CN205549568U - Unmanned aerial vehicle's rack construction - Google Patents
Unmanned aerial vehicle's rack construction Download PDFInfo
- Publication number
- CN205549568U CN205549568U CN201620210862.1U CN201620210862U CN205549568U CN 205549568 U CN205549568 U CN 205549568U CN 201620210862 U CN201620210862 U CN 201620210862U CN 205549568 U CN205549568 U CN 205549568U
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- Prior art keywords
- horn
- frame
- tubing
- head
- rack construction
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Abstract
The utility model discloses an unmanned aerial vehicle's rack construction for the unmanned air vehicle technique field, be in including frame and symmetric distribution frame horn all around, the frame includes a plurality of frame tubular product and incites somebody to action frame tubular product matched stack frame connecting piece as an organic whole, the horn includes a plurality of quick -witted arm pipe materials, the pipe wall of frame tubular product and quick -witted arm pipe material all has at least one plane. The utility model provides a pipe wall of frame tubular product and quick -witted arm pipe material all has at least one plane to come the circular tubular product among the substituting prior art with this, the structural strength of frame tubular product and quick -witted arm pipe material is high, because the pipe wall has the plane, easily fixable is held after tightening up a screw to drilling, avoids the deformation of arc pipe wall, and the security that has also improved production efficiency and unmanned aerial vehicle has simultaneously reduced manufacturing cost.
Description
Technical field
This utility model is used for unmanned air vehicle technique field, particularly relates to the rack construction of a kind of unmanned plane.
Background technology
The rack construction of unmanned plane is as the agent structure of unmanned plane, its top is used for installing power set, bottom includes foot rest etc., and in prior art, the rack construction of unmanned plane typically uses circular pipe to assemble molding, restriction due to circular pipe own structural characteristics, make, when rack construction molding, intensity to be run into low, the problem such as easy slip, and owing to the inwall of circular pipe has radian so that screws etc. are not easy clamping or clamping rear arc tube wall can deform.
Utility model content
For solving the problems referred to above, this utility model provides a kind of structural strength high, and location is easily, it is to avoid the rack construction of the unmanned plane of arc tube wall deformation.
This utility model solves its technical problem and be the technical scheme is that the rack construction of a kind of unmanned plane, including frame and the horn being symmetrically distributed in described frame surrounding, described frame includes some frame tubing and described frame tubing is assembled the barrel coupler being integrated, described horn includes that some horn tubing, the tube wall of described frame tubing and horn tubing are respectively provided with at least one plane.
It is further used as the improvement of technical solutions of the utility model, described horn includes being respectively arranged on the head horn of described frame head, middle part and afterbody, middle part horn and afterbody horn, being positioned at the described head horn of homonymy and described middle part horn to be all articulated with on same dragging connecting rod away from one end of described frame, the tube wall of described dragging connecting rod has at least one plane.
It is further used as the improvement of technical solutions of the utility model; each described horn all includes the pivot end being articulated in frame; the pivot end of described head horn and/or middle part horn is connected with frame by rotary locking mechanism; the pivot end of described afterbody horn is connected with frame by rotary locking mechanism; described horn can draw in around pivot end or launch, and is fixed with rack locking by corresponding rotary locking mechanism when horn launches.
It is further used as the improvement of technical solutions of the utility model, described barrel coupler includes laying respectively at described frame head and the head connector of afterbody and Caudal connectors, four frame tubing it are provided with parallel between described head connector and Caudal connectors, the medium position of the two frame tubing being positioned at homonymy is provided with middle part connector, described head horn is articulated on head connector, afterbody horn is articulated on Caudal connectors, and middle part horn is articulated on the connector of middle part.
Being further used as the improvement of technical solutions of the utility model, described barrel coupler is provided with and passes for frame tubing and by profiling hole fixing for frame tubing.
Being further used as the improvement of technical solutions of the utility model, described head horn and middle part horn and be equipped with the cuff connecting described dragging connecting rod in the one end away from frame, cuff is provided with for dragging the profiling hole that connecting rod passes and fixed by dragging connecting rod.
Being further used as the improvement of technical solutions of the utility model, described frame tubing, horn tubing and dragging connecting rod are polygonal pipe.
The beneficial effects of the utility model: frame tubing and the tube wall of horn tubing in this utility model are respectively provided with at least one plane, and substitute circular pipe of the prior art with this, the structural strength of frame tubing and horn tubing is high, owing to tube wall has plane, boring is the most fixing after tightening up a screw, avoid arc tube wall deformation, also improve the safety of production efficiency and unmanned plane simultaneously, reduce production cost.
Accompanying drawing explanation
The utility model is described in further detail below in conjunction with the accompanying drawings:
Structural representation when Fig. 1 is the expansion of this utility model horn.
Detailed description of the invention
With reference to Fig. 1, that show the concrete structure of the preferred embodiment of this utility model.Will be detailed below the construction features of each element of this utility model, if and when being described direction (upper and lower, left and right, before and after), it is to describe for reference with the structure shown in Fig. 1, but actually used direction of the present utility model is not limited thereto.
This utility model provides the rack construction of a kind of unmanned plane, including frame 1 and the horn 2 being symmetrically distributed in described frame 1 surrounding, described frame 1 includes some frame tubing and described frame tubing is assembled the barrel coupler being integrated, described horn 2 includes some horn tubing, the tube wall of described frame tubing and horn tubing is respectively provided with at least one plane, described frame tubing, horn tubing are polygonal pipe, more preferably hexagon tubing.Frame tubing and the tube wall of horn tubing in this utility model are respectively provided with at least one plane, and substitute circular pipe of the prior art with this, the structural strength of frame tubing and horn tubing is high, owing to tube wall has plane, boring is the most fixing after tightening up a screw, avoid arc tube wall deformation, also improve the safety of production efficiency and unmanned plane simultaneously, reduce production cost.
Wherein, described horn 2 includes being respectively arranged on described frame 1 head, middle part and the head horn 21 of afterbody, middle part horn 22 and afterbody horn 23, it is positioned at the described head horn 21 of homonymy and described middle part horn 22 to be all articulated with on same dragging connecting rod 24 away from one end of described frame 1, the tube wall of described dragging connecting rod 24 has at least one plane, dragging connecting rod 24 is also polygonal pipe, more preferably hexagon tubing.Each described horn 2 all includes the pivot end being articulated in frame 1; the pivot end of described head horn 21 and/or middle part horn 22 is connected with frame 1 by rotary locking mechanism 3; the pivot end of described afterbody horn 23 is connected with frame 1 by rotary locking mechanism 3; described horn 2 can draw in around pivot end or launch, and is locked with frame 1 by corresponding rotary locking mechanism 3 when horn 2 launches.
Horn 2 of the present utility model uses the version of deployable gathering, exerted a force by dragging connecting rod 24 when launching horn 2, drag connecting rod 24 and drive horn so that horn 2 outwards launches, after being rotated in place, rotary locking mechanism 3(rotary locking mechanism 3 belongs to prior art and does not repeats them here) auto lock, limit horn 2 to circle round, now horn 2 can not double swerve, effectively fixed, improve stability in the large and the mechanical strength of unmanned plane, and easy to operate.When folding horn 2, discharge rotary locking mechanism 3, then drive horn 2 to fold by dragging connecting rod 24 and draw in, transport and storage space can be saved, have without the rack construction of this unmanned plane is dismantled.
As this utility model preferred embodiment, described barrel coupler includes laying respectively at described frame 1 head and the head connector 11 of afterbody and Caudal connectors 12, four frame tubing it are provided with parallel between described head connector 11 and Caudal connectors 12, the medium position of the two frame tubing being positioned at homonymy is provided with middle part connector 13, described head horn 21 is articulated on head connector 11, afterbody horn 23 is articulated on Caudal connectors 12, and middle part horn 22 is articulated on the connector 13 of middle part.Described barrel coupler is provided with and passes for frame tubing and by profiling hole fixing for frame tubing.Described head horn 21 and middle part horn 22 are equipped with the cuff 25 connecting described dragging connecting rod 24 in the one end away from frame 1, and cuff 25 is provided with and passes and will drag the fixing profiling hole of connecting rod 24 for dragging connecting rod 24.When making unmanned plane, drag the two ends of connecting rod 24 and head horn 21 and be equipped with rotor away from one end of frame 1.By rotor wing rotation, produce lift upwards, drive unmanned plane during flying of the present invention.
Certainly, the invention is not limited to above-mentioned embodiment, those of ordinary skill in the art also can make equivalent variations or replacement on the premise of this utility model spirit, and modification or the replacement of these equivalents are all contained in the application claim limited range.
Claims (7)
1. the rack construction of a unmanned plane, it is characterized in that: include frame and be symmetrically distributed in the horn of described frame surrounding, described frame includes some frame tubing and described frame tubing is assembled the barrel coupler being integrated, described horn includes that some horn tubing, the tube wall of described frame tubing and horn tubing are respectively provided with at least one plane.
The rack construction of unmanned plane the most according to claim 1, it is characterized in that: described horn includes being respectively arranged on the head horn of described frame head, middle part and afterbody, middle part horn and afterbody horn, being positioned at the described head horn of homonymy and described middle part horn to be all articulated with on same dragging connecting rod away from one end of described frame, the tube wall of described dragging connecting rod has at least one plane.
The rack construction of unmanned plane the most according to claim 2; it is characterized in that: each described horn all includes the pivot end being articulated in frame; the pivot end of described head horn and/or middle part horn is connected with frame by rotary locking mechanism; the pivot end of described afterbody horn is connected with frame by rotary locking mechanism; described horn can draw in around pivot end or launch, and is fixed with rack locking by corresponding rotary locking mechanism when horn launches.
The rack construction of unmanned plane the most according to claim 3, it is characterized in that: described barrel coupler includes laying respectively at described frame head and the head connector of afterbody and Caudal connectors, four frame tubing it are provided with parallel between described head connector and Caudal connectors, the medium position of the two frame tubing being positioned at homonymy is provided with middle part connector, described head horn is articulated on head connector, afterbody horn is articulated on Caudal connectors, and middle part horn is articulated on the connector of middle part.
The rack construction of unmanned plane the most according to claim 4, it is characterised in that: described barrel coupler is provided with and passes for frame tubing and by profiling hole fixing for frame tubing.
The rack construction of unmanned plane the most according to claim 4, it is characterized in that: described head horn and middle part horn are equipped with the cuff connecting described dragging connecting rod in the one end away from frame, cuff is provided with for dragging the profiling hole that connecting rod passes and fixed by dragging connecting rod.
7. according to the rack construction of the unmanned plane according to any one of claim 2～6, it is characterised in that: described frame tubing, horn tubing and dragging connecting rod are polygonal pipe.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620210862.1U CN205549568U (en) | 2016-03-18 | 2016-03-18 | Unmanned aerial vehicle's rack construction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620210862.1U CN205549568U (en) | 2016-03-18 | 2016-03-18 | Unmanned aerial vehicle's rack construction |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205549568U true CN205549568U (en) | 2016-09-07 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620210862.1U Expired - Fee Related CN205549568U (en) | 2016-03-18 | 2016-03-18 | Unmanned aerial vehicle's rack construction |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205549568U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106542087A (en) * | 2016-11-01 | 2017-03-29 | 顺丰科技有限公司 | A kind of frame of multi-rotor unmanned aerial vehicle |
| CN106564581A (en) * | 2016-11-01 | 2017-04-19 | 顺丰科技有限公司 | Rack of multi-rotor-ring unmanned aerial vehicle |
| CN107914877A (en) * | 2017-12-20 | 2018-04-17 | 聊城揽悦创新科技有限公司 | Three axis connecting rod unmanned planes |
| CN108583840A (en) * | 2018-01-05 | 2018-09-28 | 河南正大航空科技股份有限公司 | A kind of unmanned plane integral frame structure |
| WO2022082383A1 (en) * | 2020-10-19 | 2022-04-28 | 深圳市大疆创新科技有限公司 | Self-locking structure, arm assembly and movable platform |
-
2016
- 2016-03-18 CN CN201620210862.1U patent/CN205549568U/en not_active Expired - Fee Related
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106542087A (en) * | 2016-11-01 | 2017-03-29 | 顺丰科技有限公司 | A kind of frame of multi-rotor unmanned aerial vehicle |
| CN106564581A (en) * | 2016-11-01 | 2017-04-19 | 顺丰科技有限公司 | Rack of multi-rotor-ring unmanned aerial vehicle |
| CN106564581B (en) * | 2016-11-01 | 2020-03-27 | 顺丰科技有限公司 | Many rotor unmanned aerial vehicle's frame |
| CN106542087B (en) * | 2016-11-01 | 2023-11-28 | 丰翼科技(深圳)有限公司 | Multi-rotor unmanned aerial vehicle's frame |
| CN107914877A (en) * | 2017-12-20 | 2018-04-17 | 聊城揽悦创新科技有限公司 | Three axis connecting rod unmanned planes |
| CN108583840A (en) * | 2018-01-05 | 2018-09-28 | 河南正大航空科技股份有限公司 | A kind of unmanned plane integral frame structure |
| WO2022082383A1 (en) * | 2020-10-19 | 2022-04-28 | 深圳市大疆创新科技有限公司 | Self-locking structure, arm assembly and movable platform |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: Room 1012, 1015 and 1017, 10th floor, No. 9 Software Building, Zhongxin Road, Yuehai Street, Nanshan District, Shenzhen City, Guangdong Province Patentee after: Shenzhen Xiang Nong Creative Technology Limited Address before: 511400 Guangdong Guangzhou Panyu District Panyu Avenue North 383 (3 buildings) 1202 rooms Patentee before: TIAN-XIANG AVIATION SCIENCE AND TECHNOLOGY 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: 20160907 Termination date: 20210318 |