CN209617477U - A kind of unmanned plane wing protective device - Google Patents
A kind of unmanned plane wing protective device Download PDFInfo
- Publication number
- CN209617477U CN209617477U CN201920030528.1U CN201920030528U CN209617477U CN 209617477 U CN209617477 U CN 209617477U CN 201920030528 U CN201920030528 U CN 201920030528U CN 209617477 U CN209617477 U CN 209617477U
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- China
- Prior art keywords
- top surface
- unmanned plane
- shield
- cross bar
- protective device
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Abstract
The utility model relates to unmanned plane protective device technical fields, and disclose a kind of unmanned plane wing protective device, including drone body, the left and right sides of the drone body is fixedly installed with master link, two master links are fixedly installed with supported rod erecting far from the top surface of drone body one end, the outer surface of supported rod erecting bottom end is fixedly installed with, and the outer surface movable sleeve in the middle part of supported rod erecting is connected to top surface shield, and the bottom surface of top surface shield is fixedly installed with side shield.The unmanned plane wing protective device, by top surface be arranged top surface shield sum side be provided with side shield, utilize the effect of top surface shield and side shield, wing can be allowed to be not damaged in the process of movement, block injury of the exterior object to unmanned plane wing, make the wing of unmanned plane be not easily susceptible to damage, economic unnecessary loss is avoided, to improve the practicability of the wing protective device.
Description
Technical field
The utility model relates to unmanned plane protective device technical field, specially a kind of unmanned plane wing protective device.
Background technique
Unmanned plane is the unmanned aircraft manipulated using radio robot and the presetting apparatus provided for oneself, or
Be by car-mounted computer completely or intermittently autonomous operation.
In the use process of unmanned plane, unmanned plane may lead to nobody because of not controlling when flying high
Machine touches the object of some branches being higher by etc, damages the wing of unmanned plane, and existing unmanned plane wing, which is not installed, appoints
What protective device, causes the wing of unmanned plane not have any safeguard measure during operating, has damaged unmanned plane wing,
Economic loss is caused, if desired existing unmanned plane is installed protective device and then needed in the installation protection of the top of wing support rod
Device, but install step too complex, be not easy to be rapidly performed by installation.
Utility model content
In view of the deficiencies of the prior art, the utility model provides a kind of unmanned plane wing protective device, has to wing
Play the role of protection and the advantages of can quickly install to protective device, solve unmanned plane wing do not install it is any
Protective device causes the wing of unmanned plane not have any safeguard measure during operating, has damaged unmanned plane wing, makes
At economic loss, if desired existing unmanned plane is installed protective device and is then needed in the installation protection of the top of wing support rod
Device, but the step too complex installed, are not easy to the problem of quickly being installed.
The utility model provides the following technical solutions: a kind of unmanned plane wing protective device, including drone body, described
The left and right sides of drone body is fixedly installed with master link, and two master links are far from drone body one end
Top surface is fixedly installed with supported rod erecting, and the outer surface of the supported rod erecting bottom end is fixedly installed with connection cross bar, and the support is vertical
Outer surface movable sleeve in the middle part of bar is connected to top surface shield, and the bottom surface of the top surface shield is fixedly installed with side shield,
The top surface of the top surface shield offers venthole, and the inner cavity of the top surface shield is circumferentially uniformly fixedly installed with frame linking
Bar, the quantity of the connecting rod are eight, and locking level is fixedly installed in the middle part of top surface shield top surface, and the support is vertical
The top of bar sequentially passes through top surface shield and locking level and extends to the outside of locking level, the left and right sides of the locking level
It is fixedly installed with lock box, the middle part movable sleeve of the lock box left side is connected to locking cross bar, a left side for the locking cross bar
End is fixedly connected with pull rod, and the right end of the locking cross bar sequentially passes through lock box and locking level and extends to the interior of locking level
The outer surface movable sleeve in portion, the locking cross bar is connected between the left side of lock box inner cavity and the left side of locking level
Lock spring.
Preferably, the shape of the top surface shield be circle, the diameter of the top surface shield with connect the straight of cross bar
Diameter is adapted.
Preferably, the connection cross bar is filled in flabellum, and the quantity for connecting cross bar is four.
Preferably, left side of the both ends of the Lock spring respectively with the left side of lock box inner cavity and locking level is fixed
Connection.
Preferably, the left and right side of the supported rod erecting top surface offers limit hole, and the size and shape of limit hole
It is adapted with the size and shape of locking cross bar.
Preferably, the top surface shield and side shield are made of aluminium alloy.
Be compared with the prior art, the utility model have it is following the utility model has the advantages that
1, the unmanned plane wing protective device, by top surface the side of top surface shield sum is set to be provided with side anti-
Shield can allow wing to be not damaged in the process of movement using the effect of top surface shield and side shield, resistance
Injury of the exterior object to unmanned plane wing has been kept off, the wing of unmanned plane is made to be not easily susceptible to damage, has avoided the unnecessary of economy
Loss, to improve the practicability of the wing protective device.
2, the unmanned plane wing protective device utilizes supported rod erecting, limit hole, locking level, locking by pulling pull rod
Mutual cooperation between box, locking cross bar and Lock spring, makes Lock spring carry out normal elastic force compression, then unclamps locking
Spring makes to lock in the limit hole that is inserted at the top of supported rod erecting of right end of cross bar, can carry out protective device quick
It is fixed, to improve the suitability of the wing protective device.
Detailed description of the invention
FIG. 1 is a schematic structural view of the utility model；
Fig. 2 is the utility model local structure top view；
Fig. 3 is the schematic enlarged-scale view in the utility model at A.
In figure: 1, drone body；2, connecting rod；3, supported rod erecting；4, cross bar is connected；5, top surface shield；6, side
Shield；7, connecting rod；8, locking level；9, lock box；10, cross bar is locked；11, pull rod；12, Lock spring；13, venthole.
Specific embodiment
The following will be combined with the drawings in the embodiments of the present invention, carries out the technical scheme in the embodiment of the utility model
Clearly and completely describe, it is clear that the described embodiments are only a part of the embodiments of the utility model, rather than whole
Embodiment.Based on the embodiments of the present invention, those of ordinary skill in the art are without making creative work
Every other embodiment obtained, fall within the protection scope of the utility model.
Please refer to Fig. 1-3, a kind of unmanned plane wing protective device, including drone body 1, the left and right of drone body 1
Two sides are fixedly installed with master link 2, and two master links 2 are fixedly installed with branch far from the top surface of 1 one end of drone body
Upright bar 3 is supportted, the left and right side of 3 top surface of supported rod erecting offers limit hole, and the size and shape of limit hole and locking cross bar
10 size and shape is adapted, and limit hole opens up the company for allowing locking cross bar 10 that can allow supported rod erecting 3 and top surface shield 5
Connect it is firm, the outer surface of 3 bottom end of supported rod erecting be fixedly installed with connection cross bar 4, connection cross bar 4 in flabellum fill, and connection cross bar 4
Quantity be four, connection cross bar 4 setting unmanned plane can be allowed normally to operate, guarantee connection cross bar 4 be drone body 1
Enough lift is provided, the outer surface movable sleeve at 3 middle part of supported rod erecting is connected to top surface shield 5, and the shape of top surface shield 5 is
Circle, the diameter of top surface shield 5 are adapted with the diameter for connecting cross bar 4, and circular setting can allow connection cross bar 4 rotating
During side shield 6 collide with the flank section for connecting cross bar 4, top surface shield 5 and side shield 6 are that aluminium closes
Gold is made, and the hardness height of aluminium alloy and the light weight of its material, the bottom surface of top surface shield 5 is fixedly installed with side shield
6, the top surface of top surface shield 5 offers venthole 13, and the inner cavity of top surface shield 5 is circumferentially uniformly fixedly installed with connecting rod 7,
The quantity of connecting rod 7 is eight, is fixedly installed with locking level 8 in the middle part of 5 top surface of top surface shield, the top of supported rod erecting 3 according to
It is secondary through top surface shield 5 and locking level 8 and the outside for extending to locking level 8, the left and right sides of locking level 8 are fixedly mounted
There is lock box 9, the middle part movable sleeve of 9 left side of lock box is connected to locking cross bar 10, and the left end of locking cross bar 10 is fixedly connected with
The right end of pull rod 11, locking cross bar 10 sequentially passes through lock box 9 and locking level 8 and the inside for extending to locking level 8, locks cross bar
10 outer surface movable sleeve is connected to the Lock spring 12 between the left side of 9 inner cavity of lock box and the left side of locking level 8,
The both ends of Lock spring 12 are fixedly connected with the left side of the left side of 9 inner cavity of lock box and locking level 8 respectively, Lock spring 12
Being fixedly connected for both ends can allow spring to play the effect of its elastic force in the inside of lock box 9.
When work, user of service first pulls open pull rod 11, and supported rod erecting 3 is enable to pass through from the inside of locking level 8, to
The top surface of locking level 8 is exposed on the top of supported rod erecting 3, can releasing lever 11, then top surface shield 5 is pressed downward again, directly
The inside that limit hole can be penetrated to one end of locking cross bar 10, makes the connection relationship between supported rod erecting 3 and top surface shield 5
It is fixed, unmanned plane can be opened, to unmanned plane carry out using.
It should be noted that, in this document, relational terms such as first and second and the like are used merely to a reality
Body or operation are distinguished with another entity or operation, are deposited without necessarily requiring or implying between these entities or operation
In any actual relationship or order or sequence.Moreover, the terms "include", "comprise" or its any other variant are intended to
Non-exclusive inclusion, so that the process, method, article or equipment including a series of elements is not only wanted including those
Element, but also including other elements that are not explicitly listed, or further include for this process, method, article or equipment
Intrinsic element.
While there has been shown and described that the embodiments of the present invention, for the ordinary skill in the art,
It is understood that these embodiments can be carried out with a variety of variations in the case where not departing from the principles of the present invention and spirit, repaired
Change, replacement and variant, the scope of the utility model is defined by the appended claims and the equivalents thereof.
Claims (6)
1. a kind of unmanned plane wing protective device, including drone body (1), it is characterised in that: the drone body (1)
The left and right sides is fixedly installed with master link (2), top of two master links (2) far from drone body (1) one end
Face is fixedly installed with supported rod erecting (3), and the outer surface of supported rod erecting (3) bottom end is fixedly installed with connection cross bar (4), described
Outer surface movable sleeve in the middle part of supported rod erecting (3) is connected to top surface shield (5), the fixed peace in the bottom surface of the top surface shield (5)
Equipped with side shield (6), the top surface of the top surface shield (5) is offered venthole (13), the top surface shield (5)
Inner cavity is circumferentially uniformly fixedly installed with connecting rod (7), and the quantity of the connecting rod (7) is eight, top surface shield (5) top
It is fixedly installed in the middle part of face locking level (8), the top of the supported rod erecting (3) sequentially passes through top surface shield (5) and locking
The left and right sides of bar (8) and the outside for extending to locking level (8), the locking level (8) are fixedly installed with lock box (9),
The middle part movable sleeve of lock box (9) left side is connected to locking cross bar (10), and the left end of locking cross bar (10) is fixed to be connected
It is connected to pull rod (11), the right end of locking cross bar (10) sequentially passes through lock box (9) and locking level (8) and extends to locking level
(8) the outer surface movable sleeve of inside, locking cross bar (10) is connected to left side and locking level positioned at lock box (9) inner cavity
(8) Lock spring (12) between left side.
2. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that: the top surface shield (5)
Shape be circle, the diameter of the top surface shield (5) is adapted with the diameter for connecting cross bar (4).
3. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that: the connection cross bar (4) is in
Flabellum dress, and the quantity for connecting cross bar (4) is four.
4. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that: the Lock spring (12)
Both ends are fixedly connected with the left side of the left side of lock box (9) inner cavity and locking level (8) respectively.
5. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that: supported rod erecting (3) top
The left and right side in face offers limit hole, and the size and shape of limit hole and the size and shape of locking cross bar (10) are mutually fitted
Match.
6. a kind of unmanned plane wing protective device according to claim 1, it is characterised in that: the top surface shield (5)
It is made with side shield (6) of aluminium alloy.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920030528.1U CN209617477U (en) | 2019-01-08 | 2019-01-08 | A kind of unmanned plane wing protective device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201920030528.1U CN209617477U (en) | 2019-01-08 | 2019-01-08 | A kind of unmanned plane wing protective device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN209617477U true CN209617477U (en) | 2019-11-12 |
Family
ID=68449228
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201920030528.1U Expired - Fee Related CN209617477U (en) | 2019-01-08 | 2019-01-08 | A kind of unmanned plane wing protective device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN209617477U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110877720A (en) * | 2019-12-06 | 2020-03-13 | 湖南浩天翼航空技术有限公司 | Conveniently accomodate unmanned aerial vehicle wing protector |
| CN111017204A (en) * | 2020-01-13 | 2020-04-17 | 深圳市星图智控科技有限公司 | Rapid take-off and landing unmanned aerial vehicle and take-off and landing control method of unmanned aerial vehicle |
-
2019
- 2019-01-08 CN CN201920030528.1U patent/CN209617477U/en not_active Expired - Fee Related
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110877720A (en) * | 2019-12-06 | 2020-03-13 | 湖南浩天翼航空技术有限公司 | Conveniently accomodate unmanned aerial vehicle wing protector |
| CN111017204A (en) * | 2020-01-13 | 2020-04-17 | 深圳市星图智控科技有限公司 | Rapid take-off and landing unmanned aerial vehicle and take-off and landing control method of unmanned aerial vehicle |
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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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20191112 Termination date: 20210108 |