CN105292495B - A kind of quick parachute-opening umbrella cabin structure of unmanned plane - Google Patents
A kind of quick parachute-opening umbrella cabin structure of unmanned plane Download PDFInfo
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- CN105292495B CN105292495B CN201510774088.7A CN201510774088A CN105292495B CN 105292495 B CN105292495 B CN 105292495B CN 201510774088 A CN201510774088 A CN 201510774088A CN 105292495 B CN105292495 B CN 105292495B
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- steering wheel
- hanging point
- canopy
- umbrella cabin
- parachute
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- 230000005540 biological transmission Effects 0.000 claims abstract description 8
- 238000009434 installation Methods 0.000 claims description 5
- 239000007787 solid Substances 0.000 claims 1
- 238000006073 displacement reaction Methods 0.000 description 3
- 238000010586 diagram Methods 0.000 description 2
- 230000005611 electricity Effects 0.000 description 2
- 230000002950 deficient Effects 0.000 description 1
- 238000003780 insertion Methods 0.000 description 1
- 230000037431 insertion Effects 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
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Abstract
The invention discloses a kind of unmanned plane with quick parachute-opening umbrella cabin structure, including umbrella cabin nacelle and canopy, wherein, umbrella cabin nacelle is provided with a steering wheel mounting bracket, the two-way steering wheel piece for a steering wheel is installed with steering wheel mounting bracket, being connected with steering wheel, and the left hanging point auricle being connected respectively with two-way steering wheel piece and right hanging point auricle；Wherein, left hanging point auricle is connected by left unblock power transmission shaft with two-way steering wheel piece, and right hanging point auricle is connected by right unblock power transmission shaft with two-way steering wheel piece；Also it is fixedly installed on canopy and is fixed on for the fixed pilot sleeve for hanging over left hanging point auricle and right hanging point auricle, each pilot sleeve by screw on canopy respectively.After the present invention installs parachute under not power supply state, unmanned plane can be simple to operate with auto lock, also, when running into emergency situations or task is completed to need parachuting, automatically can open canopy and complete the parachuting of unmanned plane, safe and convenient.
Description
Technical field
The present invention relates to unmanned machine equipment, more particularly to a kind of quick parachute-opening umbrella cabin structure of unmanned plane.
Background technology
Conventional unmanned plane parachute deployment means can leak outside part, and can not ensure smooth parachute-opening, can not be in steering wheel not
It is upper electricity in the state of carry out repeatedly dress umbrella and carry out self-locking, can not be carried out under steering wheel parachute-opening moment unexpected off-position backhaul certainly
Lock.
Therefore, the prior art is defective, it is necessary to improve.
The content of the invention
The technical problems to be solved by the invention are：One kind is provided under not power supply state after installation parachute, unmanned plane
Can be simple to operate with auto lock, also, when running into emergency situations or task is completed to need parachuting, can be automatically by canopy
Open and complete the parachuting of unmanned plane, the quick parachute-opening umbrella cabin structure of the unmanned plane of safe and convenient.
Technical scheme is as follows：A kind of unmanned plane quick parachute-opening umbrella cabin structure, including umbrella cabin nacelle and canopy,
Wherein, umbrella cabin nacelle is provided with a steering wheel mounting bracket, is installed with a steering wheel in steering wheel mounting bracket, is connected with steering wheel
Two-way steering wheel piece, and the left hanging point auricle being connected respectively with two-way steering wheel piece and right hanging point auricle；Wherein, left hanging point auricle leads to
Cross left unblock power transmission shaft to be connected with two-way steering wheel piece, right hanging point auricle is connected by right unblock power transmission shaft with two-way steering wheel piece；Umbrella
Cover also to be fixedly installed respectively and lead to for the fixed pilot sleeve for hanging over left hanging point auricle and right hanging point auricle, each pilot sleeve
Screw is crossed to be fixed on canopy.
Applied to above-mentioned technical proposal, with quick parachute-opening umbrella cabin structure, left hanging point auricle also passes through described unmanned plane
One left torsion spring is fixed in steering wheel mounting bracket, also, right hanging point auricle is also fixed on steering wheel by a right torsion spring
In mounting bracket.
Applied to each above-mentioned technical proposal, described unmanned plane with quick parachute-opening umbrella cabin structure, pacify by each pilot sleeve
Dress is fixed on the parachute-opening leading section of canopy, and the parachute-opening rearward end of canopy is additionally provided with one group of lug boss, and umbrella cabin nacelle is provided with position
One group of hole clipping corresponding to putting.
Applied to each above-mentioned technical proposal, with quick parachute-opening umbrella cabin structure, umbrella cabin nacelle is embedded in described unmanned plane
It is fixed on the fuselage interior of unmanned plane.
Using such scheme, the present invention unlocks power transmission shaft by left and right and drives left and right by the two-way steering wheel piece of servos control
Moved in hanging point auricle phase, after pilot sleeve is departed from left and right hanging point auricle, canopy sinks to reaching unblock shape by self gravitation
State, it is simple to operate；Also, by setting left and right torsion spring, left and right torsion spring produces torsion to left and right hanging point auricle, it is fixed not
Rotate displacement, if there is unexpected power-off, can reach the self-locking of canopy, and it is possible to realize steering wheel not on it is electric
Under state, repeatedly dress umbrella is carried out to unmanned plane and carries out self-locking, also, is returned under steering wheel parachute-opening moment unexpected off-position
Cheng Zisuo, safe and convenient.
Brief description of the drawings
Fig. 1 is the schematic diagram after present invention installation；
Fig. 2 is the assembling assumption diagram of the present invention.
Embodiment
Below in conjunction with the drawings and specific embodiments, the present invention is described in detail.
A kind of quick parachute-opening umbrella cabin structure of unmanned plane is present embodiments provided, as depicted in figs. 1 and 2, unmanned plane is with soon
Fast parachute-opening umbrella cabin structure 102 is arranged on the fuselage 101 of unmanned plane, wherein, the insertion of umbrella cabin nacelle 103 is fixed on unmanned plane
Fuselage 101 inside, canopy is arranged on the surface of unmanned aerial vehicle body.
Wherein, unmanned plane includes umbrella cabin nacelle 103 and canopy 111 with quick parachute-opening umbrella cabin structure, wherein, umbrella cabin nacelle
103 are provided with a steering wheel mounting bracket 104, and steering wheel mounting bracket can be arranged on the inner side of umbrella cabin nacelle, also, steering wheel
A steering wheel 105 is installed with mounting bracket 104, steering wheel 105 is connected with two-way steering wheel piece 108, two-way steering wheel piece 108 is distinguished
Be connected with left hanging point auricle 106 and right hanging point auricle 107, wherein, left hanging point auricle 106 by left unblock power transmission shaft 114 with it is double
Connected to steering wheel piece 108, right hanging point auricle 107 is connected by right unblock power transmission shaft 115 with two-way steering wheel piece 108, on canopy
On the left of parachute-opening leading section and right side is respectively mounted and is provided with pilot sleeve 110, and each pilot sleeve 110 is entered by a screw 109
Row is fixed on canopy 111；Also, the parachute-opening rearward end of canopy 111 is additionally provided with one group of lug boss 112, one group raised
Shape, the size and location of one group hole clipping 113 of the portion 112 with being set in umbrella cabin nacelle 103, which correspond, to be set, in this way, locking
When tight, one group of lug boss 112 that the parachute-opening rearward end of canopy 111 is set by it is correspondingly caught in what is set in umbrella cabin nacelle 103
In one group of hole clipping 113, also, the parachute-opening leading section of canopy is arranged on the pilot sleeve 110 of the left and right sides by its fixed installation
Correspond to and hung on the hangers of left hanging point auricle 106 and right hanging point auricle 107 respectively, complete its auto-lock function.
Also, when steering wheel 105 is powered, two-way steering wheel piece 108 is controlled by steering wheel 105, passes through the two-way band of steering wheel piece 108
Turn is moved, the motion so that left hanging point auricle 106 and the right inward direction of hanging point auricle 107 are distorted, i.e., left hanging point auricle 106
End motion to the right, the right end motion to the left of hanging point auricle 107, so that the pilot sleeve 110 of canopy left and right sides departs from left hanging point ear
Piece 106 and right hanging point auricle 107, canopy sink to reaching released state by self gravitation.
Or left hanging point auricle 106 is also fixed in steering wheel mounting bracket 104 by a left torsion spring 116, also,
Right hanging point auricle 107 is also fixed in steering wheel mounting bracket by a right torsion spring 117, and left torsion spring 116 can be to left hanging point
Auricle 106 produces a torsion, it is fixed the displacement that do not rotate, and right hanging point auricle 107 can produce to right torsion spring 117
One torsion, it is set to fix the displacement that do not rotate.
In this way, if there is unexpected power-off, the torsion of the left right torsion spring 117 of torsion spring 116 can be left hanging point auricle 106 and right extension
Point auricle 107 tenses, so as to reach the self-locking of canopy, so, it is possible to achieve steering wheel not in the state of electricity, unmanned plane is entered
Row repeatedly dress umbrella and progress self-locking, also, backhaul self-locking is carried out under steering wheel parachute-opening moment unexpected off-position.
These are only presently preferred embodiments of the present invention, be not intended to limit the invention, it is all the present invention spirit and
All any modification, equivalent and improvement made within principle etc., should be included in the scope of the protection.
Claims (3)
- A kind of 1. quick parachute-opening umbrella cabin structure of unmanned plane, it is characterised in that：Including umbrella cabin nacelle and canopy, wherein, umbrella cabin nacelle is provided with a steering wheel mounting bracket, and peace is fixed in steering wheel mounting bracket The two-way steering wheel piece being connected equipped with a steering wheel, with steering wheel, and the left hanging point auricle being connected respectively with two-way steering wheel piece and right extension Point auricle, left hanging point auricle are fixed in steering wheel mounting bracket by a left torsion spring, and right hanging point auricle passes through a right torsion spring It is fixed in steering wheel mounting bracket；Wherein, left hanging point auricle is connected by left unblock power transmission shaft with two-way steering wheel piece, and right hanging point auricle is driven by right unblock Axle is connected with two-way steering wheel piece；Also it is fixedly installed respectively on canopy for the fixed pilot sleeve for hanging over left hanging point auricle and right hanging point auricle, it is each to be oriented to Sleeve is fixed on canopy by screw；Also, each pilot sleeve by a screw be fixed on canopy；In locking, one group of lug boss that the parachute-opening rearward end of canopy is set by it is correspondingly caught in set in the nacelle of umbrella cabin one In group hole clipping, also, the pilot sleeve that the parachute-opening leading section of canopy is arranged on the left and right sides by its fixed installation corresponds to respectively On the hangers for hanging over left hanging point auricle and right hanging point auricle, and its auto-lock function is completed by left torsion spring and right torsion spring.
- 2. the quick parachute-opening umbrella cabin structure of unmanned plane according to claim 1, it is characterised in that：Each pilot sleeve installation is solid The parachute-opening leading section of canopy is scheduled on, the parachute-opening rearward end of canopy is additionally provided with one group of lug boss, and umbrella cabin nacelle is provided with position pair The one group of hole clipping answered.
- 3. according to the quick parachute-opening umbrella cabin structure of any described unmanned planes of claim 1-2, it is characterised in that：Umbrella cabin nacelle is embedding Enter to be fixed on the fuselage interior of 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 |
|---|---|
| CN105292495A CN105292495A (en) | 2016-02-03 |
| CN105292495B true CN105292495B (en) | 2018-01-05 |
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| Application Number | Title | Priority Date | Filing Date |
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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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Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105818993B (en) * | 2016-04-29 | 2018-03-27 | 易瓦特科技股份公司 | Unmanned plane 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 |
Citations (5)
| 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 |
| 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 |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US8033507B2 (en) * | 2008-11-05 | 2011-10-11 | Fox Jr Roy L | Parachute release system and method |
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2015
- 2015-11-13 CN CN201510774088.7A patent/CN105292495B/en active Active
Patent Citations (5)
| 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 |
| 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 |
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| Publication number | Publication date |
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| CN105292495A (en) | 2016-02-03 |
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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 |