CN203753393U - Double-door release device of unmanned aerial vehicle - Google Patents
Double-door release device of unmanned aerial vehicle Download PDFInfo
- Publication number
- CN203753393U CN203753393U CN201320869919.5U CN201320869919U CN203753393U CN 203753393 U CN203753393 U CN 203753393U CN 201320869919 U CN201320869919 U CN 201320869919U CN 203753393 U CN203753393 U CN 203753393U
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- Prior art keywords
- cabin
- release device
- double
- door
- steering engine
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Abstract
The utility model discloses a double-door release device of an unmanned aerial vehicle. The double-door release device comprises a cabin of which one surface is open; two sides of the open end of the cabin are respectively and movably connected with cabin doors through hinges; a steering engine is arranged on one side of the cabin; the steering engine is connected with a pull rod; one ends of the two cabin doors are respectively connected with connecting rods; the two connecting rods are connected to one end of the pull rod together. According to the double-door release device, the problems that a conventional release device is complicated and cargoes easily leak are solved. The double-door release device has the advantages that stress of a cabin door opening/closing structure is greatly reduced, an original operation mode of controlling low-load cabin doors by a large steering engine is improved into an operation mode of controlling high-load cabin doors by a small steering engine, the structure weight and part weight brought by the complicated cabin door opening/closing structure are reduced, and the cabin door opening release flexibility and rapidness of the unmanned aerial vehicle are improved.
Description
Technical field
The utility model belongs to unmanned plane equipment technical field, is specifically related to a kind of unmanned plane double door delivery device.
Background technology
The current information age, unmanned plane is widely used in every field, but by aircraft own wt limit and delivery device loaded down with trivial details and unreliable, throw in volume of compartment easily awing because all little reasons go wrong, such as wind-force in-flight has pressure to hatch door, door-down switch insufficient strength and occur seriously missing goods, likely wrap up door-down switch structure, even wrap up, occurs unexpected.
Utility model content
The purpose of this utility model is to provide a kind of unmanned plane double door delivery device, has solved existing delivery device loaded down with trivial details and easily miss the problem of goods.
The technical scheme that the utility model adopts is: unmanned plane double door delivery device, comprise the cabin body of an opening, and the both sides of the open end of cabin body are connected with hatch door by loose-leaf respectively, and a side of cabin body is provided with steering wheel, and steering wheel is connected with pull bar; One end of two hatch doors is respectively arranged with pipe link, and two pipe links are connected to one end of pull bar jointly.
The beneficial effects of the utility model are: unmanned plane double door delivery device of the present utility model has reduced the stressed of door-down switch structure greatly, original little load hatch door of large steering wheel control is promoted to and controls heavy load hatch door with little steering wheel, reduce because of the loaded down with trivial details structural weight bringing of door-down switch structure and pts wt, increased unmanned plane open the cabin alerting ability and the rapidity of throwing in.
Brief description of the drawings
Fig. 1 is the structural representation of unmanned plane double door delivery device of the present utility model.
In figure, 1. cabin body, 2. steering wheel, 3. pull bar, 4. hatch door, 5. pipe link.
Detailed description of the invention
Below in conjunction with accompanying drawing and detailed description of the invention, the utility model is elaborated.
The utility model provides a kind of unmanned plane double door delivery device, as shown in Figure 1, comprises the cabin body 1 of an opening, and the both sides of the open end of cabin body 1 are connected with hatch door 4 by loose-leaf respectively, and a side of cabin body 1 is provided with steering wheel 2, and steering wheel 2 is connected with pull bar 3; One end of two hatch doors 4 is respectively arranged with 5, two pipe links 5 of pipe link and is jointly connected to one end of pull bar 3.
When use, after steering wheel 2 receives the signal of unmanned plane, start half-twist, now pull bar 3 moves along with the rotation of steering wheel 2, and the mobile of pull bar 2 drives two pipe links 5 to move together, and the motion of pipe link 5 is opened hatch door or be closed.
By the way, unmanned plane double door delivery device of the present utility model, has solved existing delivery device loaded down with trivial details and easily miss the problem of goods.Unmanned plane double door delivery device of the present utility model has reduced the stressed of door-down switch structure greatly, original little load hatch door of large steering wheel control is promoted to and controls heavy load hatch door with little steering wheel, reduce because of the loaded down with trivial details structural weight bringing of door-down switch structure and pts wt, increased unmanned plane open the cabin alerting ability and the rapidity of throwing in.
Claims (1)
1. unmanned plane double door delivery device, comprise the cabin body (1) of an opening, the both sides of the open end of described cabin body (1) are connected with hatch door (4) by loose-leaf respectively, one side of described cabin body (1) is provided with steering wheel (2), and described steering wheel (2) is connected with pull bar (3); One end of two hatch doors (4) is respectively arranged with pipe link (5), and described two pipe links (5) are connected to one end of described pull bar (3) jointly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320869919.5U CN203753393U (en) | 2013-12-24 | 2013-12-24 | Double-door release device of unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320869919.5U CN203753393U (en) | 2013-12-24 | 2013-12-24 | Double-door release device of unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203753393U true CN203753393U (en) | 2014-08-06 |
Family
ID=51248695
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320869919.5U Expired - Fee Related CN203753393U (en) | 2013-12-24 | 2013-12-24 | Double-door release device of unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203753393U (en) |
Cited By (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104648684A (en) * | 2014-12-23 | 2015-05-27 | 哈尔滨蒙鹰科技有限公司 | Small-sized unmanned aerial vehicle (UAV) hoisting equipment and hoisting method |
| CN104857726A (en) * | 2015-03-26 | 2015-08-26 | 王长民 | Remote control aircraft for dispersing articles |
| CN105046835A (en) * | 2015-08-26 | 2015-11-11 | 广州极飞电子科技有限公司 | Goods receiving method and device and goods delivery method and system |
| CN106005360A (en) * | 2016-07-20 | 2016-10-12 | 海鹰航空通用装备有限责任公司 | Small unmanned aerial vehicle openable-closeable cabin door load lifting mechanism |
| CN106114866A (en) * | 2016-07-28 | 2016-11-16 | 顺丰科技有限公司 | Unmanned plane cargo hold |
| CN106314796A (en) * | 2016-09-01 | 2017-01-11 | 肇庆高新区异星科技有限公司 | Ejection device |
| CN106741733A (en) * | 2016-12-30 | 2017-05-31 | 哈瓦国际航空技术（深圳）有限公司 | A kind of lifebuoy carry and unmanned plane of jettisoninging by several times |
| CN107600439A (en) * | 2017-09-26 | 2018-01-19 | 上海重塑能源科技有限公司 | A kind of long endurance unmanned aircraft electrical source of power device and unmanned plane |
| CN108313295A (en) * | 2018-03-28 | 2018-07-24 | 湖南星思科技有限公司 | A kind of unmanned plane delivery device and its control method |
-
2013
- 2013-12-24 CN CN201320869919.5U patent/CN203753393U/en not_active Expired - Fee Related
Cited By (13)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104648684A (en) * | 2014-12-23 | 2015-05-27 | 哈尔滨蒙鹰科技有限公司 | Small-sized unmanned aerial vehicle (UAV) hoisting equipment and hoisting method |
| CN104648684B (en) * | 2014-12-23 | 2018-01-12 | 哈尔滨蒙鹰科技有限公司 | Small-sized unmanned aircraft hanging device and the method lifted |
| CN104857726A (en) * | 2015-03-26 | 2015-08-26 | 王长民 | Remote control aircraft for dispersing articles |
| CN105046835A (en) * | 2015-08-26 | 2015-11-11 | 广州极飞电子科技有限公司 | Goods receiving method and device and goods delivery method and system |
| CN106005360A (en) * | 2016-07-20 | 2016-10-12 | 海鹰航空通用装备有限责任公司 | Small unmanned aerial vehicle openable-closeable cabin door load lifting mechanism |
| CN106005360B (en) * | 2016-07-20 | 2017-12-29 | 海鹰航空通用装备有限责任公司 | SUAV can be opened and closed hatch door load lift mechanism |
| CN106114866B (en) * | 2016-07-28 | 2019-02-01 | 顺丰科技有限公司 | Unmanned plane cargo hold |
| CN106114866A (en) * | 2016-07-28 | 2016-11-16 | 顺丰科技有限公司 | Unmanned plane cargo hold |
| CN106314796A (en) * | 2016-09-01 | 2017-01-11 | 肇庆高新区异星科技有限公司 | Ejection device |
| CN106741733A (en) * | 2016-12-30 | 2017-05-31 | 哈瓦国际航空技术（深圳）有限公司 | A kind of lifebuoy carry and unmanned plane of jettisoninging by several times |
| CN106741733B (en) * | 2016-12-30 | 2018-12-11 | 哈瓦国际航空技术（深圳）有限公司 | A kind of gradation is jettisoninged lifebuoy carry and unmanned plane |
| CN107600439A (en) * | 2017-09-26 | 2018-01-19 | 上海重塑能源科技有限公司 | A kind of long endurance unmanned aircraft electrical source of power device and unmanned plane |
| CN108313295A (en) * | 2018-03-28 | 2018-07-24 | 湖南星思科技有限公司 | A kind of unmanned plane delivery device and its control method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| 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: 20140806 Termination date: 20161224 |