CN216834268U

CN216834268U - Wing protective structure for unmanned aerial vehicle

Info

Publication number: CN216834268U
Application number: CN202121111960.7U
Authority: CN
Inventors: 张志荣; 袁泉; 张正涛; 顾俊峰; 吴卿; 唐中一
Original assignee: Global Eagle Aviation Technology Co ltd; Huaiyin Institute of Technology
Current assignee: Global Eagle Aviation Technology Co ltd; Huaiyin Institute of Technology
Priority date: 2021-05-21
Filing date: 2021-05-21
Publication date: 2022-06-28
Anticipated expiration: 2031-05-21

Abstract

The utility model relates to an unmanned air vehicle technique field just discloses a wing protective structure for unmanned aerial vehicle, including the cover body and cystosepiment, the connecting block is all installed to the both sides of the cover body, connecting block one side sets up a wing shell, the rotation axis is installed to wing shell one side, rotation axis one side is provided with and keeps off the lid. This wing protective structure for unmanned aerial vehicle, through setting up the grip block, telescopic machanism, the end cover, electronic flexible loop bar, the supporting shoe, the slider, spout and regulating plate, can be to protective structure's the effectual change effect of playing of mounting dimension, when needs protect different unmanned aerial vehicle, open electronic flexible loop bar power, through promoting the grip block at the spout, make the slider carry out the left and right sides motion, drive grip block self and move simultaneously, make it can change the size of self according to the size of different unmanned aerial vehicle bottoms, make its unmanned aerial vehicle of laminating more, reduce the possibility that drops, increase this protective structure's practicality.

Description

Wing protective structure for unmanned aerial vehicle

Technical Field

The utility model relates to an unmanned air vehicle technique field specifically is a wing protective structure for unmanned aerial vehicle.

Background

Unmanned aircraft is abbreviated as "unmanned aerial vehicle", and is abbreviated as "UAV", is an unmanned aircraft operated by using a radio remote control device and a self-contained program control device, or is operated by an on-board computer completely or intermittently and autonomously, and compared with a piloted aircraft, the unmanned aircraft is more suitable for tasks too "fool, dirty or dangerous", and can be divided into military and civil according to the application field, and the existing unmanned aircraft needs a wing protection structure to protect the wings thereof in the using process.

But current protector, the installation function of most of self is not good, and when the unmanned aerial vehicle of many not unidimensionals of needs carried out protection work, can not install according to different unmanned aerial vehicle's size, makes its use too single when using, has reduced this protector's practicality.

SUMMERY OF THE UTILITY MODEL

Not enough to prior art, the utility model provides a wing protective structure for unmanned aerial vehicle possesses advantages such as can change self mounting dimension, has solved the not good problem of current protector installation function.

For realizing the purpose that above-mentioned protector can change self erection dimension, the utility model provides a following technical scheme: a wing protection structure for an unmanned aerial vehicle comprises a sleeve body and a foam plate, wherein connecting blocks are respectively installed on two sides of the sleeve body, a wing shell is arranged on one side of each connecting block, a rotating shaft is installed on one side of the wing shell, an upper blocking cover is arranged on one side of the rotating shaft, a fixing block is arranged on one side of the upper blocking cover, a fixing groove is formed in the other side of the fixing block, a rubber cushion is arranged on one side of the fixing groove, a first fixing bolt is arranged inside the rubber cushion, the foam plate is installed below the outer portion of the sleeve body, a clamping block is welded on one side of the foam plate, the other side of the clamping block is arranged in a clamping groove, a clamping plate is arranged above the outer portion of the clamping groove, a telescopic mechanism is arranged on one side of the clamping plate, a sliding block is arranged on one side of the telescopic mechanism, a sliding groove is formed in the outer portion of a regulating plate, a mounting plate is arranged below the outer portion of the regulating plate, and second fixing bolts are arranged on two sides of the mounting plate.

Preferably, the upper blocking cover, the rotating shaft and the wing shell form a rotating structure, and the upper blocking cover and the wing shell are distributed in parallel.

Preferably, the upper blocking cover is connected with the wing shell in a clamping mode through a fixing block, and the fixing block is matched with the fixing groove in size.

Preferably, the rubber cushion is in threaded connection with the wing shell through first fixing bolts, and the number of the first fixing bolts is four.

Preferably, the foam board is connected with the sleeve body in a clamping mode through a clamping block, and the clamping block is matched with the clamping groove in size.

Preferably, the telescopic mechanism, the sliding block and the sliding groove form a sliding structure, and the sliding block is symmetrically arranged on the central axis of the sliding groove.

Preferably, the mounting plate is in threaded connection with the sleeve body through second fixing bolts, and the number of the second fixing bolts is eight.

Compared with the prior art, the utility model provides a wing protective structure for unmanned aerial vehicle possesses following beneficial effect:

1. this wing protective structure for unmanned aerial vehicle, through setting up the grip block, telescopic machanism, the end cover, electronic flexible loop bar, the supporting shoe, the slider, spout and regulating plate, can be to protective structure's the effectual change effect of playing of mounting dimension, when needs protect different unmanned aerial vehicle, open electronic flexible loop bar power, through promoting the grip block at the spout, make the slider carry out the left and right sides motion, drive grip block self and move simultaneously, make it can change the size of self according to the size of different unmanned aerial vehicle bottoms, make its unmanned aerial vehicle of laminating more, reduce the possibility that drops, increase this protective structure's practicality.

2. This wing protective structure for unmanned aerial vehicle can play effectual safeguard effect to the wing through setting up wing shell, rotation axis and last fender lid, and when the wing is carrying out the during operation, will go up the fender lid through the rotation axis and rotate, forms the protection to the wing part, prevents to have great object striking or drop the wing and make it take place to damage, the effectual security that has increased unmanned aerial vehicle self.

3. This wing protective structure for unmanned aerial vehicle can play effectual abrasionproof and decrease effect to unmanned aerial vehicle and protection machanism through setting up rubber cushion and first fixing bolt, installs unmanned aerial vehicle after when protection machanism, can great wearing and tearing each other during the use, moves first fixing bolt through clockwise twisting and installs rubber cushion in the cover body, makes it form effectual protection to both sides, increases unmanned aerial vehicle's life.

Drawings

FIG. 1 is a schematic view of a front cross-sectional structure of the present invention;

FIG. 2 is a schematic view of the installation mechanism of the present invention;

FIG. 3 is a schematic view of the connection between the rubber cushion and the first fixing bolt according to the present invention;

fig. 4 is an enlarged view of a structure a in fig. 1 according to the present invention.

In the figure: 1. a sleeve body; 2. connecting blocks; 3. a wing shell; 4. a rotating shaft; 5. an upper blocking cover; 6. a fixed block; 7. fixing grooves; 8. a rubber cushion; 9. a first fixing bolt; 10. a foam board; 11. a clamping block; 12. a card slot; 13. a clamping plate; 14. a telescoping mechanism; 1401. a bottom cover; 1402. an electric telescopic loop bar; 1403. a support block; 15. a slider; 16. a chute; 17. an adjusting plate; 18. mounting a plate; 19. and a second fixing bolt.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Referring to fig. 1-4, a wing protection structure for an unmanned aerial vehicle comprises a sleeve body 1 and a foam board 10, wherein connecting blocks 2 are respectively installed on two sides of the sleeve body 1, a wing shell 3 is arranged on one side of each connecting block 2, a rotating shaft 4 is installed on one side of the wing shell 3, a rotating structure is formed by an upper blocking cover 5, the rotating shaft 4 and the wing shell 3, the upper blocking cover 5 and the wing shell 3 are distributed in parallel, the wing shell 3, the rotating shaft 4 and the upper blocking cover 5 are arranged to effectively protect the wing, when the wing works, the upper blocking cover 5 is rotated through the rotating shaft 4 to protect the wing part, so that a large object is prevented from colliding with or falling down to the wing to cause damage, the safety of the unmanned aerial vehicle is effectively improved, the upper blocking cover 5 is arranged on one side of the rotating shaft 4, a fixing block 6 is arranged on one side of the upper blocking cover 5, go up to keep off lid 5 and be connected with 3 blocks of wing shell through fixed block 6, and fixed block 6 is identical with the size of

fixed slot

7, 6 opposite sides of fixed block are provided with fixed slot 7, fixed slot 7 one side is provided with rubber cushion 8, the inside first fixing bolt 9 that is provided with of rubber cushion 8, rubber cushion 8 is through

first fixing bolt

9 and 3 threaded connection of wing shell, and the quantity of first fixing bolt 9 is four, cystosepiment 10 is installed in the 1 outside below of the cover body, cystosepiment 10 one side welding has fixture block 11, cystosepiment 10 is connected with the 1 block of the cover body through fixture block 11, and the size of fixture block 11 and draw-in groove 12 is identical, fixture block 11 opposite side sets up in there being draw-in groove 12, the outside top of draw-in groove 12 is provided with grip block 13, grip block 13 one side is provided with telescopic machanism 14, through setting up grip block 13, The telescopic mechanism 14, the bottom cover 1401, the electric telescopic sleeve rod 1402, the supporting block 1403, the sliding block 15, the sliding groove 16 and the adjusting plate 17 can effectively replace the installation size of the protective structure, when different unmanned aerial vehicles need to be protected, the power supply of the electric telescopic sleeve rod 1402 is turned on, the clamping plate 13 is pushed to the sliding groove 16, the sliding block 15 moves left and right, the clamping plate 13 is driven to move simultaneously, the size of the clamping plate 13 can be changed according to the size of the bottom of different unmanned aerial vehicles, the clamping plate is more fit with the unmanned aerial vehicles, the possibility of falling is reduced, the practicability of the protective structure is improved, the sliding block 15 is arranged on one side of the telescopic mechanism 14, the sliding block 15 and the sliding groove 16 form a sliding structure, the sliding blocks 15 are symmetrically arranged on the central axis of the sliding groove 16, the sliding groove 16 is arranged on the outer portion of the sliding block 15, and the sliding groove 16 is arranged on one side of the adjusting plate 17, the outside below of regulating plate 17 is provided with mounting panel 18, mounting panel 18 both sides all are provided with second fixing bolt 19, mounting panel 18 is through second fixing bolt 19 and cover 1 threaded connection, and second fixing bolt 19's quantity is eight.

The electrical components presented in the document are all electrically connected with an external master controller and 220V mains, and the master controller can be a conventional known device controlled by a computer or the like.

When in use, firstly, an external power supply is connected, the wing shell 3 is connected to the sleeve body 1 by using the connecting block 2, then when the wing works, the upper blocking cover 5 is rotated by the rotating shaft 4 to protect the wing part, so that a larger object is prevented from being impacted or falling onto the wing to cause damage, the safety of the unmanned aerial vehicle is effectively improved, then the switch of the electric telescopic sleeve rod 1402 is opened, the clamping plate 13 is pushed to the sliding groove 16 by the electric telescopic sleeve rod 1402, the sliding block 15 moves left and right, and meanwhile, the clamping plate 13 is driven to move, so that the size of the clamping plate can be changed according to the sizes of the bottoms of different unmanned aerial vehicles, the unmanned aerial vehicles are more attached, the falling possibility is reduced, the practicability of the protection structure is improved, secondly, the rubber cushion 8 is installed on the sleeve body 1 by screwing the first fixing bolt 9 clockwise, so that the protection structure effectively protects both sides, increase unmanned aerial vehicle's life, install cystosepiment 10 through fixture block 11 and draw-in groove 12 at last.

To sum up, this protective structure can reach the purpose that changes self size, makes it can change the size of self according to different unmanned aerial vehicle's size, increases this protective structure's practicality.

It is noted that, herein, relational terms such as first and second, and the like may be used solely to distinguish one entity or action from another entity or action without necessarily requiring or implying any actual such relationship or order between such entities or actions. Also, the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a wing protective structure for unmanned aerial vehicle, includes cover body (1) and cystosepiment (10), its characterized in that: the connecting block (2) is installed on two sides of the sleeve body (1), a wing shell (3) is arranged on one side of the connecting block (2), a rotating shaft (4) is installed on one side of the wing shell (3), an upper blocking cover (5) is arranged on one side of the rotating shaft (4), a fixed block (6) is arranged on one side of the upper blocking cover (5), a fixed groove (7) is arranged on the other side of the fixed block (6), a rubber cushion (8) is arranged on one side of the fixed groove (7), a first fixing bolt (9) is arranged inside the rubber cushion (8), the foam board (10) is installed below the outer portion of the sleeve body (1), a clamping block (11) is welded on one side of the foam board (10), the other side of the clamping block (11) is arranged on a clamping groove (12), a clamping plate (13) is arranged above the outer portion of the clamping groove (12), a telescopic mechanism (14) is arranged on one side of the clamping plate (13), telescopic machanism (14) one side is provided with slider (15), slider (15) outside is provided with spout (16), regulating plate (17) one side is seted up in spout (16), regulating plate (17) outside below is provided with mounting panel (18), mounting panel (18) both sides all are provided with second fixing bolt (19).

2. The wing protection structure for the unmanned aerial vehicle as claimed in claim 1, wherein: the upper blocking cover (5), the rotating shaft (4) and the wing shell (3) form a rotating structure, and the upper blocking cover (5) and the wing shell (3) are distributed in parallel.

3. The wing protection structure for the unmanned aerial vehicle as claimed in claim 1, wherein: the upper blocking cover (5) is connected with the wing shell (3) in a clamping mode through the fixing block (6), and the fixing block (6) is matched with the fixing groove (7) in size.

4. The wing protection structure for the unmanned aerial vehicle as claimed in claim 1, wherein: the rubber cushion (8) is in threaded connection with the wing shell (3) through first fixing bolts (9), and the number of the first fixing bolts (9) is four.

5. The wing protection structure for the unmanned aerial vehicle as claimed in claim 1, wherein: the foam plate (10) is connected with the sleeve body (1) in a clamping mode through a clamping block (11), and the clamping block (11) is matched with the clamping groove (12) in size.

6. The wing protection structure for the unmanned aerial vehicle as claimed in claim 1, wherein: the telescopic mechanism (14), the sliding block (15) and the sliding groove (16) form a sliding structure, and the sliding block (15) is symmetrically arranged by the central axis of the sliding groove (16).

7. The wing protection structure for the unmanned aerial vehicle as claimed in claim 1, wherein: the mounting plate (18) is in threaded connection with the sleeve body (1) through second fixing bolts (19), and the number of the second fixing bolts (19) is eight.