CN219524254U

CN219524254U - Unmanned aerial vehicle with anticollision structure

Info

Publication number: CN219524254U
Application number: CN202320575985.5U
Authority: CN
Inventors: 王静静; 马铭钰
Original assignee: Xuzhou Yangfan Qihang Intelligent Technology Co ltd
Current assignee: Xuzhou Yangfan Qihang Intelligent Technology Co ltd
Priority date: 2023-03-22
Filing date: 2023-03-22
Publication date: 2023-08-15
Anticipated expiration: 2033-03-22

Abstract

The utility model discloses an unmanned aerial vehicle with an anti-collision structure, which comprises a body, a mounting rod and a shock absorption box, wherein the mounting rod is welded on the outer surface of the body, a sliding groove is formed in the inner surface of the mounting rod, a sliding block is embedded in the inner surface of the sliding groove, the shock absorption box is welded on the outer surface of the sliding block, a sliding plate is embedded in the inner surface of the shock absorption box, a connecting rod is welded on the outer surface of the sliding plate, a rubber pad is arranged on the outer surface of the connecting rod, a mounting sleeve is welded on the inner surface of the shock absorption box, a fixing sleeve is welded on the outer surface of the sliding plate, and a shock absorption spring is embedded in the inner surface of the mounting sleeve. According to the unmanned aerial vehicle with the anti-collision structure, firstly, the rubber pad is welded on the upper surface of the sliding plate through the connecting rod, the installation sleeve is matched with the installation of the damping spring in the fixed sleeve, and meanwhile, the damper is used for being installed, so that the effect of damping protection can be achieved when the unmanned aerial vehicle collides and collides, and the unmanned aerial vehicle can be prevented from influencing the normal operation of the unmanned aerial vehicle when the unmanned aerial vehicle collides.

Description

Unmanned aerial vehicle with anticollision structure

Technical Field

The utility model belongs to the technical field of unmanned aerial vehicles, and particularly relates to an unmanned aerial vehicle with an anti-collision structure.

Background

The drone is an unmanned aircraft that is maneuvered using a radio remote control device and a self-contained programming device, or is operated autonomously, either entirely or intermittently, by an on-board computer. Unmanned aerial vehicle controls through radio remote control equipment, carries out practical application in fields such as take photo by plane, agriculture, plant protection, miniature auto heterodyne, express delivery transportation, disaster relief, observe wild animal, monitor infectious disease, survey, news report, electric power inspection, rescue, film and television shooting, make romantic etc..

Unmanned aerial vehicle often causes unmanned aerial vehicle's phenomenon of colliding with and striking because of operator's operation carelessness or because of topography and air current etc. at the flight in-process, causes the damage of certain degree to unmanned aerial vehicle's rotor and fuselage, leads to unmanned aerial vehicle to suffer the damage, causes the danger of crash to can have caused the influence to work. Therefore, we propose an unmanned aerial vehicle with crashproof structure.

Disclosure of Invention

The utility model aims to provide an unmanned aerial vehicle with an anti-collision structure, which can effectively solve the problems in the background technology.

In order to achieve the above purpose, the technical scheme adopted by the utility model is as follows:

the utility model relates to an unmanned aerial vehicle with an anti-collision structure, which comprises a body, a mounting rod and a shock absorption box, wherein the mounting rod is welded on the outer surface of the body, the inner surface of the mounting rod is provided with a sliding groove, the inner surface of the sliding groove is embedded with a sliding block, the shock absorption box is welded on the outer surface of the sliding block, the inner surface of the shock absorption box is embedded with a sliding plate, the outer surface of the sliding plate is welded with a connecting rod, the outer surface of the connecting rod is provided with a rubber pad, the outer surface of the mounting rod is welded with a mounting seat, the inner surface of the mounting seat is provided with a wing, the inner surface of the shock absorption box is welded with a mounting sleeve, the inner surface of the mounting sleeve is embedded with a shock absorption spring, the rubber pad is welded on the upper surface of the sliding plate through the connecting rod, and the mounting sleeve is matched with the inner shock absorption spring of the mounting sleeve, and the shock absorption protection effect can be achieved when the unmanned aerial vehicle collides and collides, and the unmanned aerial vehicle can be prevented from influencing normal operation of the unmanned aerial vehicle when the unmanned aerial vehicle collides.

Preferably, the inner surface of the shock absorption box is welded with a sliding sleeve, the outer surface of the sliding plate is welded with a positioning sliding rod, and the outer surface of the positioning sliding rod is in sliding connection with the inner surface of the sliding sleeve.

Preferably, a connecting plate is welded on the inner surface of the sliding sleeve, a damper is arranged on the outer surface of the connecting plate, and the outer surface of the damper is connected with the outer surface of the positioning sliding rod.

Preferably, the installation pole internal surface is provided with the recess, recess internal surface welding has the rotation sleeve, it has the threaded rod to rotate sleeve internal surface gomphosis, threaded rod external surface welding has the regulating block, sliding block internal surface welding has the screw sleeve, threaded rod external surface and screw sleeve internal surface threaded connection, through rotatory regulating block, drive the threaded rod and rotate, then utilize threaded connection between threaded rod external surface and the screw sleeve internal surface, drive the sliding block and carry out directional slip in the sliding tray inside to conveniently adjust the position of damper box, thereby can adjust the position of damper box according to the size of wing, thereby conveniently protect the wing of equidimension.

The utility model has the following beneficial effects:

1. according to the utility model, the rubber pad is welded on the upper surface of the sliding plate through the connecting rod, the installation sleeve is matched with the installation of the damping spring in the fixed sleeve, and meanwhile, the damper is used for being installed, so that the damping protection effect can be achieved when the unmanned aerial vehicle collides and collides, and the unmanned aerial vehicle can be prevented from influencing the normal operation of the unmanned aerial vehicle when the unmanned aerial vehicle collides.

2. According to the wing protection device, the adjusting block is rotated to drive the threaded rod to rotate, and then the sliding block is driven to directionally slide in the sliding groove by utilizing the threaded connection between the outer surface of the threaded rod and the inner surface of the threaded sleeve, so that the position of the damping box can be conveniently adjusted, the position of the damping box can be adjusted according to the size of the wing, and the wings with different sizes can be conveniently protected.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present utility model, the drawings that are needed for the description of the embodiments will be briefly described below, and it is obvious that the drawings in the following description are only some embodiments of the present utility model, and that other drawings may be obtained according to these drawings without inventive effort for a person skilled in the art.

Fig. 1 is a schematic diagram of the overall structure of an unmanned aerial vehicle with an anti-collision structure according to the present utility model;

fig. 2 is a schematic diagram of a front view structure of an unmanned aerial vehicle with an anti-collision structure according to the present utility model;

FIG. 3 is a schematic view of the cross-sectional structure A-A in FIG. 2;

FIG. 4 is an enlarged partial view of portion A of FIG. 3;

fig. 5 is a schematic top view of an unmanned aerial vehicle with an anti-collision structure according to the present utility model.

In the figure: 1. a body; 2. a mounting rod; 3. a sliding groove; 4. a sliding block; 5. a damper box; 6. a sliding plate; 7. a connecting rod; 8. a rubber pad; 9. a mounting sleeve; 10. a fixed sleeve; 11. a damping spring; 12. positioning a slide bar; 13. a sliding sleeve; 14. a connecting plate; 15. a damper; 16. a groove; 17. rotating the sleeve; 18. a threaded rod; 19. a threaded sleeve; 20. an adjusting block; 21. a mounting base; 22. and (3) a wing.

Detailed Description

The utility model is further described in connection with the following detailed description, in order to make the technical means, the creation characteristics, the achievement of the purpose and the effect of the utility model easy to understand.

In the description of the present utility model, it should be noted that the directions or positional relationships indicated by the terms "upper", "lower", "inner", "outer", "front", "rear", "both ends", "one end", "the other end", etc. are based on the directions or positional relationships shown in the drawings, are merely for convenience of describing the present utility model and simplifying the description, and do not indicate or imply that the devices or elements referred to must have a specific direction, be configured and operated in the specific direction, and thus should not be construed as limiting the present utility model. Furthermore, the terms "first," "second," and the like, are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present utility model, it should be noted that, unless explicitly specified and limited otherwise, the terms "mounted," "provided," "connected," and the like are to be construed broadly, and may be fixedly connected, detachably connected, or integrally connected, for example; can be mechanically or electrically connected; can be directly connected or indirectly connected through an intermediate medium, and can be communication between two elements. The specific meaning of the above terms in the present utility model will be understood in specific cases by those of ordinary skill in the art.

As shown in fig. 1-5, an unmanned aerial vehicle with anticollision structure, including body 1, installation pole 2 and damper 5, installation pole 2 welding is at body 1 surface, installation pole 2 internal surface is provided with sliding tray 3, sliding tray 3 internal surface gomphosis has slider 4, damper 5 welding is at slider 4 surface, damper 5 internal surface gomphosis has sliding plate 6, sliding plate 6 surface welding has connecting rod 7, connecting rod 7 surface mounting has rubber pad 8, installation pole 2 external surface welding has mount pad 21, mount pad 21 internal surface installs wing 22, damper 5 internal surface welding has mount sleeve 9, the welding of sliding plate 6 external surface has fixed sleeve 10, mount sleeve 9 internal surface gomphosis has damping spring 11, damping spring 11 external surface gomphosis has at mount sleeve 9 internal surface, at first with rubber pad 8 welding at sliding plate 6 upper surface through connecting rod 7, the installation of cooperation mount sleeve 9 and the inside damping spring 11 of fixed sleeve 10, the installation that utilizes damper 15 simultaneously can play the shock attenuation guard action when unmanned aerial vehicle takes place to collide with, thereby can avoid when unmanned aerial vehicle's normal work that bumps.

The inner surface of the shock absorption box 5 is welded with a sliding sleeve 13, the outer surface of the sliding plate 6 is welded with a positioning sliding rod 12, and the outer surface of the positioning sliding rod 12 is in sliding connection with the inner surface of the sliding sleeve 13.

The inner surface of the sliding sleeve 13 is welded with a connecting plate 14, a damper 15 is arranged on the outer surface of the connecting plate 14, and the outer surface of the damper 15 is connected with the outer surface of the positioning slide rod 12.

The installation pole 2 internal surface is provided with recess 16, recess 16 internal surface welding has rotation sleeve 17, rotation sleeve 17 internal surface gomphosis has threaded rod 18, threaded rod 18 external surface welding has regulating block 20, sliding block 4 internal surface welding has threaded sleeve 19, threaded rod 18 external surface and threaded sleeve 19 internal surface threaded connection, through rotatory regulating block 20, drive threaded rod 18 and rotate, then utilize threaded connection between threaded rod 18 external surface and the threaded sleeve 19 internal surface, drive sliding block 4 and carry out directional slip in sliding tray 3 inside, thereby conveniently adjust the position of damper 5, thereby can adjust the position of damper 5 according to the size of wing 22, thereby the convenience protects the wing 22 of equidimension not.

The utility model relates to an unmanned aerial vehicle with an anti-collision structure, which is characterized in that an adjusting block 20 is rotated to drive a threaded rod 18 to rotate, then a sliding block 4 is driven to directionally slide in a sliding groove 3 by utilizing threaded connection between the outer surface of the threaded rod 18 and the inner surface of a threaded sleeve 19, so that the position of a damping box 5 can be adjusted according to requirements, a rubber pad 8 is welded on the upper surface of a sliding plate 6 through a connecting rod 7, the installation of a damping spring 11 in a mounting sleeve 9 and a fixing sleeve 10 is matched, and meanwhile, the installation of a damper 15 is utilized, so that the unmanned aerial vehicle can play a role in damping protection when the unmanned aerial vehicle collides and collides, and the normal operation of the unmanned aerial vehicle can be prevented from being influenced when the unmanned aerial vehicle collides.

The foregoing has shown and described the basic principles and main features of the present utility model and the advantages of the present utility model. It will be understood by those skilled in the art that the present utility model is not limited to the embodiments described above, and that the above embodiments and descriptions are merely illustrative of the principles of the present utility model, and various changes and modifications may be made without departing from the spirit and scope of the utility model, which is defined in the appended claims. The scope of the utility model is defined by the appended claims and equivalents thereof.

Claims

1. Unmanned aerial vehicle with crashproof structure, including body (1), installation pole (2) and damper box (5), its characterized in that: the utility model discloses a mounting rod, including body (1), mounting rod (2) internal surface is provided with sliding tray (3), sliding tray (3) internal surface gomphosis has sliding block (4), shock attenuation case (5) welding is at sliding block (4) surface, shock attenuation case (5) internal surface gomphosis has sliding plate (6), sliding plate (6) external surface welding has connecting rod (7), connecting rod (7) external surface mounting has rubber pad (8), mounting rod (2) external surface welding has mount pad (21), mount pad (21) internal surface mounting has wing (22).

2. The unmanned aerial vehicle with an anti-collision structure according to claim 1, wherein: the inner surface of the shock absorption box (5) is welded with a mounting sleeve (9), and the outer surface of the sliding plate (6) is welded with a fixing sleeve (10).

3. An unmanned aerial vehicle with an anti-collision structure according to claim 2, wherein: the damping spring (11) is embedded on the inner surface of the mounting sleeve (9), and the damping spring (11) is embedded on the inner surface of the mounting sleeve (9) on the outer surface.

4. The unmanned aerial vehicle with an anti-collision structure according to claim 1, wherein: the inner surface of the shock absorption box (5) is welded with a sliding sleeve (13), the outer surface of the sliding plate (6) is welded with a positioning sliding rod (12), and the outer surface of the positioning sliding rod (12) is in sliding connection with the inner surface of the sliding sleeve (13).

5. The unmanned aerial vehicle with anti-collision structure according to claim 4, wherein: the inner surface of the sliding sleeve (13) is welded with a connecting plate (14), a damper (15) is arranged on the outer surface of the connecting plate (14), and the outer surface of the damper (15) is connected with the outer surface of the positioning sliding rod (12).

6. The unmanned aerial vehicle with an anti-collision structure according to claim 1, wherein: the mounting rod (2) internal surface is provided with recess (16), recess (16) internal surface welding has rotation sleeve (17), rotation sleeve (17) internal surface gomphosis has threaded rod (18), threaded rod (18) external surface welding has regulating block (20).

7. The unmanned aerial vehicle with anti-collision structure according to claim 6, wherein: the inner surface of the sliding block (4) is welded with a threaded sleeve (19), and the outer surface of the threaded rod (18) is in threaded connection with the inner surface of the threaded sleeve (19).