CN215475687U - Unmanned aerial vehicle head shell turns over a structure - Google Patents
Unmanned aerial vehicle head shell turns over a structure Download PDFInfo
- Publication number
- CN215475687U CN215475687U CN202121857108.4U CN202121857108U CN215475687U CN 215475687 U CN215475687 U CN 215475687U CN 202121857108 U CN202121857108 U CN 202121857108U CN 215475687 U CN215475687 U CN 215475687U
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- hinge
- head shell
- seat
- fixed
- pin chain
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Abstract
The utility model discloses an unmanned aerial vehicle head shell turnover structure, which is characterized in that: including fixed pin chain seat, head shell connecting pin chain seat, hinge and spring catch, the fuselage is connected to fixed pin chain seat, hinge seat connecting head shell is connected to the head shell, fixed pin chain seat is connected to the one end of hinge, and hinge seat is connected to other end connecting head shell, the spring catch sets up the lateral part of fixed hinge seat, spring catch under natural state its outer end protrusion just can support partial hinge in the side of fixed hinge seat, make head shell connecting hinge seat turn over with fixed hinge seat and turn over and open, under the compression state, stretch out and draw back in fixed hinge seat, its holding power or the resistance that produces the hinge cancel, make fixed pin chain seat and head shell connecting pin chain seat lock. When the unmanned aerial vehicle is inspected or installed, the head shell of the unmanned aerial vehicle can be turned over, so that the operation space is enlarged.
Description
Technical Field
The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle head shell turnover structure.
Background
Most unmanned aerial vehicle's head shell and fuselage all are fixed connection or integrated into one piece at present, and operating space is little when carrying out equipment inspection and installation to fuselage inside like this, and is very unchangeable.
SUMMERY OF THE UTILITY MODEL
In order to solve the problems, the utility model provides an unmanned aerial vehicle head shell turnover structure, which is used for turning a head shell of an unmanned aerial vehicle open during inspection or installation, so that the operation space is enlarged.
The technical scheme of the utility model is as follows:
the utility model provides an unmanned aerial vehicle head shell turns over a structure which characterized in that: including fixed pin chain seat, head shell connecting pin chain seat, hinge and spring catch, the fuselage is connected to fixed pin chain seat, hinge seat connecting head shell is connected to the head shell, fixed pin chain seat is connected to the one end of hinge, and hinge seat is connected to other end connecting head shell, the spring catch sets up the lateral part of fixed hinge seat, spring catch under natural state its outer end protrusion just can support partial hinge in the side of fixed hinge seat, make head shell connecting hinge seat and the fixed hinge seat of fuselage turn over and open, under the compression state, stretch out and draw back in fixed hinge seat, make its holding power or resistance to the hinge production cancel.
Furthermore, the hinge comprises a first hinge knuckle, a second hinge knuckle and a hinge pin, the first hinge knuckle is arranged on the fixed hinge base, the second hinge knuckle is fixed on the head shell connecting hinge base, and the first hinge knuckle and the second hinge knuckle are rotatably connected through the hinge pin.
Further, a wear-resistant spacer is arranged between the first hinge joint and the second hinge joint and is in contact with the first hinge joint and the second hinge joint through the wear-resistant spacer.
The utility model has the beneficial effects that: unmanned aerial vehicle can turn over unmanned aerial vehicle's head-cover and open when inspection or installation, has enlarged operating space.
Drawings
FIG. 1 is a schematic view of an open configuration of the present invention;
fig. 2 is a development use state diagram of the present invention.
Detailed Description
The present invention will be described in detail below with reference to the accompanying drawings in conjunction with embodiments. It should be noted that the features of the following embodiments and examples may be combined with each other without conflict.
As shown in fig. 1 and 2, an unmanned aerial vehicle head shell turns over a structure, including fixed pin chain seat 1, head shell connecting pin chain seat 2, hinge 3 and spring pin 4, the fuselage is connected to fixed pin chain seat 1, 2 connecting head shells of hinge seat are connected to the head shell, fixed pin chain seat 1 is connected to the one end of hinge 3, and hinge seat 2 is connected to other end connecting head shell, spring pin 4 sets up the lateral part of fixed hinge seat 1, spring pin 4 its outer end protrusion under natural state just can support partial hinge in the side of fixed hinge seat 1, makes head shell connecting hinge seat 2 turn over with fixed hinge seat 1 and opens, under compression state, stretches out and draws back in fixed hinge seat 1, makes its holding power or the resistance that produces hinge 3 cancel.
The hinge 3 of the present embodiment includes a first hinge knuckle 31, a second hinge knuckle 32 and a hinge pin 33, the first hinge knuckle 31 is disposed on the fixed hinge base 1, the second hinge knuckle 32 is fixed on the head shell connecting hinge base 2, and the first hinge knuckle 31 and the second hinge knuckle 32 are rotatably connected by the hinge pin 33. The hinge pin 33 can be movably connected with the first hinge joint and the second hinge joint respectively, can also be fixedly connected with one hinge joint and movably connected with the other hinge joint, and the requirements can be met as long as the fixed hinge seat connected with the first hinge joint and the head shell connecting hinge seat connected with the second hinge joint can realize relative rotation. The first hinge joint of the embodiment is fixed on the fixed hinge seat and comprises two first installation pieces 31a which are parallel and arranged at intervals, two hinge pin holes are respectively arranged on the two first installation pieces, the second hinge joint comprises two second installation pieces 32a which are respectively arranged at two sides of the two first installation pieces and are fixedly connected with the hinge seat connected with the head shell, two insertion holes are respectively arranged on the two second installation pieces, the positions of the two insertion holes are opposite to the two hinge pin holes, and the hinge pin is sequentially inserted into the insertion holes, the hinge pin holes and the insertion holes from the side part, so that the four installation pieces are connected in series.
To sum up, when the head shell upturning position exceeded the spring pinhole, the spring catch can pop out automatically, withstood head shell connection hinge seat, the head shell will keep the open mode this moment, can also prevent that the head shell from dropping and influencing the operation, when needs closed head shell, only need press into the fixed hinge seat of fuselage with the handle spring catch, the head shell can reply, the rebound that the spring catch had been blocked to head shell connection hinge seat inner wall simultaneously, realize convenient opening and shutting for operation sight space grow has made things convenient for inspection and the installation of head equipment.
The above embodiments are merely representative of the centralized embodiments of the present invention, and the description thereof is specific and detailed, but it should not be understood as the limitation of the scope of the present invention, and it should be noted that those skilled in the art can make various changes and modifications without departing from the spirit of the present invention, and these changes and modifications all fall into the protection scope of the present invention. Therefore, the protection scope of the present patent should be subject to the appended claims.
Claims (3)
1. The utility model provides an unmanned aerial vehicle head shell turns over a structure which characterized in that: including fixed pin chain seat, head shell connecting pin chain seat, hinge and spring catch, the fuselage is connected to fixed pin chain seat, hinge seat connecting head shell is connected to the head shell, fixed pin chain seat is connected to the one end of hinge, and hinge seat is connected to other end connecting head shell, the spring catch sets up the lateral part of fixed pin chain seat, spring catch under natural state its outer end protrusion just can support partial hinge in the side of fixed hinge seat, make head shell connecting hinge seat turn over with fixed hinge seat and turn over and open, under the compression state, stretch out and draw back in fixed hinge seat, its holding power or the resistance that produces the hinge cancel, make fixed pin chain seat and head shell connecting pin chain seat lock.
2. The unmanned aerial vehicle head shell turn-over structure of claim 1, characterized in that: the hinge comprises a first hinge joint, a second hinge joint and a hinge pin, wherein the first hinge joint is arranged on the fixed hinge base, the second hinge joint is fixed on the head shell connecting hinge base, and the first hinge joint and the second hinge joint are rotationally connected through the hinge pin.
3. The unmanned aerial vehicle head shell turn-over structure of claim 2, characterized in that: and a wear-resistant spacer is arranged between the first hinge joint and the second hinge joint and is contacted with the first hinge joint and the second hinge joint through the wear-resistant spacer.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121857108.4U CN215475687U (en) | 2021-08-10 | 2021-08-10 | Unmanned aerial vehicle head shell turns over a structure |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202121857108.4U CN215475687U (en) | 2021-08-10 | 2021-08-10 | Unmanned aerial vehicle head shell turns over a structure |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN215475687U true CN215475687U (en) | 2022-01-11 |
Family
ID=79757734
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202121857108.4U Active CN215475687U (en) | 2021-08-10 | 2021-08-10 | Unmanned aerial vehicle head shell turns over a structure |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN215475687U (en) |
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2021
- 2021-08-10 CN CN202121857108.4U patent/CN215475687U/en active Active
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CB03 | Change of inventor or designer information | ||
| CB03 | Change of inventor or designer information |
Inventor after: Tang Zhiyang Inventor after: Li Zhao Inventor after: Wang Jiangping Inventor before: Tang Zhiyang Inventor before: Li Zhao Inventor before: Wang Jiangping Inventor before: Deng Zhenzhen Inventor before: Tang Yiheng |
|
| TR01 | Transfer of patent right | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20230105 Address after: 519000 unit 101, building 2, No.1, Keji 7th Road, Tangjiawan Town, high tech Zone, Zhuhai City, Guangdong Province Patentee after: ZHUHAI ZIYAN UNMANNED AERIAL VEHICLE CO.,LTD. Address before: 519000 unit 203, building 1, No.1, Keji 7th Road, Tangjiawan Town, high tech Zone, Zhuhai City, Guangdong Province Patentee before: Zhuhai Ziyan New Technology Co.,Ltd. |