CN207644630U - A kind of supporting mechanism of unmanned plane - Google Patents
A kind of supporting mechanism of unmanned plane Download PDFInfo
- Publication number
- CN207644630U CN207644630U CN201721507652.XU CN201721507652U CN207644630U CN 207644630 U CN207644630 U CN 207644630U CN 201721507652 U CN201721507652 U CN 201721507652U CN 207644630 U CN207644630 U CN 207644630U
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- China
- Prior art keywords
- unmanned plane
- main body
- supporting mechanism
- flexible support
- support foot
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Abstract
The utility model discloses a kind of supporting mechanism of unmanned plane, including unmanned plane main body, the bottom of unmanned plane main body is equipped with the flexible support foot being detachably arranged, flexible support foot includes flexible support main body and detachable assembly side, and unmanned plane main body is equipped with the department of assembly to match with detachable assembly side.The supporting mechanism of the utility model can play the role of buffering, and influence of the impact force to unmanned plane internal component, extends the service life of unmanned plane when reducing unmanned plane landing.It is hardly damaged when by greater impact power, meets the needs of unmanned plane rises and falls.Supporting mechanism is replaceable, meets replacement demand.It is simple for structure ingenious, application easy to implement to promote.
Description
Technical field
The utility model is related to a kind of unmanned plane more particularly to a kind of supporting mechanisms of unmanned plane, belong to the skill of unmanned plane
Art field.
Background technology
UAV abbreviation unmanned plane, english abbreviation UAV are to utilize radio robot and the program provided for oneself
The not manned aircraft that control device manipulates.It can be divided into from technical standpoint definition：Unmanned helicopter, unmanned fixed-wing aircraft, nobody
Multi-rotor aerocraft, unmanned airship, unmanned parasol etc..
Traditional multi-rotor unmanned aerial vehicle volume is larger, the phenomenon that be easy to causeing casualties when there is aircraft bombing accident, deposits
In larger security risk.Therefore, current unmanned plane is towards miniaturization, and miniaturization has that price is low, is easy to push away
Extensively, the high advantage of security performance.
Small drone in the prior art in order to ensure cruise duration, therefore largely uses plastic casing, and supports
For foot generally by being integrally formed, the support leg intensity of injection molding is low, and there are certain impact forces for unmanned plane landing, are easy
Lead to support leg fracture damage, and be substituted for metalwork or the larger undercarriage of volume influences whether the counterweight of unmanned plane, reduces
Cruise duration, and impact force can hardness conduction, unmanned plane internal component had an impact.
Utility model content
The purpose of this utility model is to solve above-mentioned the deficiencies in the prior art, provides a kind of supporting mechanism of unmanned plane.
In order to achieve the above object, technical solution used by the utility model is：
A kind of supporting mechanism of unmanned plane, including unmanned plane main body,
The bottom of the unmanned plane main body is equipped with the flexible support foot being detachably arranged, and the flexible support foot includes flexibility
Supportive body and detachable assembly side, the unmanned plane main body are equipped with the department of assembly to match with the detachable assembly side.
Preferably, the detachable assembly side includes being oriented to inserting column and limiting groove.
Preferably, the guiding inserting column is taper guide post, and the bottom of the taper guide post is equipped with guide and limit portion.
Preferably, the top of the flexible support main body is equipped with positive stop lug boss, and the limiting groove is set to the limit
Between boss and the guide and limit portion.
Preferably, the section of the flexible support main body is triangular in shape or class triangle.
Preferably, the alien invasion of the flexible support main body is equipped with groove.
Preferably, the unmanned plane is four wing unmanned planes, and the arbitrary wing bottom of the unmanned plane is equipped with the flexible branch
Spike.
The beneficial effects of the utility model are mainly reflected in：
1. the supporting mechanism can play the role of buffering, impact force is to unmanned plane internal component when reducing unmanned plane landing
Influence, extend the service life of unmanned plane.
2. being hardly damaged when by greater impact power, meets the needs of unmanned plane rises and falls.
3. supporting mechanism is replaceable, meet replacement demand.
4. simple for structure ingenious, application easy to implement to promote.
Description of the drawings
Fig. 1 is a kind of configuration schematic diagram of the supporting mechanism of unmanned plane of the utility model.
Fig. 2 is the overall structure diagram of unmanned plane in the utility model.
Specific implementation mode
The utility model provides a kind of supporting mechanism of unmanned plane.Below in conjunction with attached drawing to technical solutions of the utility model into
Row detailed description, so that it is more readily understood and grasps.
A kind of supporting mechanism of unmanned plane, as depicted in figs. 1 and 2, including unmanned plane main body 1, the bottom of unmanned plane main body 1
Equipped with the flexible support foot 2 being detachably arranged, which is made of the material of more excellent elasticity, such as silica gel, rubber
Include flexible support main body 3 and detachable assembly side 4 Deng, flexible support foot 2, unmanned plane main body 1 is equipped with and detachable assembly
The department of assembly 5 that end 4 matches.
It specifically describes, is mainly used in four wing unmanned planes, the arbitrary wing bottom of unmanned plane is equipped with flexible support foot 2.
The flexible support foot 2 is detachably set to uav bottom, plays supporting role when unmanned plane rises and falls.It is well known that nobody
Machine can have larger impact force when landing, and use flexible support foot 2 that can play certain cushioning effect, prevent hardness shock pair
Component inside unmanned plane has an impact, in addition, structure flexible is not easily damaged, service life is long.Even if there is damage,
Also the replacement of flexible support foot 2 can be realized by detachable assembly side 4.
Refinement description is carried out to detachable assembly side 4 comprising be oriented to inserting column 6 and limiting groove 7, the guiding inserting column
6 are oriented to convenient for the loading of flexible support foot 2, and the limiting groove 7 increases for the limit between flexible support foot 2 and department of assembly 5
The stability and reliability for adding the two to be coupled.
In preferred embodiment, guiding inserting column 6 is taper guide post, and the bottom of taper guide post is equipped with guide and limit portion 8.
Pine to tight guiding can be played by the taper surface and guide and limit portion 8 of the taper guide post to be coupled, assembly is transitional good, and flexible
The top of supportive body 3 is equipped with positive stop lug boss 9, and limiting groove 7 is set between positive stop lug boss 9 and guide and limit portion 8, and limit is recessed
Slot 7, positive stop lug boss 9, guide and limit portion 8 match so that being coupled between flexible support foot 2 and department of assembly 5 more stable.
The section of the flexible support main body 3 is triangular in shape or class triangle, the structure of triangle are more stable.And flexible support
The alien invasion 31 of main body 3 is equipped with groove 10.The groove 10 can increase the elasticity of flexible support main body, be convenient for the buffering of landing,
In addition, having the characteristics of good appearance, moreover it is possible to reduce weight.
By foregoing description, the supporting mechanism of the utility model can play the role of buffering, be rushed when reducing unmanned plane landing
Influence of the power to unmanned plane internal component is hit, the service life of unmanned plane is extended.Not rapid wear when by greater impact power
It is bad, meet the needs of unmanned plane rises and falls.Supporting mechanism is replaceable, meets replacement demand.It is simple for structure ingenious, it is easy to implement to promote
Using.
The technical solution of the utility model is fully described above, it should be noted that the tool of the utility model
Body embodiment is simultaneously not limited by the description set out above, and those skilled in the art exist according to the Spirit Essence of the utility model
All technical solutions that structure, method or function etc. are formed using equivalents or equivalent transformation, all fall within this reality
Within novel protection domain.
Claims (7)
1. a kind of supporting mechanism of unmanned plane, including unmanned plane main body, it is characterised in that：
The bottom of the unmanned plane main body is equipped with the flexible support foot being detachably arranged, and the flexible support foot includes flexible support
Main body and detachable assembly side, the unmanned plane main body are equipped with the department of assembly to match with the detachable assembly side.
2. a kind of supporting mechanism of unmanned plane according to claim 1, it is characterised in that：The detachable assembly side includes
It is oriented to inserting column and limiting groove.
3. a kind of supporting mechanism of unmanned plane according to claim 2, it is characterised in that：The guiding inserting column is taper
Guide post, and the bottom of the taper guide post is equipped with guide and limit portion.
4. a kind of supporting mechanism of unmanned plane according to claim 3, it is characterised in that：The top of the flexible support main body
Portion is equipped with positive stop lug boss, and the limiting groove is set between the positive stop lug boss and the guide and limit portion.
5. a kind of supporting mechanism of unmanned plane according to claim 1, it is characterised in that：The flexible support main body is cut
Face is triangular in shape or class triangle.
6. a kind of supporting mechanism of unmanned plane according to claim 5, it is characterised in that：Outside the flexible support main body
Facade is equipped with groove.
7. a kind of supporting mechanism of unmanned plane according to claim 1, it is characterised in that：The unmanned plane be four wings nobody
The arbitrary wing bottom of machine, the unmanned plane is equipped with the flexible support foot.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721507652.XU CN207644630U (en) | 2017-11-13 | 2017-11-13 | A kind of supporting mechanism of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201721507652.XU CN207644630U (en) | 2017-11-13 | 2017-11-13 | A kind of supporting mechanism of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN207644630U true CN207644630U (en) | 2018-07-24 |
Family
ID=62889153
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201721507652.XU Active CN207644630U (en) | 2017-11-13 | 2017-11-13 | A kind of supporting mechanism of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN207644630U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109229347A (en) * | 2018-09-20 | 2019-01-18 | 芜湖星禾无人机科技有限公司 | A kind of novel unmanned plane |
-
2017
- 2017-11-13 CN CN201721507652.XU patent/CN207644630U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109229347A (en) * | 2018-09-20 | 2019-01-18 | 芜湖星禾无人机科技有限公司 | A kind of novel unmanned plane |
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