under the bigger situation of airflow influence; Security and stability is poor, and the metal hinge connects dumb, and the parachute-opening of unmanned plane parachute is unreliable; Cause aircraft accident easily, cause aircraft damage.
Summary of the invention
In order to overcome the shortcoming of existing unmanned plane parachute parachute deployment means, the utility model provides the micro-unmanned aircraft down-throwing of a kind of back-pushed hatchcover parachute opener that is flexible coupling.
The utility model solves the technical scheme that its technical matters adopted: the micro-unmanned aircraft down-throwing of a kind of back-pushed hatchcover parachute opener that is flexible coupling; Comprise umbrella cabin (7), parachute (2) and umbrella hatchcover (4); Unmanned plane umbrella hatchcover (4) one ends are provided with plug (5) and connect unmanned aerial vehicle body; (7) one ends are provided with and the pairing groove of plug (5) in the umbrella cabin of unmanned aerial vehicle, and plug (5) inserts in the groove of umbrella cabin (7), and umbrella cabin (7) other end is provided with steering wheel draw-in groove (1); Steering wheel (3) rocking arm (9) snaps in the draw-in groove (1); Soft cloth (6) one ends in umbrella cabin are connected with umbrella hatchcover (4), and the other end is bonded on the umbrella cabin (7) of unmanned aerial vehicle, on umbrella hatchcover (4) and unmanned aerial vehicle body, is provided with magnet (8).
The beneficial effect of the utility model is, when unmanned plane runs into emergency situation in-flight under any state of flight, and when need release a parachute, but parachute umbrella cabin hatchcover safety; Open fast, safety ejects the unmanned plane parachute, and is simple in structure; Safety, stable, reliability is high.
Description of drawings
Fig. 1 is the structural representation of the utility model.
Fig. 2 is the utility model umbrella hatchcover unfolding mode structural representation.
Fig. 3 is a umbrella cabin structure scheme drawing.
The specific embodiment
Below in conjunction with accompanying drawing and embodiment the utility model is further specified.
The micro-unmanned aircraft of a kind of back-pushed hatchcover parachute opener that is flexible coupling; Comprise umbrella cabin 7, parachute 2 and umbrella hatchcover 4, unmanned plane umbrella hatchcover 4 one ends are provided with plug 5, and 7 one ends are provided with and plug 5 pairing grooves in the umbrella cabin of unmanned aerial vehicle; Plug 5 inserts in 7 grooves of umbrella cabin; Umbrella cabin 7 other ends are provided with steering wheel draw-in groove 1, and steering wheel 3 rocking arms 9 snap in the draw-in groove 1, and umbrella cabin soft cloth 6 one ends are connected with umbrella hatchcover 4; The other end is bonded on the umbrella cabin 7 of unmanned aerial vehicle, on umbrella hatchcover 4 and unmanned aerial vehicle body, is provided with magnet 8.
In the unmanned plane during flying process, when unmanned plane need be opened umbrella cabin 7, steering wheel 3 rocking arms 9 withdrawed from from steering wheel 3 draw-in grooves 1; Umbrella hatchcover 4 is opened; The umbrella cabin connects fuselage plug 5 and skids off from fuselage, receives airflow influence, and umbrella hatchcover 4 moves backward; The magnet 8 of umbrella hatchcover 4 is adsorbed onto on the unmanned aerial vehicle body automatically, and parachute 2 ejects.
Claims (1)
1. the micro-unmanned aircraft down-throwing of back-pushed hatchcover parachute opener that is flexible coupling; Comprise umbrella cabin (7), parachute (2) and umbrella hatchcover (4), it is characterized in that: unmanned plane umbrella hatchcover (4) one ends are provided with plug (5), and (7) one ends are provided with and the pairing groove of plug (5) in the umbrella cabin of unmanned aerial vehicle; Plug (5) inserts in the groove of umbrella cabin (7); Umbrella cabin (7) other end is provided with steering wheel (3) draw-in groove (1), and steering wheel (3) rocking arm (9) snaps in the draw-in groove (1), and soft cloth (6) one ends in umbrella cabin are connected with umbrella hatchcover (4); The other end is bonded on the umbrella cabin (7) of unmanned aerial vehicle, on umbrella hatchcover (4) and unmanned aerial vehicle body, is provided with magnet (8).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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CN 201220195447 CN202609087U (en) | 2012-05-03 | 2012-05-03 | Downward dropping type flexible-connection cabin cover parachute-opening device of push-back type mini-sized pilotless plane |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201220195447 CN202609087U (en) | 2012-05-03 | 2012-05-03 | Downward dropping type flexible-connection cabin cover parachute-opening device of push-back type mini-sized pilotless plane |
Publications (1)
Publication Number | Publication Date |
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CN202609087U true CN202609087U (en) | 2012-12-19 |
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CN 201220195447 Expired - Lifetime CN202609087U (en) | 2012-05-03 | 2012-05-03 | Downward dropping type flexible-connection cabin cover parachute-opening device of push-back type mini-sized pilotless plane |
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CN (1) | CN202609087U (en) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103253374A (en) * | 2013-05-17 | 2013-08-21 | 湖州鹏翼航空器科技有限公司 | Quick parachute opening device based on control of distance measuring device |
CN105292495A (en) * | 2015-11-13 | 2016-02-03 | 深圳飞马机器人科技有限公司 | Fast parachute-opening parachute bay structure for unmanned aerial vehicle |
CN106314802A (en) * | 2016-09-20 | 2017-01-11 | 北京韦加无人机科技股份有限公司 | Parachute bay device for unmanned aerial vehicle and unmanned aerial vehicle |
CN106956780A (en) * | 2017-05-09 | 2017-07-18 | 嘉兴安行信息科技有限公司 | Unmanned plane parachute assembly |
CN108981919A (en) * | 2018-06-08 | 2018-12-11 | 北京航空航天大学 | A kind of sky polarised light detecting vertical distribution device and method |
CN109250111A (en) * | 2018-09-29 | 2019-01-22 | 长光卫星技术有限公司 | A kind of Modularized unmanned machine parachute cabin system |
CN112441238A (en) * | 2020-11-20 | 2021-03-05 | 航天时代飞鸿技术有限公司 | Mechanical elastic parachute unfolding device and unfolding method |
-
2012
- 2012-05-03 CN CN 201220195447 patent/CN202609087U/en not_active Expired - Lifetime
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN103253374A (en) * | 2013-05-17 | 2013-08-21 | 湖州鹏翼航空器科技有限公司 | Quick parachute opening device based on control of distance measuring device |
CN103253374B (en) * | 2013-05-17 | 2015-05-13 | 湖州鹏翼航空器科技有限公司 | Quick parachute opening device based on control of distance measuring device |
CN105292495A (en) * | 2015-11-13 | 2016-02-03 | 深圳飞马机器人科技有限公司 | Fast parachute-opening parachute bay structure for unmanned aerial vehicle |
CN105292495B (en) * | 2015-11-13 | 2018-01-05 | 深圳飞马机器人科技有限公司 | A kind of quick parachute-opening umbrella cabin structure of unmanned plane |
CN106314802A (en) * | 2016-09-20 | 2017-01-11 | 北京韦加无人机科技股份有限公司 | Parachute bay device for unmanned aerial vehicle and unmanned aerial vehicle |
CN106956780A (en) * | 2017-05-09 | 2017-07-18 | 嘉兴安行信息科技有限公司 | Unmanned plane parachute assembly |
CN108981919A (en) * | 2018-06-08 | 2018-12-11 | 北京航空航天大学 | A kind of sky polarised light detecting vertical distribution device and method |
CN109250111A (en) * | 2018-09-29 | 2019-01-22 | 长光卫星技术有限公司 | A kind of Modularized unmanned machine parachute cabin system |
CN112441238A (en) * | 2020-11-20 | 2021-03-05 | 航天时代飞鸿技术有限公司 | Mechanical elastic parachute unfolding device and unfolding method |
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Legal Events
Date | Code | Title | Description |
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C14 | Grant of patent or utility model | ||
GR01 | Patent grant | ||
C56 | Change in the name or address of the patentee | ||
CP03 | Change of name, title or address |
Address after: 710054 Shaanxi province Xi'an Xiying Road No. 63 Patentee after: Xi'an Dadi surveying and mapping Limited by Share Ltd Address before: 710054 Shaanxi province Xi'an Xiying Road No. 63 Yan Ying Vista P layer Patentee before: Xi'an Dadi Surveying Mapping Project Co., Ltd. |
|
CX01 | Expiry of patent term | ||
CX01 | Expiry of patent term |
Granted publication date: 20121219 |