CN203946278U - The parachuting umbrella cabin of unmanned plane - Google Patents
The parachuting umbrella cabin of unmanned plane Download PDFInfo
- Publication number
- CN203946278U CN203946278U CN201420311190.4U CN201420311190U CN203946278U CN 203946278 U CN203946278 U CN 203946278U CN 201420311190 U CN201420311190 U CN 201420311190U CN 203946278 U CN203946278 U CN 203946278U
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- Prior art keywords
- umbrella
- umbrella cabin
- parachute
- cabin
- cover plate
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Abstract
The utility model relates to a kind of parachuting umbrella cabin of unmanned plane, comprises the umbrella cabin that is installed on body top, in umbrella cabin, install parachute and be connected with parachute draw umbrella, the lower end of parachute is connected with body by many ropes; Described umbrella cabin is with cover plate, and cover plate is connected with umbrella cabin side plate by electromagnetic lock and elastic axis; The medial surface of described cover plate is with drawing with described the connection structure that umbrella is connected; The side in described umbrella cabin is with the guide channel consistent with described rope number; On described body with the buckle of described cover plate clamping.Umbrella cabin device of the present utility model, in the top of body, has been avoided the reversing that in traditional umbrella cabin, parachute is opened rear body, has improved safety in utilization; Adopt connection structure to realize drawing the tractive of umbrella, realize easily parachute and open, it is easy and simple to handle, reliable; Umbrella arranges guide channel on cabin, avoids the winding between rope, has further improved the unlatching reliability of parachute.
Description
Technical field
The utility model relates to the parachuting recovery technology field of unmanned plane, relates in particular to the parachuting umbrella cabin of unmanned plane.
Background technology
Unmanned plane is a kind of unmanned vehicle of being handled by radio robot or self process controller, is widely used in military and civilian occasion.
The parachute landing recovery device of unmanned plane is for protection unmanned plane, while preventing aircraft landing, damages.The parachute landing recovery device of existing unmanned plane is to rely on the device for ejecting in umbrella cabin that parachute is ejected and opened, and the shortcoming of its existence is: umbrella cabin device is in the bottom of body, and body requirement reversing after parachute starts, easily causes the damage of internal body separating device; The complex structure of the device for ejecting in umbrella cabin, manufacturing cost is higher, and because needs support whole umbrella body, when device for ejecting work, reliability is not high; The rope that connects body after parachute starts is prone to wrapping phenomena, causes parachute normally to open, thereby loses protective effect.
Utility model content
The applicant, for the above-mentioned shortcoming of prior art, provides a kind of parachuting umbrella cabin of unmanned plane, and it can open parachute easily, has improved functional reliability, and has feature simple in structure, cost is low.
The technical scheme that the utility model adopts is as follows:
A parachuting umbrella cabin for unmanned plane, comprises the umbrella cabin being installed on body, in umbrella cabin, install parachute and be connected with parachute draw umbrella, the lower end of parachute is connected with body by many ropes,
Described umbrella cabin device is in the top of body, and umbrella cabin is with cover plate, and one end of cover plate is connected with umbrella cabin side plate by electromagnetic lock, and the other end is realized elastic rotation by elastic axis with umbrella cabin and is connected; The medial surface of described cover plate is with drawing with described the connection structure that umbrella is connected;
The side in described umbrella cabin is with the guide channel consistent with described rope number.
Further improvement as technique scheme:
Described connection structure is VELCRO;
Described connection structure is elastic clip;
Described as connection structure be arranged at as described in the opening end front portion of cover plate;
On described body with the buckle of described cover plate clamping.
The beneficial effects of the utility model are as follows:
Umbrella cabin device of the present utility model, in the top of body, has been avoided the reversing that in traditional umbrella cabin, parachute is opened rear body, has improved safety in utilization; Adopt VELCRO or elastic clip to realize drawing the tractive of umbrella, realize easily parachute and open, it is easy and simple to handle, reliable; The guide channel of rope is set on umbrella cabin, avoids the winding between rope, further improved the unlatching reliability of parachute.The utlity model has advantage simple in structure, cost is low, safe.
Brief description of the drawings
Fig. 1 is main TV structure schematic diagram of the present utility model.
Fig. 2 is the birds-eye view of Fig. 1.
Fig. 3 and Fig. 4 are working state schematic representation of the present utility model.
In figure: 1, body; 2, umbrella cabin; 21, cover plate; 22, guide channel; 3, parachute; 4, draw umbrella;
5, connection structure; 6, electromagnetic lock; 7, rope; 8, buckle; 9, elastic axis.
Detailed description of the invention
Below in conjunction with accompanying drawing, detailed description of the invention of the present utility model is described.
As shown in Figures 1 to 4, the parachuting umbrella cabin of the unmanned plane of the present embodiment, comprise the umbrella cabin 2 that is installed on body 1 top, in umbrella cabin 2, install parachute 3 and be connected with parachute 3 draw umbrella 4, the lower end of parachute 3 is connected with body 1 by many ropes 7, umbrella cabin 2 is with cover plate 21, and one end of cover plate 21 is connected with umbrella cabin 2 side plates by electromagnetic lock 6, and the other end is realized elastic rotation by elastic axis 9 with umbrella cabin 2 and is connected; The medial surface of cover plate 21 with the connection structure 5 of drawing umbrella 4 and being connected, connection structure 5 can realize drawing and between umbrella 4 and cover plate 21, realize pull type and be connected, connection structure 5 can be the structure such as VELCRO, elastic clip; In order to prevent that parachute 3 from strutting the winding of rope 7 in process, the side in umbrella cabin 2 is with the guide channel 22 consistent with rope 7 numbers, and parachute 3 struts in process, and rope 7 scatters to surrounding along guide channel 22;
After cover plate 21 is opened, cover plate 21 180 degree that pivot under the effect of elastic axis 9, for avoiding the swing of cover plate 21, on body 1 with the buckle 8 of cover plate 21 clampings.
When the utility model uses, in the time that unmanned plane need to land, automatically open electromagnetic lock 6, the cover plate 21 in umbrella cabin 2 is automatically opened under the effect of elastic axis 9, cover plate 21 is opened after certain angle, cover plate 21 and the pulling force drawing between umbrella 4 constantly increase finally disengaging between the two, buckle 8 clampings after cover plate 21 continues rotation and on body 1; Draw umbrella 4 and pull in the process that parachute 3 struts, the rope 7 between parachute 3 and body 1 opens along the guide channel 22 in umbrella cabin 2, finally realizes the normal unlatching of parachute 3.
In the utility model, electromagnetic lock 6 is prior art.
More than describing is to explanation of the present utility model, is not the restriction to utility model, and the utility model limited range is referring to claim, and without prejudice to spirit of the present utility model in the situation that, the utility model can be done any type of amendment.
Claims (5)
1. the parachuting umbrella cabin of a unmanned plane, comprise the umbrella cabin (2) being installed on body (1), in umbrella cabin (2) device parachute (3) and be connected with parachute (3) draw umbrella (4), the lower end of parachute (3) is connected with body (1) by many ropes (7), it is characterized in that:
Described umbrella cabin (2) is installed on the top of body (1), umbrella cabin (2) is with cover plate (21), one end of cover plate (21) is connected with umbrella cabin (2) side plate by electromagnetic lock (6), and the other end is realized elastic rotation by elastic axis (9) with umbrella cabin (2) and is connected; The medial surface of described cover plate (21) is with drawing with described the connection structure (5) that umbrella (4) is connected;
The side in described umbrella cabin (2) is with the guide channel (22) consistent with described rope (7) number.
2. the parachuting umbrella cabin of unmanned plane as claimed in claim 1, is characterized in that: described connection structure (5) is VELCRO.
3. the parachuting umbrella cabin of unmanned plane as claimed in claim 1, is characterized in that: described connection structure (5) is elastic clip.
4. the parachuting umbrella cabin of the unmanned plane as described in above-mentioned arbitrary claim, is characterized in that: described connection structure (5) is arranged at the opening end front portion of described cover plate (21).
5. the parachuting umbrella cabin of unmanned plane claimed in claim 1, is characterized in that: described body (1) upper with the buckle (8) of described cover plate (21) clamping.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420311190.4U CN203946278U (en) | 2014-06-11 | 2014-06-11 | The parachuting umbrella cabin of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201420311190.4U CN203946278U (en) | 2014-06-11 | 2014-06-11 | The parachuting umbrella cabin of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203946278U true CN203946278U (en) | 2014-11-19 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201420311190.4U Expired - Fee Related CN203946278U (en) | 2014-06-11 | 2014-06-11 | The parachuting umbrella cabin of unmanned plane |
Country Status (1)
| Country | Link |
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| CN (1) | CN203946278U (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104691788A (en) * | 2015-01-23 | 2015-06-10 | 北京空间机电研究所 | Pop-up parachute capable of realizing self-adaptive equilibrium |
| CN104986339A (en) * | 2015-06-10 | 2015-10-21 | 浙江空行飞行器技术有限公司 | Unmanned aerial vehicle capable of being prevented from being crashed |
| CN105387771A (en) * | 2015-11-26 | 2016-03-09 | 中国航空工业集团公司沈阳飞机设计研究所 | Hiding structure for drone aircraft parachute lanyards |
| CN106081125A (en) * | 2016-08-24 | 2016-11-09 | 广州朱雀航空科技有限公司 | A kind of parachute construction of unmanned plane |
| CN107514185A (en) * | 2017-07-08 | 2017-12-26 | 西北工业大学 | A kind of unmanned plane umbrella hatchcover automatic-opening mechanism |
| CN109279033A (en) * | 2018-09-28 | 2019-01-29 | 谢垚峰 | A kind of forest fire monitoring unmanned plane electromagnetism limit abandoning umbrella device |
| CN109353519A (en) * | 2018-12-06 | 2019-02-19 | 中国科学院工程热物理研究所 | Unmanned plane parachuting Emergency recovery system |
-
2014
- 2014-06-11 CN CN201420311190.4U patent/CN203946278U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104691788A (en) * | 2015-01-23 | 2015-06-10 | 北京空间机电研究所 | Pop-up parachute capable of realizing self-adaptive equilibrium |
| CN104986339A (en) * | 2015-06-10 | 2015-10-21 | 浙江空行飞行器技术有限公司 | Unmanned aerial vehicle capable of being prevented from being crashed |
| CN105387771A (en) * | 2015-11-26 | 2016-03-09 | 中国航空工业集团公司沈阳飞机设计研究所 | Hiding structure for drone aircraft parachute lanyards |
| CN105387771B (en) * | 2015-11-26 | 2018-04-13 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of target drone umbrella rope stealth structure |
| CN106081125A (en) * | 2016-08-24 | 2016-11-09 | 广州朱雀航空科技有限公司 | A kind of parachute construction of unmanned plane |
| CN107514185A (en) * | 2017-07-08 | 2017-12-26 | 西北工业大学 | A kind of unmanned plane umbrella hatchcover automatic-opening mechanism |
| CN109279033A (en) * | 2018-09-28 | 2019-01-29 | 谢垚峰 | A kind of forest fire monitoring unmanned plane electromagnetism limit abandoning umbrella device |
| CN109353519A (en) * | 2018-12-06 | 2019-02-19 | 中国科学院工程热物理研究所 | Unmanned plane parachuting Emergency recovery system |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20160623 Address after: 224000. D6 building, Hi-tech Innovation Park, salt Dragon Street office, Yancheng City, Jiangsu Patentee after: DIGITAL EAGLE TECHNOLOGY DEVELOPMENT (YANCHENG) Co.,Ltd. Address before: 214000, Room 411, building A1, No. 999 High East Road, Binhu District, Wuxi, Jiangsu Patentee before: JIANGSU DIGITAL EAGLE TECHNOLOGY DEVELOPMENT Co.,Ltd. |
|
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141119 |