CN208119402U - A kind of UAV Landing shock-absorbing protecting structure - Google Patents
A kind of UAV Landing shock-absorbing protecting structure Download PDFInfo
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- CN208119402U CN208119402U CN201820423657.2U CN201820423657U CN208119402U CN 208119402 U CN208119402 U CN 208119402U CN 201820423657 U CN201820423657 U CN 201820423657U CN 208119402 U CN208119402 U CN 208119402U
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Abstract
The utility model discloses a kind of UAV Landing shock-absorbing protecting structures,It is characterized in that,Main structure body including being set to unmanned aerial vehicle body top,It is convex stupefied that the top of main structure body offers the first ellipse,Second ellipse is convex stupefied,Third ellipse is convex stupefied,First ellipse is convex stupefied,Second ellipse is convex stupefied,Third ellipse is convex stupefied along the setting of unmanned aerial vehicle body length direction and and wing vertical,First ellipse is convex stupefied,Second ellipse is convex stupefied and third ellipse is convex stupefied mutual is equidistant and is parallel to each other,The convex stupefied close port wing setting of first ellipse,The convex stupefied close starboard wing setting of third ellipse,Second ellipse is convex stupefied to be set on the center line of unmanned aerial vehicle body along its length,The high height of unmanned plane of UAV Landing shock-absorbing protecting structure-steel framing,The simultaneously high height between task device and ground of frame,There is impact force when can effectively absorb landing,More preferably save task device and electronic equipment from damage.
Description
Technical field
The utility model relates to unmanned plane equipment technical field more particularly to a kind of UAV Landing shock-absorbing protecting structures.
Background technique
The rear body of previous aircraft landing is easy to damage, and the electronic equipment facility of fuselage interior is also easy to damage.It lacks
Few shock-absorbing protecting, unmanned plane impact force in landing is big, and speed is fast, if not effective shock-absorbing protecting, the task in fuselage is set
It is standby to be just easily broken, it is unable to complete task, and now some simply protect task device with foam-rubber cushion, in fact
It is to be unable to reach to reduce this loss, acts on very little, task device very little at a distance from ground；
Therefore, those skilled in the art has been devoted to research and develop a kind of high height of unmanned plane of frame, while frame is high
Height between task device and ground, four spue come it is stupefied, have impact force when can effectively absorb landing, more preferably save from damage
The UAV Landing shock-absorbing protecting structure of task device and electronic equipment.
Utility model content
The technical problem to be solved by the present invention is to provide a kind of UAV Landing shock-absorbing protecting structure, the unmanned plane
The land shock-absorbing protecting structure-steel framing high height of unmanned plane, while the high height between task device and ground of frame, having can be effective
Absorption landing when impact force, more preferably save task device and electronic equipment from damage.
In order to solve the above technical problems, the utility model provides a kind of UAV Landing shock-absorbing protecting structure, including setting
Main structure body in unmanned aerial vehicle body top, the top of main structure body offer convex stupefied, the second ellipse of the first ellipse it is convex it is stupefied,
Third ellipse is convex stupefied, convex stupefied, the second ellipse of first ellipse it is convex it is stupefied, third ellipse is convex stupefied along unmanned aerial vehicle body
Length direction setting and and wing vertical, convex stupefied, the second ellipse of the first ellipse is convex stupefied and third ellipse it is convex it is stupefied each other
Be equidistant and be parallel to each other, the convex stupefied close port wing setting of first ellipse, the third ellipse is convex stupefied close
Starboard wing setting, second ellipse it is convex it is stupefied be set on the center line of unmanned aerial vehicle body along its length, described first is ellipse
It is convex stupefied that round convex stupefied, convex stupefied, the convex stupefied rear portion of third ellipse of the second ellipse is provided with the 4th ellipse, and the described 4th is oval
Type it is convex it is stupefied be set on the center line of unmanned aerial vehicle body along its length, the 4th ellipse it is convex it is stupefied be set to left and right wing with
Between empennage.
Preferably, convex stupefied, the second ellipse of first ellipse is convex stupefied and the convex stupefied length of third ellipse is from nothing
At people's fuselage head to the 1/3 of unmanned left and right wing.
Preferably, second ellipse it is convex it is stupefied with the 4th ellipse it is convex it is stupefied between be provided with a cylindrical type for absorbing
The shock relieve vent of impact force when landing, the shock relieve vent are set on the central point between port wing and starboard wing.
Preferably, note the distance between left and right wing and empennage is L, and the convex stupefied length of the 4th ellipse is from left and right
Wing to far from the left and right wing direction to 1/2L at.
Preferably, convex stupefied, the third ellipse of convex stupefied, the second ellipse of the first ellipse is convex stupefied and the convex stupefied packet of the 4th ellipse
Intermediate projections are included, intermediate projections both sides offer arc groove.
After using the above structure, UAV Landing shock-absorbing protecting structure, the knot including being set to unmanned aerial vehicle body top
Structure main body, the top of main structure body offer convex stupefied, the second ellipse of the first ellipse it is convex it is stupefied, third ellipse is convex stupefied, first
Convex stupefied, the third ellipse of convex stupefied, the second ellipse of ellipse is convex stupefied to be arranged along unmanned aerial vehicle body length direction and hangs down with wing
Directly, convex stupefied, the second ellipse of the first ellipse is convex stupefied and third ellipse is convex stupefied mutual is equidistant and is parallel to each other, the
The convex stupefied close port wing setting of one ellipse, convex stupefied close the starboard wing of third ellipse are arranged, and the second ellipse is convex stupefied to be set to
On the center line of unmanned aerial vehicle body along its length, convex stupefied, the second ellipse of the first ellipse it is convex it is stupefied, third ellipse is convex stupefied
It is convex stupefied that rear portion is provided with the 4th ellipse, the 4th ellipse it is convex it is stupefied be set on the center line of unmanned aerial vehicle body along its length,
4th ellipse it is convex it is stupefied be set between left and right wing and empennage, convex stupefied, the second ellipse of the first ellipse it is convex it is stupefied, third is oval
Type is convex stupefied and the 4th ellipse is convex stupefied is equipped with, can effectively reduce unmanned plane land into vibration, and absorb vibration, subtract
Few impact force, the high height of unmanned plane of the UAV Landing shock-absorbing protecting structure-steel framing, while frame high task device and ground
Between height, have impact force when can effectively absorb landing, more preferably save task device and electronic equipment from damage.
Detailed description of the invention
Fig. 1 is a kind of overall structure figure of UAV Landing shock-absorbing protecting structure of the utility model.
Specific embodiment
In order to make the purpose of the utility model, technical solutions and advantages more clearly understood, below in conjunction with attached drawing and implementation
Example, the present invention will be further described in detail.It should be appreciated that specific embodiment described herein is used only for explaining
The utility model is not used to limit the utility model.
Referring to Fig. 1, Fig. 1 is a kind of overall structure figure of UAV Landing shock-absorbing protecting structure of the utility model.
Embodiment 1
A kind of UAV Landing shock-absorbing protecting structure, the main structure body 1 including being set to unmanned aerial vehicle body top, structure master
The top of body 1 offers that the first ellipse is convex stupefied 15, the second ellipse is convex stupefied 14, third ellipse convex stupefied 11, the first ellipse
Convex stupefied 15, the second ellipse is convex stupefied 14, third ellipse convex stupefied 11 is arranged along unmanned aerial vehicle body length direction and hangs down with wing
Directly, the first ellipse is convex stupefied 15, the second ellipse convex stupefied 14 and third ellipse convex stupefied 11 are mutual is equidistant and mutually
In parallel, the first ellipse convex stupefied 15 is arranged close to port wing, and third ellipse convex stupefied 11 is arranged close to starboard wing, the second ellipse
Convex stupefied 14 are set on the center line of unmanned aerial vehicle body along its length, the first ellipse is convex stupefied 15, the second ellipse is convex stupefied 14,
Convex stupefied 11 rear portion of third ellipse is provided with that the 4th ellipse is convex stupefied, and the 4th ellipse convex stupefied 13 is set to unmanned aerial vehicle body edge
On the center line of length direction, the 4th ellipse convex stupefied 13 is set between left and right wing 2 and empennage 3.
In the present embodiment, the first ellipse is convex stupefied 15, the second ellipse convex stupefied 14 and convex stupefied 11 length of third ellipse
Degree is from from unmanned fuselage head to the 1/3 of unmanned left and right wing
In the present embodiment, a cylindrical type is provided between the second ellipse convex stupefied 14 and the 4th ellipse convex stupefied 13 to use
The shock relieve vent of impact force when absorbing landing, the shock relieve vent are set on the central point between port wing and starboard wing.
Remember that the distance between left and right wing and empennage are L, convex stupefied 13 length of the 4th ellipse is from left and right wing 2 to remote
At direction to 1/2L from left and right wing 2.
First ellipse is convex stupefied 15, the second ellipse is convex stupefied 14, third ellipse convex stupefied 11 and the 4th ellipse convex stupefied 13
Including intermediate projections, intermediate projections both sides offer arc groove.
After using the above structure, UAV Landing shock-absorbing protecting structure, the knot including being set to unmanned aerial vehicle body top
Structure main body 1, the top of main structure body 1 offer that the first ellipse is convex stupefied 15, the second ellipse is convex stupefied 14, third ellipse is convex stupefied
11, the first ellipse is convex stupefied 15, the second ellipse is convex stupefied 14, third ellipse convex stupefied 11 is set along unmanned aerial vehicle body length direction
Set and and wing vertical, the first ellipse is convex stupefied 15, the second ellipse convex stupefied 14 and third ellipse convex stupefied 11 are mutual away from
From equal and be parallel to each other, the first ellipse convex stupefied 15 is arranged close to port wing, and third ellipse convex stupefied 11 is set close to starboard wing
It sets, the second ellipse convex stupefied 14 is set on the center line of unmanned aerial vehicle body along its length, the first ellipse convex stupefied 15, second
Convex stupefied, convex stupefied 13 setting of the 4th ellipse that ellipse is convex stupefied 14, convex stupefied 11 rear portion of third ellipse is provided with the 4th ellipse
In on the center line of unmanned aerial vehicle body along its length, the 4th ellipse convex stupefied 13 is set between left and right wing 2 and empennage 3,
First ellipse is convex stupefied 15, the second ellipse is convex stupefied 14, third ellipse convex stupefied 11 and the 4th convex stupefied 13 cooperation of ellipse are set
Set, can effectively reduce unmanned plane land into vibration, and absorb vibration, reduce impact force, the UAV Landing shock-absorbing protecting
The structure-steel framing high height of unmanned plane, while the high height between task device and ground of frame, landing can effectively be absorbed by having
When impact force, more preferably save task device and electronic equipment from damage.
It should be understood that cannot therefore limit the utility model the above is only the preferred embodiment of the utility model
The scope of the patents, equivalent structure or equivalent flow shift made by using the description of the utility model and the drawings, or it is straight
It connects or is used in other related technical areas indirectly, be also included in the patent protection scope of the utility model.
Claims (5)
1. a kind of UAV Landing shock-absorbing protecting structure, which is characterized in that the structure master including being set to unmanned aerial vehicle body top
Body, the top of main structure body offer convex stupefied, the second ellipse of the first ellipse it is convex it is stupefied, third ellipse is convex stupefied, described first
Convex stupefied, the third ellipse of convex stupefied, the second ellipse of ellipse is convex stupefied to be arranged along unmanned aerial vehicle body length direction and hangs down with wing
Directly, convex stupefied, the second ellipse of the first ellipse is convex stupefied and third ellipse is convex stupefied mutual is equidistant and is parallel to each other, institute
The convex stupefied close port wing setting of the first ellipse is stated, the convex stupefied close starboard wing setting of third ellipse, described second is oval
Type it is convex it is stupefied be set on the center line of unmanned aerial vehicle body along its length, convex stupefied, the second ellipse of first ellipse it is convex it is stupefied,
It is convex stupefied that the convex stupefied rear portion of third ellipse is provided with the 4th ellipse, and the 4th ellipse is convex stupefied to be set to unmanned aerial vehicle body edge
On the center line of length direction, the 4th ellipse is convex stupefied to be set between left and right wing and empennage.
2. UAV Landing shock-absorbing protecting structure according to claim 1, which is characterized in that first ellipse is convex
Stupefied, the second ellipse is convex stupefied and the convex stupefied length of third ellipse is from from unmanned fuselage head to the 1/3 of unmanned left and right wing.
3. UAV Landing shock-absorbing protecting structure according to claim 1, which is characterized in that second ellipse is convex stupefied
With the 4th ellipse it is convex it is stupefied between be provided with a cylindrical type for absorbs land when impact force shock relieve vent, the shock relieve vent
It is set on the central point between port wing and starboard wing.
4. UAV Landing shock-absorbing protecting structure according to claim 1, which is characterized in that note left and right wing and empennage it
Between distance be L, the convex stupefied length of the 4th ellipse is from left and right wing to the direction far from the left and right wing to 1/
At 2L.
5. UAV Landing shock-absorbing protecting structure according to claim 1, which is characterized in that the first ellipse it is convex it is stupefied,
Convex stupefied, the third ellipse of two ellipses is convex stupefied and the 4th ellipse it is convex it is stupefied include intermediate projections, intermediate projections both sides offer arc
Connected in star.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201820423657.2U CN208119402U (en) | 2018-03-27 | 2018-03-27 | A kind of UAV Landing shock-absorbing protecting structure |
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| CN201820423657.2U CN208119402U (en) | 2018-03-27 | 2018-03-27 | A kind of UAV Landing shock-absorbing protecting structure |
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| CN208119402U true CN208119402U (en) | 2018-11-20 |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109774948A (en) * | 2019-02-13 | 2019-05-21 | 山东蜂巢航空科技有限公司 | It is a kind of can a variety of load of carry oil electricity mixing multi-rotor unmanned aerial vehicle |
-
2018
- 2018-03-27 CN CN201820423657.2U patent/CN208119402U/en active Active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN109774948A (en) * | 2019-02-13 | 2019-05-21 | 山东蜂巢航空科技有限公司 | It is a kind of can a variety of load of carry oil electricity mixing multi-rotor unmanned aerial vehicle |
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| GR01 | Patent grant | ||
| GR01 | Patent grant | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A shock absorption protection structure for UAV Landing Effective date of registration: 20210125 Granted publication date: 20181120 Pledgee: Shanxi Financing Reinsurance Group Co.,Ltd. Pledgor: SHENZHEN DI AOPU UAV Co.,Ltd. Registration number: Y2021980000704 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20210601 Granted publication date: 20181120 Pledgee: Shanxi Financing Reinsurance Group Co.,Ltd. Pledgor: SHENZHEN DI AOPU UAV Co.,Ltd. Registration number: Y2021980000704 |
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| CP03 | Change of name, title or address | ||
| CP03 | Change of name, title or address |
Address after: 518035 Room 201, building a, No. 1, Qianwan 1st Road, Qianhai Shenzhen Hong Kong cooperation zone, Nanshan street, Nanshan District, Shenzhen, Guangdong Province settled in Shenzhen Qianhai business secretary Co.,Ltd. Patentee after: Shenzhen Diop UAV Co.,Ltd. Address before: 518000 Room 201, building A, No. 1, Qian Wan Road, Qianhai Shenzhen Hong Kong cooperation zone, Shenzhen, Guangdong (Shenzhen Qianhai business secretary Co., Ltd.) Patentee before: SHENZHEN DI AOPU UAV Co.,Ltd. |
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| PE01 | Entry into force of the registration of the contract for pledge of patent right | ||
| PE01 | Entry into force of the registration of the contract for pledge of patent right |
Denomination of utility model: A damping protection structure for UAV Landing Effective date of registration: 20210907 Granted publication date: 20181120 Pledgee: Shanxi Financing Guarantee Co.,Ltd. Pledgor: Shenzhen Diop UAV Co.,Ltd. Registration number: Y2021440020091 |
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| PC01 | Cancellation of the registration of the contract for pledge of patent right | ||
| PC01 | Cancellation of the registration of the contract for pledge of patent right |
Date of cancellation: 20220905 Granted publication date: 20181120 Pledgee: Shanxi Financing Guarantee Co.,Ltd. Pledgor: Shenzhen Diop UAV Co.,Ltd. Registration number: Y2021440020091 |