CN206782069U - A kind of buffer of unmanned plane - Google Patents
A kind of buffer of unmanned plane Download PDFInfo
- Publication number
- CN206782069U CN206782069U CN201720695679.XU CN201720695679U CN206782069U CN 206782069 U CN206782069 U CN 206782069U CN 201720695679 U CN201720695679 U CN 201720695679U CN 206782069 U CN206782069 U CN 206782069U
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- Prior art keywords
- fender rod
- horn
- unmanned plane
- buffer
- main
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Abstract
The utility model provides a kind of buffer of unmanned plane, including main body, the circumference of main body is uniformly provided with several horns, the end of horn is provided with rotor, and each horn upper and lower surface is equipped with chute, location-plate is provided with chute, the side of location-plate is connected with the first spring, the other end of first spring is connected with the slide plate that can be slided in chute, and the both ends rotatable connection of slide plate has side fender rod, and the other end of two side fender rods is connected with main fender rod.The utility model can play the side fender rod of protection and main fender rod to main body, horn and rotor; and elastic connection is used between side fender rod and main fender rod and horn; certain cushioning effect can be played, is effectively protected the work of rotor, so as to ensure that unmanned plane normally works.
Description
Technical field
The utility model belongs to unmanned air vehicle technique field, in particular to a kind of buffer of unmanned plane.
Background technology
Unmanned aerial vehicle, abbreviation unmanned plane (UAV), it is a kind of new concept weapon equipment being in developing rapidly, it has
Maneuverability, rapid reaction, unmanned flight, operation require the advantages of low.Unmanned plane is by carrying multiclass sensor, it is possible to achieve
Image real-time Transmission, high-risk areas detecting function, it is the strong supplement of satellite remote sensing and traditional air remote sensing.At present, unmanned plane
Use range widened military affairs, scientific research, civilian three big field, specifically in electric power, communication, meteorology, agricultural, ocean, survey
Visit, photograph, preventing and reducing natural disasters, Crop Estimation, drug law enforcement anti-smuggling, border patrol, the field application such as public security anti-terrorism it is very wide.
Needing to fly in different more rugged environments just because of unmanned plane, the possibility that it is damaged is very big,
Especially rotor and horn part, a little damaged if having, will result in imbalance, further result in huge economic loss.
Utility model content
The purpose of this utility model is and a kind of unmanned plane for proposing in order to solve the shortcomings that proposed in background technology
Buffer.
To achieve these goals, the utility model employs following technical scheme：A kind of anticollision buffering dress of unmanned plane
Put, including main body, the circumference of the main body are uniformly provided with several horns, the end of the horn is provided with rotor, each
The horn upper and lower surface is equipped with chute, is provided with location-plate in the chute, the side of the location-plate is connected with the first bullet
Spring, the other end of first spring are connected with the slide plate that can be slided in chute, and the both ends rotatable connection of the slide plate has
Side fender rod, the other end of two side fender rods are connected with main fender rod, and two are interval with each side fender rod
Individual stop collar, the slip ring that can be slided on the fender rod of side, the slip ring and both sides are arranged between two stop collars
Stop collar between be provided with second spring, pull bar is connected with the slip ring, the other end of the pull bar is connected with horn.
It is further preferred that the utility model proposes a kind of unmanned plane buffer, wherein the main protection
Bar is arc-shaped elastic bar, and appearance bread has crossed one layer of rubber layer.
It is further preferred that the utility model proposes a kind of unmanned plane buffer, wherein the location-plate
It is parallel with the slide plate.
It is further preferred that the utility model proposes a kind of unmanned plane buffer, wherein the main protection
Bar is more than the length of horn apart from the minimum distance of main body.
It is further preferred that the utility model proposes a kind of unmanned plane buffer, wherein the side protect
Bar is more than three centimetres with the vertical height for one end corresponding horn upper surface of distance that main fender rod connects.
Compared with prior art, the beneficial effect of buffer of the present utility model is：There is provided can be to master
Body, horn and rotor play the side fender rod of protection and main fender rod, and between side fender rod and main fender rod and horn
Using elastic connection, certain cushioning effect can be played, is effectively protected the balance of rotor, so as to ensure that unmanned plane is normal
Work.
Brief description of the drawings
Fig. 1 be the utility model proposes a kind of unmanned plane buffer general structure schematic diagram；
Fig. 2 be the utility model proposes a kind of unmanned plane buffer horn at side view；
Fig. 3 be the utility model proposes a kind of unmanned plane buffer horn at structural representation.
In figure：Main body 1, chute 2, rotor 3, horn 4, location-plate 5, the first spring 6, stop collar 7, side fender rod 8, master
Fender rod 9, pull bar 10, slip ring 11, slide plate 12, second spring 13.
Embodiment
Below in conjunction with the accompanying drawing in the utility model embodiment, the technical scheme in the embodiment of the utility model is carried out
Clearly and completely describe, it is clear that described embodiment is only the preferable embodiment of the utility model, but this practicality
New protection domain is not limited thereto, the technology that any one skilled in the art discloses in the utility model
In the range of, equivalent substitution or change are subject to according to the technical solution of the utility model and its utility model design, should all be covered
Within the scope of protection of the utility model.
Reference picture 1, Fig. 2, Fig. 3, a kind of buffer of unmanned plane, the device include main body 1, main body 1
Several horns 4 circumferentially are uniformly provided with, the end of horn 4 is provided with rotor 3, and each upper and lower surface of horn 4 is equipped with chute 2, sliding
Location-plate 5 is provided with groove 2, the side of location-plate 5 is connected with the first spring 6, and the other end of the first spring 6 is connected with can be in cunning
The slide plate 12 slided in groove 2, the both ends rotatable connection of slide plate 12 have side fender rod 8, and the other end of two side fender rods 8 is connected with
Main fender rod 9, two stop collars 7 is interval with each side fender rod 8, being arranged between two stop collars 7 can protect in side
Second spring 13 is provided between the stop collar 7 of the slip ring 11 slided on bar 8, slip ring 11 and both sides, is connected on slip ring 11
There is pull bar 10, the other end of pull bar 10 is connected with horn 4.
Main fender rod 9 is arc-shaped elastic bar, and appearance bread has crossed one layer of rubber layer, and location-plate 5 and slide plate 12 are flat
OK, main fender rod 9 apart from main body 1 minimum distance be more than horn 4 length, side fender rod 8 be connected with main fender rod 9 one
The vertical height of the upper surface of horn 4 is more than three centimetres corresponding to the distance of end.
When in use, when receiving side fender rod 8 by external force, pull bar 10 pulls slip ring 11 to prevent in side to the utility model
Slided on guard bar 8, because the effect of second spring 13 can effectively buffer impact of the external force to body, while side is protected
Bar 8 promotes slide plate 12 to be slided in chute 2, due to the active force by the first spring 6, the work for serving buffering similarly
With, and external force first can offside fender rod 8 and the main bad student of fender rod 9 impact, rotor 3 and horn 4 will not be damaged.
Claims (5)
1. a kind of buffer of unmanned plane, including main body (1), the circumference of the main body (1) is uniformly provided with some
Individual horn (4), the end of the horn (4) are provided with rotor (3), it is characterised in that each horn (4) upper and lower surface is all provided with
There is chute (2), be provided with location-plate (5) in the chute (2), the side of the location-plate (5) is connected with the first spring (6), institute
The other end for stating the first spring (6) is connected with the slide plate (12) that can be slided in chute (2), the both ends rotation of the slide plate (12)
Turn to be connected with side fender rod (8), the other end of two side fender rods (8) is connected with main fender rod (9), and each side is prevented
Two stop collars (7) are interval with guard bar (8), being arranged between two stop collars (7) can slide on side fender rod (8)
Dynamic slip ring (11), second spring (13), the slip ring are provided between the slip ring (11) and the stop collar (7) of both sides
(11) pull bar (10) is connected with, the other end of the pull bar (10) is connected with horn (4).
A kind of 2. buffer of unmanned plane according to claim 1, it is characterised in that：The main fender rod (9)
For arc-shaped elastic bar, and appearance bread has crossed one layer of rubber layer.
A kind of 3. buffer of unmanned plane according to claim 1, it is characterised in that：The location-plate (5) with
The slide plate (12) is parallel.
A kind of 4. buffer of unmanned plane according to claim 1, it is characterised in that：The main fender rod (9)
Minimum distance apart from main body (1) is more than the length of horn (4).
A kind of 5. buffer of unmanned plane according to claim 1, it is characterised in that：The side fender rod (8)
It is more than three centimetres with the vertical height of one end distance corresponding horn (4) upper surface of main fender rod (9) connection.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720695679.XU CN206782069U (en) | 2017-06-15 | 2017-06-15 | A kind of buffer of unmanned plane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201720695679.XU CN206782069U (en) | 2017-06-15 | 2017-06-15 | A kind of buffer of unmanned plane |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206782069U true CN206782069U (en) | 2017-12-22 |
Family
ID=60717223
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201720695679.XU Expired - Fee Related CN206782069U (en) | 2017-06-15 | 2017-06-15 | A kind of buffer of unmanned plane |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206782069U (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108791847A (en) * | 2018-06-08 | 2018-11-13 | 南京熙赢测控技术有限公司 | A kind of device being used for automatic identification road surface inspection well cover and automatic numbering |
| CN108928467A (en) * | 2018-06-01 | 2018-12-04 | 芜湖超源力工业设计有限公司 | A kind of drop-proof unmanned plane |
| CN110203399A (en) * | 2019-04-22 | 2019-09-06 | 苏州声婉智能科技有限公司 | It is a kind of can be to the unmanned plane that crops are sprayed insecticide |
| CN111994290A (en) * | 2020-09-03 | 2020-11-27 | 清华大学合肥公共安全研究院 | Pop-up protection device, unmanned aerial vehicle and control system |
| CN112572794A (en) * | 2020-12-16 | 2021-03-30 | 深圳市瑞可创新科技有限公司 | A unmanned aerial vehicle for taking photo by plane that has a protect function |
-
2017
- 2017-06-15 CN CN201720695679.XU patent/CN206782069U/en not_active Expired - Fee Related
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108928467A (en) * | 2018-06-01 | 2018-12-04 | 芜湖超源力工业设计有限公司 | A kind of drop-proof unmanned plane |
| CN108928467B (en) * | 2018-06-01 | 2021-09-17 | 芜湖超源力工业设计有限公司 | Anti-falling type unmanned aerial vehicle |
| CN108791847A (en) * | 2018-06-08 | 2018-11-13 | 南京熙赢测控技术有限公司 | A kind of device being used for automatic identification road surface inspection well cover and automatic numbering |
| CN108791847B (en) * | 2018-06-08 | 2021-11-16 | 南京熙赢测控技术有限公司 | Device for automatically identifying road inspection well cover and automatically numbering |
| CN110203399A (en) * | 2019-04-22 | 2019-09-06 | 苏州声婉智能科技有限公司 | It is a kind of can be to the unmanned plane that crops are sprayed insecticide |
| CN111994290A (en) * | 2020-09-03 | 2020-11-27 | 清华大学合肥公共安全研究院 | Pop-up protection device, unmanned aerial vehicle and control system |
| CN111994290B (en) * | 2020-09-03 | 2022-04-01 | 清华大学合肥公共安全研究院 | Pop-up protection device, unmanned aerial vehicle and control system |
| CN112572794A (en) * | 2020-12-16 | 2021-03-30 | 深圳市瑞可创新科技有限公司 | A unmanned aerial vehicle for taking photo by plane that has a protect function |
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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: 20171222 Termination date: 20190615 |
|
| CF01 | Termination of patent right due to non-payment of annual fee |