CN204716852U - Damping device - Google Patents
Damping device Download PDFInfo
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- CN204716852U CN204716852U CN201520042854.6U CN201520042854U CN204716852U CN 204716852 U CN204716852 U CN 204716852U CN 201520042854 U CN201520042854 U CN 201520042854U CN 204716852 U CN204716852 U CN 204716852U
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- China
- Prior art keywords
- damping device
- shock absorber
- absorber part
- pedestal
- mounting plate
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Abstract
The damping device structure of a kind of unmanned vehicle that the utility model proposes, by the shock absorber part of hollow cavity structure, the resistance that the benefit done like this makes unmanned vehicle be subject to aerial all directions in flight course can both be cancelled, simultaneously simple, easy to assembly, the device of the structure of this device itself overall comparatively gently, substantially do not affect the lifting capacity of unmanned vehicle.Improve the aesthetics of outward appearance, there is low cost, high security simultaneously, while there is shock-absorbing function, also obtain better water proof and dust proof effect, improve the reliability of aircraft entirety.
Description
Technical field
The utility model relates to a kind of damping device, particularly a kind of damping device of unmanned vehicle.
Background technique
At present, unmanned vehicle has that volume is little, lightweight, expense is low, flexible operation and the high feature of Security, can be widely used in taking photo by plane, the field such as monitoring.At present, holder for aerial photographing usually direct and unmanned vehicle combines, during operation, unmanned vehicle easily produces unstable shake under aerodynamic effect, and the dither of the rotary component such as the motor of aircraft, oar also can be passed to vidicon camera, made a video recording image quality is caused to decline (e.g., image blurring, picture distortion twisting etc.), increase the burden of later image process.
Thus, the damping device that a kind of novel unmanned vehicle is provided is necessary.
Model utility content
In order to overcome above-mentioned defect of the prior art, the utility model provides a kind of damping device with shock-absorbing function, and the damping device that simultaneously the utility model proposes also has functions of waterproof and dustproof.
For achieving the above object, the utility model adopts following technological scheme:
A kind of damping device, described damping device comprises
Pedestal, fitting seat, is characterized in that: described damping device also comprises shock absorber part, and described shock absorber part one end is connected with described pedestal, and the other end is connected with described fitting seat, and described shock absorber part is the cavity of hollow.
Preferably, described shock absorber part is set to wavy.
Preferably, described shock absorber part is made up of rubber, silica gel material.
Preferably, described pedestal with described shock absorber part joint, be provided with groove,
Described shock absorber part by with described pedestal joint be provided with the projection that matches to be connected with described pedestal and/or described mounting plate with described shock absorber part joint, be provided with groove,
Described shock absorber part is by being connected with described mounting plate being provided with described mounting plate joint the projection matched.
Preferably, described pedestal with described shock absorber part joint, be provided with fixed cover outward, and/or described mounting plate with described shock absorber part joint, be provided with fixed cover outward.Effect is connected to improve.
Preferably, described pedestal is provided with link, is connected with the body of aircraft by this link.
Further, described pedestal is provided with guide rail, is connected with aircraft and body by this guide rail.
Preferably, described pedestal is provided with several for described shock absorber part by upper and lower extrusion process, the through hole that in cavity, gas can be discharged in time.
Preferably, described mounting plate is provided with several for described shock absorber part by upper and lower extrusion process, the through hole that in cavity, gas can be discharged in time.
Preferably, described mounting plate to be connected with described shock absorber part side face on be provided with limited post.
Preferably, the described damping device side of the can be bodily form.Also can be arranged to cylinder type as required, rhombus (after yielding rubber is connected with pedestal, mounting plate, forming the obturator of hollow).
In addition, the utility model additionally provides a kind of unmanned vehicle, wherein, unmanned vehicle carries above-mentioned damping device.
Beneficial effect
The damping device structure that the utility model proposes, by the shock absorber part that cavity runs through up and down, the resistance that the benefit done like this makes unmanned vehicle be subject to aerial all directions in flight course can both be cancelled, and simultaneously simple, easy to assembly, the device entirety of the structure of this device itself is lighter.Improve the aesthetics of outward appearance, there is low cost, high security simultaneously, while there is shock-absorbing function, also obtain better water proof and dust proof effect, improve the reliability of aircraft entirety.
Accompanying drawing explanation
Below in conjunction with drawings and Examples, the utility model is further described
Fig. 1 is the overall structure schematic diagram of the utility model embodiment,
Fig. 2 is the structural representation of the utility model embodiment,
Fig. 3 is the schematic cross-section of Fig. 2 along A-A ',
Fig. 4 is the schematic cross-section of the utility model embodiment's another 1.
Embodiment
Below in conjunction with specific embodiment, such scheme is described further.Should be understood that these embodiments are not limited to for illustration of the utility model limit scope of the present utility model.The implementation condition adopted in embodiment can do further adjustment according to the condition of concrete producer, and not marked implementation condition is generally the condition in normal experiment.
Embodiment
As shown in Figure 1, be the overall schematic of the damping device carrying the utility model scheme, damping device 20 one end is connected with picture obtain device 10, and the other end is connected with aircraft (not shown).
As shown in Figure 2, be the structural representation of damping device 20, damping device 20 comprises pedestal 1, yielding rubber 2 mounting plate 3; One end of yielding rubber 2 is connected with pedestal 1, and the other end is connected with mounting plate 3.Yielding rubber 2 is arranged to the cavity of hollow, and like this, the damping device 20 after pedestal 1, yielding rubber 2, dress plate 3 connect forms approximate airtight space.
As shown in Figure 3, be the structural representation along A-A ' section of damping device 20; Pedestal 1 is provided with guide rail 11, to be connected (not shown) by this guide rail 11 with aircraft; Yielding rubber 2, by being provided with protruding 22 with one end of pedestal 1, is connected with the groove 12 pedestal 1 mating setting; Yielding rubber 2, by being provided with protruding 21 with one end of mounting plate 3, is connected with the groove 33 mounting plate 3 mating setting; Yielding rubber 2 is arranged to wavy; Mounting plate 3 is provided with interface 31, is connected with picture obtain device 10 by interface 31; Mounting plate 3 is provided with multiple through hole 32, so that yielding rubber 2 is being extruded in process, in cavity, gas can be discharged in time.Mounting plate 3 to be connected with yielding rubber 2 side face on be provided with limited post 34.This limited post 34 can adopt elastic material to make, and under abnormal conditions, yielding rubber 2 forms 2 with limited post 34 in process and heavily cushions, to improve damping effect further being extruded.
As shown in Figure 4, for the one of Fig. 3 is out of shape, difference is only: mounting plate 3 to be connected with yielding rubber 2 side face on there is no limited post.
The distortion of the scheme of above-mentioned Fig. 3 or Fig. 4, after yielding rubber 2 is connected with pedestal 1, after yielding rubber 2 is connected with mounting plate 3, sets up retainer ring outward, to improve the reliability of connection further.
In the scheme of above-mentioned Fig. 3 or Fig. 4, yielding rubber 2 can adopt silica gel or other elastic material to replace rubber.
Damping device 20 side of the being bodily form in the scheme of above-mentioned Fig. 2, also can be arranged to cylinder type as required, rhombus etc. (after yielding rubber is connected with pedestal, mounting plate, forming the obturator of hollow).
Guide rail 11 in such scheme can adopt alternate manner to be connected with aircraft.
Technique effect:
Damping device is with after aircraft and after picture obtain device is connected; damping device itself roughly forms airtight cavity; the resistance making unmanned vehicle be subject to aerial all directions in flight course can both be cancelled; this airtight cavity simultaneously; improve outside the aesthetics of outward appearance; also there is water proof and dust proof effect: protection is arranged on its internal control plate (not shown), improves the reliability of aircraft entirety.
Above-mentioned example, only for technical conceive of the present utility model and feature are described, its object is to person skilled in the art can be understood content of the present utility model and implement according to this, can not limit protection domain of the present utility model with this.All equivalent transformations of doing according to the utility model Spirit Essence or modification, all should be encompassed within protection domain of the present utility model.
Claims (10)
1. a damping device, described damping device comprises
Pedestal, fitting seat, is characterized in that:
Described damping device also comprises shock absorber part,
Described shock absorber part one end is connected with described pedestal,
The other end is connected with described fitting seat,
Described shock absorber part is the cavity of hollow.
2. damping device as claimed in claim 1, is characterized in that:
Described shock absorber part is set to wavy.
3. damping device as claimed in claim 2, is characterized in that: described shock absorber part is made up of rubber or silica gel.
4. damping device as claimed in claim 1, is characterized in that:
Described pedestal with described shock absorber part joint, be provided with groove,
Described shock absorber part by with described pedestal joint be provided with the projection that matches to be connected with described pedestal and/or described mounting plate with described shock absorber part joint, be provided with groove,
Described shock absorber part is by being connected with described mounting plate being provided with described mounting plate joint the projection matched.
5. damping device as claimed in claim 4, is characterized in that: described pedestal with described shock absorber part joint, be provided with fixed cover outward, and/or described mounting plate with described shock absorber part joint, be provided with fixed cover outward.
6. damping device as claimed in claim 1, is characterized in that: described pedestal is provided with the link be connected with aircraft and body.
7. damping device as claimed in claim 6, is characterized in that: described link is guide rail.
8. damping device as claimed in claim 1, is characterized in that: the damping device side of being build or cylinder type.
9. damping device as claimed in claim 1, is characterized in that:
Described pedestal is provided with several for described shock absorber part by upper and lower extrusion process, the through hole that in cavity, gas can be discharged in time.
10. damping device as claimed in claim 1, is characterized in that:
Described mounting plate to be connected with described shock absorber part side face on be provided with limited post.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520042854.6U CN204716852U (en) | 2015-01-21 | 2015-01-21 | Damping device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520042854.6U CN204716852U (en) | 2015-01-21 | 2015-01-21 | Damping device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204716852U true CN204716852U (en) | 2015-10-21 |
Family
ID=54315854
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520042854.6U Active CN204716852U (en) | 2015-01-21 | 2015-01-21 | Damping device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204716852U (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270646A (en) * | 2015-11-16 | 2016-01-27 | 湖南云顶智能科技有限公司 | Holder device of unmanned airplane |
| CN105539819A (en) * | 2015-12-26 | 2016-05-04 | 武汉智能鸟无人机有限公司 | Plant protection machine |
| CN107672777A (en) * | 2017-09-18 | 2018-02-09 | 深圳市道通智能航空技术有限公司 | Unmanned plane and its vibration absorber |
-
2015
- 2015-01-21 CN CN201520042854.6U patent/CN204716852U/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105270646A (en) * | 2015-11-16 | 2016-01-27 | 湖南云顶智能科技有限公司 | Holder device of unmanned airplane |
| CN105270646B (en) * | 2015-11-16 | 2018-05-01 | 湖南云顶智能科技有限公司 | Cradle head device for unmanned plane |
| CN105539819A (en) * | 2015-12-26 | 2016-05-04 | 武汉智能鸟无人机有限公司 | Plant protection machine |
| CN105539819B (en) * | 2015-12-26 | 2018-03-16 | 武汉智能鸟无人机有限公司 | A kind of fog machine |
| CN107672777A (en) * | 2017-09-18 | 2018-02-09 | 深圳市道通智能航空技术有限公司 | Unmanned plane and its vibration absorber |
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|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |