CN206243493U - A kind of shock resistance structure of multi-purpose unmanned aerial vehicle - Google Patents
A kind of shock resistance structure of multi-purpose unmanned aerial vehicle Download PDFInfo
- Publication number
- CN206243493U CN206243493U CN201621315846.5U CN201621315846U CN206243493U CN 206243493 U CN206243493 U CN 206243493U CN 201621315846 U CN201621315846 U CN 201621315846U CN 206243493 U CN206243493 U CN 206243493U
- Authority
- CN
- China
- Prior art keywords
- casing
- assembly cavity
- metal clips
- aerial vehicle
- shock resistance
- 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
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Abstract
The utility model discloses a kind of shock resistance structure of multi-purpose unmanned aerial vehicle, including unmanned body, easily hitting position and offer assembly cavity on unmanned body, assembly cavity is inserted into installing a removable beam, the beam includes a casing, casing is inserted in assembly cavity, its end face outside opening, and openend is sealed by a metal clips；Bayonet connection is installed between the medial surface of metal clips and the bottom surface of assembly cavity, a support member is respectively mounted between two bayonet connections being oppositely arranged, a radiator shutter is also equipped with casing bottom surface, the radiator shutter is fixedly installed on the bottom surface of casing by base, it is provided with a rotatable rotating shaft between base, and radiator shutter is just set to the openend of casing.The utility model simple structure, the light weight of whole beam is conveniently detachable, and the installation with unmanned body is very convenient, reduces the impact to unmanned plane after clashing into, and saves the maintenance cost of unmanned plane, increases thermal diffusivity.
Description
Technical field
The utility model is related to unmanned plane field, and in particular to a kind of shock resistance structure of multi-purpose unmanned aerial vehicle.
Background technology
As the application of unmanned plane is more and more wider, requirement to unmanned plane also more and more higher.Unmanned plane passes through Remote,
In the air during flight, there is contingency unavoidably and the shock with building or ground occurs, during collision, unmanned body bears
Main impulsive force, therefore occur and be badly damaged, the substantial amounts of cost of maintenance needs.
The content of the invention
Technical problem to be solved in the utility model is to provide a kind of conveniently detachable replacing, reduces the damage after clashing into
Lose, can increase thermal diffusivity, greatly increase unmanned plane shock resistance multi-purpose unmanned aerial vehicle shock resistance structure.
The utility model is achieved through the following technical solutions：A kind of shock resistance structure of multi-purpose unmanned aerial vehicle, bag
Unmanned body is included, the position of easily hitting on unmanned body offers assembly cavity, and assembly cavity is inserted into installing a removable anticollision
Device, the beam includes a casing, and casing is inserted in assembly cavity, its end face outside opening, and openend passes through a metal elastic
Piece is sealed；
Bayonet connection is installed between the medial surface of metal clips and the bottom surface of assembly cavity, two for being oppositely arranged buckle
A support member is respectively mounted between connector, a radiator shutter is also equipped with casing bottom surface, the radiator shutter is solid by base
Surely it is arranged on the bottom surface of casing, it is provided with a rotatable rotating shaft between base, and radiator shutter is just to casing
Openend set.
Used as preferred technical scheme, the support member is made of elastomeric material, and its internal filling is hollow, and fills
There is gas.
Used as preferred technical scheme, the metal clips is metal mesh sheet, its domed shape, the outer ring tool of metal clips
There is connecting portion, connecting portion is completed to be assembled with the detachable of casing openend by screw thread, and the arc convex surface of metal clips is protruded from
The end face outside of casing.
Used as preferred technical scheme, the inwall of the casing is provided with the ventilation communicated with unmanned internal body space
Hole, casing is made of titanium alloy material.
The beneficial effects of the utility model are：The utility model simple structure, the light weight of whole beam can conveniently be torn open
Dress, the installation with unmanned body is very convenient, reduces the impact to unmanned plane after clashing into, and saves the maintenance cost of unmanned plane, increases
Plus thermal diffusivity.
Brief description of the drawings
In order to illustrate more clearly of the utility model embodiment or technical scheme of the prior art, below will be to embodiment
Or the accompanying drawing to be used needed for description of the prior art is briefly described, it should be apparent that, drawings in the following description are only
It is some embodiments of the present utility model, for those of ordinary skill in the art, is not paying the premise of creative work
Under, other accompanying drawings can also be obtained according to these accompanying drawings.
Fig. 1 is overall structure diagram of the present utility model.
Specific embodiment
All features disclosed in this specification, or disclosed all methods or during the step of, except mutually exclusive
Feature and/or step beyond, can combine by any way.
Any feature disclosed in this specification (including any accessory claim, summary and accompanying drawing), except non-specifically is chatted
State, can alternative features equivalent by other or with similar purpose replaced.I.e., unless specifically stated otherwise, each feature
It is an example in a series of equivalent or similar characteristics.
As shown in figure 1, including unmanned body 9, on unmanned body 9 easily hitting position offers assembly cavity, assembly cavity interpolation
Enter and a removable beam is installed, beam includes a casing 2, and casing 2 is inserted in assembly cavity, and its end face outside is opened
Mouthful, openend is sealed by a metal clips 5；
Bayonet connection 3 is installed, two for being oppositely arranged card between the medial surface of metal clips 5 and the bottom surface of assembly cavity
A support member 7 is respectively mounted between snap connector 3, a radiator shutter 1 is also equipped with the bottom surface of casing 2, radiator shutter 1 passes through base
4 are fixedly installed on the bottom surface of casing 2, and it is provided with a rotatable rotating shaft between base 4, and radiator shutter 1 is just
Openend to casing 2 is set.
Originally in implementing, support member 7 is made of elastomeric material, and its internal filling is hollow, and filled with gas, due to
Using the support member 7 of hollow design, internal filling air again, therefore quality is very light, when being clashed into, metal clips becomes
Shape, extrudes the support member of rear end, and support member is filled with air due to inside, therefore support member can deform, but after removing power, meeting again
Restore to the original state, light weight will not excessively influence the heavy burden of unmanned plane.
Metal clips 5 is metal mesh sheet, and its domed shape, the outer ring of metal clips 5 has connecting portion 6, and connecting portion 6 passes through
Screw thread completes to be assembled with the detachable of the openend of casing 2, and the arc convex surface of metal clips 5 protrudes from the end face outside of casing 2, when
When metal clips 5 is subject to impact, can be caved inward in the metal clips of arc convex surface shape originally, the circular arc in opposite direction is recessed
Planar, but it can again be ejected by with the pressing of finger after clashing into, it is very convenient.
In addition, the inwall of casing 2 is provided with the air-vent 8 communicated with the inner space of unmanned body 9, casing 2 is closed using titanium
Golden material is made, and the quality of whole casing 2 is very light, and heavy burden is substantially reduced, and sets air-vent 8, when flight, radiating
Blade 1 can be rotated with the relative motion of air-flow, and the radiator shutter 1 of rotation can carry out the change of current, one to the air in casing 2
Determine to help unmanned plane quick heat radiating in degree, but also dependent on the lower radiator shutter of needs dismounting.
The beneficial effects of the utility model are：The utility model simple structure, the light weight of whole beam can conveniently be torn open
Dress, the installation with unmanned body is very convenient, reduces the impact to unmanned plane after clashing into, and saves the maintenance cost of unmanned plane, increases
Plus thermal diffusivity.
The above, specific embodiment only of the present utility model, but protection domain of the present utility model do not limit to
In this, any change or replacement expected without creative work should all be covered within protection domain of the present utility model.
Therefore, protection domain of the present utility model should be determined by the scope of protection defined in the claims.
Claims (4)
1. a kind of shock resistance structure of multi-purpose unmanned aerial vehicle, it is characterised in that：Including unmanned body, easily portion is hit on unmanned body
Position offers assembly cavity, and assembly cavity is inserted into installing a removable beam, and the beam includes a casing, and casing is inserted
Enter in assembly cavity, its end face outside opening, openend is sealed by a metal clips；
Bayonet connection is installed between the medial surface of metal clips and the bottom surface of assembly cavity, two for being oppositely arranged snap connection
A support member is respectively mounted between part, a radiator shutter is also equipped with casing bottom surface, the radiator shutter is fixed by base and set
It is placed on the bottom surface of casing, it is provided with a rotatable rotating shaft between base, radiator shutter is just opened casing
Mouth end is set.
2. the shock resistance structure of multi-purpose unmanned aerial vehicle as claimed in claim 1, it is characterised in that：The support member uses rubber
Material is made, and its internal filling is hollow, and filled with gas.
3. the shock resistance structure of multi-purpose unmanned aerial vehicle as claimed in claim 1, it is characterised in that：The metal clips is metal
Mesh sheet, its domed shape, the outer ring of metal clips has connecting portion, and connecting portion completes the dismounting with casing openend by screw thread
Formula is assembled, and the arc convex surface of metal clips protrudes from the end face outside of casing.
4. the shock resistance structure of multi-purpose unmanned aerial vehicle as claimed in claim 1, it is characterised in that：The inwall of the casing is set
The air-vent that being and not being human organism inner space communicates, casing is made of titanium alloy material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621315846.5U CN206243493U (en) | 2016-12-02 | 2016-12-02 | A kind of shock resistance structure of multi-purpose unmanned aerial vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621315846.5U CN206243493U (en) | 2016-12-02 | 2016-12-02 | A kind of shock resistance structure of multi-purpose unmanned aerial vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206243493U true CN206243493U (en) | 2017-06-13 |
Family
ID=59004827
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621315846.5U Expired - Fee Related CN206243493U (en) | 2016-12-02 | 2016-12-02 | A kind of shock resistance structure of multi-purpose unmanned aerial vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206243493U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110271657A (en) * | 2019-07-05 | 2019-09-24 | 智飞智能装备科技东台有限公司 | A kind of shock resistance unmanned plane plastic shell |
-
2016
- 2016-12-02 CN CN201621315846.5U patent/CN206243493U/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110271657A (en) * | 2019-07-05 | 2019-09-24 | 智飞智能装备科技东台有限公司 | A kind of shock resistance unmanned plane plastic shell |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20170613 Termination date: 20191202 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |