CN205770152U - A kind of mounting structure of unmanned plane oar - Google Patents
A kind of mounting structure of unmanned plane oar Download PDFInfo
- Publication number
- CN205770152U CN205770152U CN201620490113.9U CN201620490113U CN205770152U CN 205770152 U CN205770152 U CN 205770152U CN 201620490113 U CN201620490113 U CN 201620490113U CN 205770152 U CN205770152 U CN 205770152U
- Authority
- CN
- China
- Prior art keywords
- oar
- unmanned plane
- mounting part
- mounting structure
- damping gasket
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
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- Vibration Prevention Devices (AREA)
Abstract
This utility model relates to the mounting structure of a kind of unmanned plane oar, including unmanned plane oar, described unmanned plane oar has mounting part, and described mounting part is provided with fixed installation hole, and the upper surface of described mounting part and lower surface are fixed with oar clamp device by a damping gasket respectively.This utility model is by fixing with oar clamp device by a damping gasket respectively with lower surface at the upper surface of the mounting part of unmanned plane oar, can farthest decrease the motion abrasion of oar, improve the life-span of oar and aircraft, the elasticity simultaneously solving oar is difficult to grasp, and pine or tension excessively all easily causes the shake even technical problem of air crash of aircraft.
Description
Technical field
This utility model belongs to unmanned air vehicle technique field, is specifically related to the mounting structure of a kind of unmanned plane oar.
Background technology
Unmanned plane is militarily and civil area has the biggest application, and the installation of current unmanned plane oar exists
Railway Project, the elasticity of oar is difficult to grasp, and crosses pine or tension all easily causes the shake of aircraft even
Air crash, therefore provides the mounting structure of a kind of novel unmanned plane oar, necessary.
Utility model content
The purpose of this utility model is to solve above-mentioned technical problem and provide a kind of novel unmanned plane
The mounting structure of oar.
For achieving the above object, this utility model adopts the following technical scheme that
The mounting structure of a kind of unmanned plane oar, including unmanned plane oar, it is fixing that described unmanned plane oar has installation
Portion, described mounting part is provided with fixed installation hole, the upper surface of described mounting part and lower surface
Fixed with oar clamp device by a damping gasket respectively.
The hole corresponding with described fixed installation hole it is preset with in described damping gasket.
Described damping gasket uses polytetrafluoro damping gasket.
This utility model is passed through with lower surface respectively by the upper surface of the mounting part at unmanned plane oar
One damping gasket is fixed with oar clamp device, can farthest decrease the motion abrasion of oar, improve
In the life-span of oar and aircraft, the elasticity simultaneously solving oar is difficult to grasp, and crosses pine or tension is the easiest
Cause the shake even technical problem of air crash of aircraft.
Accompanying drawing explanation
Fig. 1 is the structural representation of the mounting structure of unmanned plane oar.
Detailed description of the invention
Below, in conjunction with example, substantive distinguishing features of the present utility model and advantage are further described, but
This utility model is not limited to listed embodiment.
Shown in Figure 1, the mounting structure of a kind of unmanned plane oar, including unmanned plane oar 1, described unmanned
Machine oar has mounting part 11, and described mounting part is provided with fixed installation hole 12, described installation
The upper surface of fixed part and lower surface are fixed with oar clamp device by a damping gasket respectively.
Wherein, the upper surface at described mounting part is provided with the first damping gasket 21, and lower surface is provided with
Two damping gasket 20.
Wherein, each described damping gasket is preset with the hole 22 corresponding with described fixed installation hole.
Concrete, during this is novel, described damping gasket uses polytetrafluoro damping gasket.
Oar clamp device is included in folder 30 and lower folder 31, and upper folder 30 is provided with drive shaft hole 33 and oar
Fixing hole 32, the structure of lower folder is identical with upper clamping structure.
This utility model is passed through with lower surface respectively by the upper surface of the mounting part at unmanned plane oar
One damping gasket is fixed with oar clamp device, can farthest decrease the motion abrasion of oar, improve
In the life-span of oar and aircraft, the elasticity simultaneously solving oar is difficult to grasp, and crosses pine or tension is the easiest
Cause the shake even technical problem of air crash of aircraft.
The above is only preferred implementation of the present utility model, it is noted that for the art
Those of ordinary skill for, on the premise of without departing from this utility model principle, it is also possible to make some
Improvements and modifications, these improvements and modifications also should be regarded as protection domain of the present utility model.
Claims (3)
1. the mounting structure of a unmanned plane oar, it is characterised in that include unmanned plane oar, described unmanned
Machine oar has mounting part, and described mounting part is provided with fixed installation hole, and described installation is fixed
The upper surface in portion and lower surface are fixed with oar clamp device by a damping gasket respectively.
The mounting structure of unmanned plane oar the most according to claim 1, it is characterised in that described damping
The hole corresponding with described fixed installation hole it is preset with on pad.
The mounting structure of unmanned plane oar the most according to claim 1 or claim 2, it is characterised in that described
Damping gasket uses polytetrafluoro damping gasket.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620490113.9U CN205770152U (en) | 2016-05-25 | 2016-05-25 | A kind of mounting structure of unmanned plane oar |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620490113.9U CN205770152U (en) | 2016-05-25 | 2016-05-25 | A kind of mounting structure of unmanned plane oar |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN205770152U true CN205770152U (en) | 2016-12-07 |
Family
ID=58111245
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620490113.9U Expired - Fee Related CN205770152U (en) | 2016-05-25 | 2016-05-25 | A kind of mounting structure of unmanned plane oar |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN205770152U (en) |
-
2016
- 2016-05-25 CN CN201620490113.9U patent/CN205770152U/en not_active Expired - Fee Related
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CP01 | Change in the name or title of a patent holder |
Address after: 300270 Tianjin Binhai New Area, Dagang seaside street, red flag Road south side of bungalow 7. Patentee after: Tianjin City tianxiang Hongyu Technology Co. Ltd. Address before: 300270 Tianjin Binhai New Area, Dagang seaside street, red flag Road south side of bungalow 7. Patentee before: TIANJIN HONGYU TIANXIANG TECHNOLOGY CO., LTD. |
|
| CP01 | Change in the name or title of a patent holder | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20161207 Termination date: 20210525 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |