CN105292495A - Fast parachute-opening parachute bay structure for unmanned aerial vehicle - Google Patents
Fast parachute-opening parachute bay structure for unmanned aerial vehicle Download PDFInfo
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- CN105292495A CN105292495A CN201510774088.7A CN201510774088A CN105292495A CN 105292495 A CN105292495 A CN 105292495A CN 201510774088 A CN201510774088 A CN 201510774088A CN 105292495 A CN105292495 A CN 105292495A
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- sheet
- opening
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- 230000005540 biological transmission Effects 0.000 claims abstract description 9
- 230000002457 bidirectional effect Effects 0.000 abstract 5
- 238000006073 displacement reaction Methods 0.000 description 3
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- 230000007547 defect Effects 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
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Abstract
The invention discloses a fast parachute-opening parachute bay structure for an unmanned aerial vehicle. The fast parachute-opening parachute bay structure comprises a parachute bay body and a parachute cover. The parachute bay body is provided with a steering engine mounting support, a steering engine, a bidirectional steering engine sheet, a left hanging point lug sheet and a right hanging point lug sheet are fixedly mounted on the steering engine mounting support, the bidirectional steering engine sheet is connected with the steering engine, and the left hanging point and the right hanging point lug sheet are connected with the bidirectional steering engine sheet. The left hanging point lug sheet is connected with the bidirectional steering engine sheet through a left unlocking transmission shaft, and the right hanging point lug sheet is connected with the bidirectional steering engine sheet through a right unlocking transmission shaft. Guide sleeves for being fixedly hung on the left hanging point lug sheet and the right hanging point lug sheet are fixedly arranged on the parachute cover, and are fixedly mounted on the parachute cover through screws. After a parachute is mounted in a non-power-up state, the unmanned aerial vehicle can be automatically locked, operation is easy, when an emergency situation occurs or a task is completed and parachuting is needed, the parachute cover can be automatically opened to complete parachuting of the unmanned aerial vehicle, and safety and convenience are achieved.
Description
Technical field
The present invention relates to unmanned plane equipment, in particular the quick parachute-opening umbrella cabin structure of a kind of unmanned plane.
Background technology
Conventional unmanned plane parachute deployment means can leak outside part, and cannot ensure smooth parachute-opening, repeatedly fills umbrella and carry out self-locking under the state that cannot not power at steering wheel, cannot carry out backhaul self-locking under steering wheel parachute-opening moment suddenly off-position.
Therefore, prior art existing defects, needs to improve.
Summary of the invention
Technical matters to be solved by this invention is: provide a kind of under not power supply state, parachute is installed after, unmanned plane can auto lock, simple to operate, and, run into emergency situations or task complete need parachuting time, automatically canopy can be opened and complete the parachuting of unmanned plane, the quick parachute-opening umbrella cabin structure of unmanned plane of safe and convenient.
Technical scheme of the present invention is as follows: the quick parachute-opening umbrella cabin structure of a kind of unmanned plane, comprise umbrella cabin cabin body and canopy, wherein, cabin, umbrella cabin body is provided with a steering wheel mounting bracket, two-way steering wheel sheet steering wheel mounting bracket is installed with a steering wheel, being connected with steering wheel, and the left hanging point auricle be connected with two-way steering wheel sheet respectively and right hanging point auricle; Wherein, left hanging point auricle is connected with two-way steering wheel sheet by left unblock transmission shaft, and right hanging point auricle is connected with two-way steering wheel sheet by right unblock transmission shaft; Canopy is also fixedly installed respectively the pilot sleeve for fixedly hanging over left hanging point auricle and right hanging point auricle, each pilot sleeve is fixed on canopy by screw.
Be applied to technique scheme, described unmanned plane is with in quick parachute-opening umbrella cabin structure, and left hanging point auricle is also fixed on steering wheel mounting bracket by a left torsion spring, and right hanging point auricle is also fixed on steering wheel mounting bracket by a right torsion spring.
Be applied to each technique scheme, described unmanned plane is with in quick parachute-opening umbrella cabin structure, each pilot sleeve is fixed on the parachute-opening leading section of canopy, and the parachute-opening rearward end of canopy is also provided with one group of lug boss, and cabin, umbrella cabin body is provided with one group of hole clipping corresponding to position.
Be applied to each technique scheme, described unmanned plane is with in quick parachute-opening umbrella cabin structure, and cabin, umbrella cabin body embeds the fuselage interior being fixed on unmanned plane.
Adopt such scheme, the present invention is by the two-way steering wheel sheet of servos control, and unlock transmission shaft by left and right and drive the interior motion mutually of left and right hanging point auricle, after making pilot sleeve depart from left and right hanging point auricle, canopy relies on self gravitation to sink to reaching released state, simple to operate; And, by arranging left and right torsion spring, left and right torsion spring produces torsion to left and right hanging point auricle, makes its fixing displacement that do not rotate, if there is unexpected power-off, the self-locking of canopy can be reached, and, under can be implemented in the state that steering wheel do not power on, repeatedly umbrella is filled to unmanned plane and carries out self-locking, further, under steering wheel parachute-opening moment suddenly off-position, backhaul self-locking is carried out, safe and convenient.
Accompanying drawing explanation
Fig. 1 is the schematic diagram after the present invention installs;
Fig. 2 is assembling assumption diagram of the present invention.
Detailed description of the invention
Below in conjunction with the drawings and specific embodiments, the present invention is described in detail.
Present embodiments provide the quick parachute-opening umbrella cabin structure of a kind of unmanned plane, as depicted in figs. 1 and 2, the quick parachute-opening umbrella cabin structure 102 of unmanned plane is arranged on the fuselage 101 of unmanned plane, wherein, it is inner that cabin, umbrella cabin body 103 embeds the fuselage 101 being fixed on unmanned plane, and canopy is arranged on the surface of unmanned aerial vehicle body.
Wherein, the quick parachute-opening umbrella cabin structure of unmanned plane comprises cabin, umbrella cabin body 103 and canopy 111, wherein, cabin, umbrella cabin body 103 is provided with a steering wheel mounting bracket 104, steering wheel mounting bracket can be arranged on the inner side of cabin, umbrella cabin body, and, steering wheel mounting bracket 104 is installed with a steering wheel 105, steering wheel 105 is connected with two-way steering wheel sheet 108, two-way steering wheel sheet 108 is connected with left hanging point auricle 106 and right hanging point auricle 107 respectively, wherein, left hanging point auricle 106 is connected with two-way steering wheel sheet 108 by left unblock transmission shaft 114, right hanging point auricle 107 is connected with two-way steering wheel sheet 108 by right unblock transmission shaft 115, on the left of parachute-opening leading section on canopy and right side is all installed and is provided with pilot sleeve 110, each pilot sleeve 110 is all undertaken being fixed on canopy 111 by a screw 109, and, the parachute-opening rearward end of canopy 111 is also provided with one group of lug boss 112, the shape of one group of hole clipping 113 that one group of lug boss 112 and cabin, umbrella cabin body 103 are arranged, size and position one_to_one corresponding are arranged, so, when locking, the parachute-opening rearward end of canopy 111 is snapped in by one group of lug boss 112 correspondence that it is arranged in one group of hole clipping 113 of setting on cabin, umbrella cabin body 103, and, the parachute-opening leading section of canopy is arranged on by its fixed installation that the pilot sleeve 110 of the left and right sides is corresponding respectively to be hung on the hangers of left hanging point auricle 106 and right hanging point auricle 107, complete its auto-lock function.
And, when steering wheel 105 is energized, two-way steering wheel sheet 108 is controlled by steering wheel 105, driven by two-way steering wheel sheet 108 and rotate, thus left hanging point auricle 106 and right hanging point auricle 107 inward direction are distorted motion, i.e. left hanging point auricle 106 end motion to the right, the end motion left of right hanging point auricle 107, thus making the pilot sleeve 110 of canopy left and right sides depart from left hanging point auricle 106 and right hanging point auricle 107, canopy relies on self gravitation to sink to reaching released state.
Or, left hanging point auricle 106 is also fixed on steering wheel mounting bracket 104 by a left torsion spring 116, and, right hanging point auricle 107 is also fixed on steering wheel mounting bracket by a right torsion spring 117, left torsion spring 116 can produce a torsion to left hanging point auricle 106, make its fixing displacement that do not rotate, right hanging point auricle 107 can produce a torsion to right torsion spring 117, makes its fixing displacement that do not rotate.
So, if there is unexpected power-off, the torsion of the right torsion spring of left torsion spring 116 117 can be strained left hanging point auricle 106 and right hanging point auricle 107, thus reach the self-locking of canopy, so, under can be implemented in the state that steering wheel do not power on, repeatedly umbrella is filled to unmanned plane and carries out self-locking, further, under steering wheel parachute-opening moment suddenly off-position, backhaul self-locking is carried out.
These are only preferred embodiment of the present invention, be not limited to the present invention, all any amendments done within the spirit and principles in the present invention, equivalent replacement and improvement etc., all should be included within protection scope of the present invention.
Claims (4)
1. the quick parachute-opening umbrella cabin structure of unmanned plane, is characterized in that:
Comprise umbrella cabin cabin body and canopy, wherein, cabin, umbrella cabin body is provided with a steering wheel mounting bracket, two-way steering wheel sheet steering wheel mounting bracket is installed with a steering wheel, being connected with steering wheel, and the left hanging point auricle be connected with two-way steering wheel sheet respectively and right hanging point auricle;
Wherein, left hanging point auricle is connected with two-way steering wheel sheet by left unblock transmission shaft, and right hanging point auricle is connected with two-way steering wheel sheet by right unblock transmission shaft;
Canopy is also fixedly installed respectively the pilot sleeve for fixedly hanging over left hanging point auricle and right hanging point auricle, each pilot sleeve is fixed on canopy by screw.
2. the quick parachute-opening umbrella cabin structure of unmanned plane according to claim 1, it is characterized in that: left hanging point auricle is also fixed on steering wheel mounting bracket by a left torsion spring, further, right hanging point auricle is also fixed on steering wheel mounting bracket by a right torsion spring.
3. the quick parachute-opening umbrella cabin structure of unmanned plane according to claim 1, it is characterized in that: each pilot sleeve is fixed on the parachute-opening leading section of canopy, the parachute-opening rearward end of canopy is also provided with one group of lug boss, and cabin, umbrella cabin body is provided with one group of hole clipping corresponding to position.
4., according to the arbitrary described quick parachute-opening umbrella cabin structure of unmanned plane of claim 1-3, it is characterized in that: cabin, umbrella cabin body embeds the fuselage interior being fixed on unmanned plane.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510774088.7A CN105292495B (en) | 2015-11-13 | 2015-11-13 | A kind of quick parachute-opening umbrella cabin structure of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510774088.7A CN105292495B (en) | 2015-11-13 | 2015-11-13 | A kind of quick parachute-opening umbrella cabin structure of unmanned plane |
Publications (2)
| Publication Number | Publication Date |
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| CN105292495A true CN105292495A (en) | 2016-02-03 |
| CN105292495B CN105292495B (en) | 2018-01-05 |
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| CN201510774088.7A Active CN105292495B (en) | 2015-11-13 | 2015-11-13 | A kind of quick parachute-opening umbrella cabin structure of unmanned plane |
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| CN (1) | CN105292495B (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818993A (en) * | 2016-04-29 | 2016-08-03 | 湖北易瓦特科技股份有限公司 | Unmanned aerial vehicle with detaching structure |
| CN110654553A (en) * | 2018-06-29 | 2020-01-07 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle steering wheel mechanism of opening umbrella |
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| CN201287829Y (en) * | 2008-10-30 | 2009-08-12 | 航宇救生装备有限公司 | Parachute assembly suitable for rocket |
| US20100108817A1 (en) * | 2008-11-05 | 2010-05-06 | Fox Jr Roy L | Parachute release system and method |
| CN202609087U (en) * | 2012-05-03 | 2012-12-19 | 西安大地测绘工程有限责任公司 | Downward dropping type flexible-connection cabin cover parachute-opening device of push-back type mini-sized pilotless plane |
| CN104260892A (en) * | 2014-09-30 | 2015-01-07 | 浙江工业大学之江学院 | Electric control separation mechanism of unmanned aerial vehicle and parachute |
| CN204095635U (en) * | 2014-09-15 | 2015-01-14 | 中国兵器工业计算机应用技术研究所 | A kind of depopulated helicopter catch gear |
| CN205113723U (en) * | 2015-11-13 | 2016-03-30 | 深圳飞马机器人科技有限公司 | Unmanned aerial vehicle is with quick parachute -opening umbrella cabin structure |
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2015
- 2015-11-13 CN CN201510774088.7A patent/CN105292495B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201287829Y (en) * | 2008-10-30 | 2009-08-12 | 航宇救生装备有限公司 | Parachute assembly suitable for rocket |
| US20100108817A1 (en) * | 2008-11-05 | 2010-05-06 | Fox Jr Roy L | Parachute release system and method |
| CN202609087U (en) * | 2012-05-03 | 2012-12-19 | 西安大地测绘工程有限责任公司 | Downward dropping type flexible-connection cabin cover parachute-opening device of push-back type mini-sized pilotless plane |
| CN204095635U (en) * | 2014-09-15 | 2015-01-14 | 中国兵器工业计算机应用技术研究所 | A kind of depopulated helicopter catch gear |
| CN104260892A (en) * | 2014-09-30 | 2015-01-07 | 浙江工业大学之江学院 | Electric control separation mechanism of unmanned aerial vehicle and parachute |
| CN205113723U (en) * | 2015-11-13 | 2016-03-30 | 深圳飞马机器人科技有限公司 | Unmanned aerial vehicle is with quick parachute -opening umbrella cabin structure |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818993A (en) * | 2016-04-29 | 2016-08-03 | 湖北易瓦特科技股份有限公司 | Unmanned aerial vehicle with detaching structure |
| CN110654553A (en) * | 2018-06-29 | 2020-01-07 | 海鹰航空通用装备有限责任公司 | Unmanned aerial vehicle steering wheel mechanism of opening umbrella |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105292495B (en) | 2018-01-05 |
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Address after: 518000, 13th Floor, Building A4, Nanshan Zhiyuan, No. 1001 Xueyuan Avenue, Changyuan Community, Taoyuan Street, Nanshan District, Shenzhen, Guangdong Province Patentee after: Shenzhen Pegasus Robotics Co.,Ltd. Country or region after: China Address before: 518000, 1st Floor, 16th Building, Zhiheng Industrial Park, Nantou Street, Nanshan District, Shenzhen City, Guangdong Province Patentee before: SHENZHEN FEIMA ROBOTICS Co.,Ltd. Country or region before: China |