Unmanned aerial vehicle supporting rod switching structure

Abstract

The utility model discloses an unmanned aerial vehicle supporting rod switching structure, and relates to the technical field of unmanned aerial vehicles. Comprising a supporting rod, wing mechanisms and a supporting rod switching mechanism, the wing mechanisms are arranged on the two sides of the supporting rod, the supporting rod switching mechanism is arranged in the supporting rod and used for wiring connection of electric wires, each wing mechanism comprises a plurality of wing bodies, the wing bodies are arranged on the two sides of the supporting rod, and the side, close to the supporting rod, of each wing body is fixedly connected with a wing bottom skin. Through the arrangement of the supporting rod, the wing mechanism and the switching mechanism, the equipment can be quickly disassembled during transportation, so that the occupied area of the equipment can be reduced when the equipment is used, the possibility that the equipment is damaged is reduced, the use cost of the equipment is ensured, and the equipment can achieve a good use effect when being used; and the convenience of the equipment is improved, the practicability of the equipment is improved, and the applicability of the equipment is improved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a support pole transfer structure for unmanned aerial vehicles. Background Art

[0002] The strut is an important body structure of the electric vertical take-off and landing UAV, which is used to carry the propeller components and is connected to the wings. However, part of the strut structure may not be well stored due to the influence of the wings during transportation, resulting in more space being occupied during transportation, and may also cause damage during transportation, resulting in the need for repairs and increasing the cost of using the equipment. Therefore, the utility model proposes a new solution. Utility Model Content

[0003] The purpose of the utility model is to provide a UAV support pole switching structure to solve the problems raised in the above-mentioned background technology.

[0004] To achieve the above purpose, the utility model provides the following technical solution: a UAV support pole transfer structure, comprising:

[0005] poles;

[0006] The wing mechanism is arranged on both sides of the strut.

[0007] A support rod switching mechanism, which is arranged inside the support rod and is used for connecting the wire routing;

[0008] The wing mechanism includes:

[0009] Multiple wing bodies, each wing body is arranged on both sides of the strut, each wing body is fixedly connected to a wing bottom skin on one side close to the strut, one side surface of the wing bottom skin and the strut are movably connected, a wing aid is installed on the other side of each wing bottom skin, and multiple wing metal parts are installed on the other side of the wing aid, one side of the wing metal part, one side of the wing aid and one side of the wing bottom skin are all provided with matching connection holes, and one side of the wing aid and one side of the wing bottom skin are both provided with matching holes that pass through the other side.

[0010] Preferably, the support rod switching mechanism comprises:

[0011] A support rod adapter is arranged on the inner wall of the support rod. A connecting hole is opened on one side of the support rod adapter and passes through the other side. A connecting tube is installed on the inner wall of each connecting hole. Both ends of each connecting tube pass through the support rod to the outer surface. The outer surfaces at both ends of each connecting tube are movably connected to the inner walls of multiple corresponding connecting holes.

[0012] Preferably, one end of the strut adapter is provided with a plurality of wire holes passing through the other end, one side of the strut adapter and one side of the strut are both provided with wire holes passing through the other side, and the wire holes on one side of the strut adapter and the wire holes on one side of the strut and the adapter holes on one side of the wing auxiliary skin and one side of the wing bottom skin are connected.

[0013] Preferably, the top end of the support rod and the top end of the support rod adapter are both provided with a plurality of pin holes penetrating through the bottom end, and a quick-release pin is installed inside each pin hole.

[0014] Preferably, threaded holes are provided on one side of both sides of the support rod adapter and on one side of both sides of the support rod.

[0015] Preferably, a plurality of through holes are provided on one side of the wing auxiliary skin and one side of the wing bottom skin, and a bolt is provided on the inner wall of each through hole, and one end of the bolt surface is screwed to the inner wall of the threaded hole on both sides of the strut adapter and the strut.

[0016] Compared with the prior art, the beneficial effects of the utility model are:

[0017] The UAV strut adapter structure, through the arrangement of the strut, the wing mechanism, and the adapter mechanism, enables the equipment to be quickly disassembled during transportation, so that the equipment can reduce the occupied area of ​​the equipment when in use, reduce the possibility of damage to the equipment, ensure the use cost of the equipment, ensure that the equipment can achieve good use effect when in use, increase the convenience of the equipment, increase the practicality of the equipment, and increase the applicability of the equipment.

[0018] At the same time, through the provision of wire holes, convenient wiring can be achieved when the device is in use, so that the wires can be conveniently connected when the device is in use, which facilitates convenient assembly and installation, increases the convenience of the device, increases the practicality of the device, and increases the applicability of the device. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] Figure 1 It is a schematic diagram of the overall axial side structure of the utility model;

[0020] Figure 2 It is a schematic diagram of the overall explosion structure of the utility model;

[0021] Figure 3 It is a schematic diagram of the explosion structure between the support rod and the support rod transfer mechanism of the utility model;

[0022] Figure 4 It is a schematic diagram of the exploded structure of the wing mechanism of the utility model.

[0023] In the figure: 1. strut; 2. wing mechanism; 201. wing body; 202. connecting hole; 203. wing metal part; 204. wing auxiliary; 205. adapter hole; 206. through hole; 207. bolt; 3. strut adapter mechanism; 301. strut adapter; 302. connecting hole; 303. threaded hole; 304. wire hole; 305. connecting tube; 306. quick release pin; 307. pin hole. DETAILED DESCRIPTION

[0024] The following will be combined with the drawings in the embodiments of the utility model to clearly and completely describe the technical solutions in the embodiments of the utility model. Obviously, the described embodiments are only part of the embodiments of the utility model, not all of the embodiments. Based on the embodiments in the utility model, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the utility model.

[0025] The drone support pole transition structure will be used during the use of the drone. The support pole transition structure provided by the utility model is specifically used for fast installation of the equipment during use and disassembly during transportation. The equipment needs to be regularly maintained during use to ensure that the equipment can achieve good use effects during use, and the equipment needs to be wired during use to ensure that the equipment can operate normally during use.

[0026] like Figure 1 - Figure 4 As shown, the utility model provides a technical solution: a UAV support pole 1 switching structure, comprising:

[0027] A strut 1, a wing mechanism 2, the wing mechanism 2 is arranged on both sides of the strut 1, a strut adapter mechanism 3, the strut adapter mechanism 3 is arranged inside the strut 1, and is used for connecting the wiring of the wires. The wing mechanism 2 includes multiple wing bodies 201, each wing body 201 is arranged on both sides of the strut 1, each wing body 201 is fixedly connected with a wing bottom skin on one side close to the strut 1, and a surface of one side of the wing bottom skin is movably connected to the strut 1, and a wing auxiliary 204 is installed on the other side of each wing bottom skin, and multiple wing metal parts 203 are installed on the other side of the wing auxiliary 204, and matching connection holes 202 are opened on one side of the wing metal part 203, one side of the wing auxiliary 204 and one side of the wing bottom skin, and matching holes 205 that pass through the other side are opened on one side of the wing auxiliary 204 and one side of the wing bottom skin.

[0028] Through the setting of this structure, the equipment can be disassembled and installed when in use, which is convenient for transportation and use, ensuring that a good installation effect can be achieved during use, increasing the convenience of the equipment, increasing the practicality of the equipment, and increasing the applicability of the equipment.

[0029] like Figure 3As shown, the support rod adapter mechanism 3 includes a support rod adapter 301, which is arranged on the inner wall of the support rod 1. A connecting hole 302 is opened on one side of the support rod adapter 301 and penetrates the other side. A connecting pipe 305 is installed on the inner wall of each connecting hole 302. Both ends of each connecting pipe 305 penetrate the support rod 1 to the outer surface. Both ends of the outer surface of each connecting pipe 305 are movably connected to the inner walls of multiple corresponding connecting holes 202. One end of the support rod adapter 301 has multiple connecting holes 202 that penetrate the other end. A wire hole 304 is provided on one side of the strut adapter 301 and one side of the strut 1, and the wire hole 304 passing through the other side is provided. The wire hole 304 on one side of the strut adapter 301 is connected with the wire hole 304 on one side of the strut 1 and the adapter hole 205 on one side of the wing auxiliary 204 and one side of the wing bottom skin. The top of the strut 1 and the top of the strut adapter 301 are provided with multiple pin holes 307 passing through the bottom end, and a quick-release pin 306 is installed inside each pin hole 307.

[0030] It should be noted that, through the setting of this structure, the equipment can be disassembled during transportation, etc., ensuring that the occupied area of ​​the equipment can be reduced when in use, making the transportation process more convenient, achieving good use effects, increasing the convenience of the equipment, increasing the practicality of the equipment, and providing good guidance when in use, so that wires and other lines can be well guided when in use, ensuring that wiring can be well performed during use, ensuring that good use effects can be achieved during use, and the equipment can be quickly installed when assembling it, facilitating the quick use of the equipment and increasing the convenience of the equipment.

[0031] like Figure 4 As shown, threaded holes 303 are provided on one side of both sides of the strut adapter 301 and one side of both sides of the strut 1, and multiple through holes 206 are provided on one side of the wing auxiliary 204 and one side of the wing bottom skin. A bolt 207 is provided on the inner wall of each through hole 206, and one end of the surface of the bolt 207 is screwed to the inner wall of the threaded holes 303 on both sides of the strut adapter 301 and the strut 1.

[0032] It should be noted that through the setting of this structure, the equipment can be quickly installed when in use, which facilitates the rapid use of the equipment, improves the deployment efficiency of the equipment, increases the practicality of the equipment, increases the convenience of the equipment, and increases the practicality of the equipment.

[0033] Working principle: When the utility model is used, the strut adapter 301 is first positioned and glued to the strut 1; then the connecting tube 305 is passed through the strut 1 and inserted into the connecting hole 302; then the quick-release pin 306 is passed through the strut 1 and the strut adapter 301 to achieve a locking effect, and then the multiple wings are locked to the strut 1 through the bolt 207.

[0034] Although the embodiments of the present invention have been shown and described, it will be understood by those skilled in the art that various changes, modifications, substitutions and variations may be made to the embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is limited by the attached embodiments and their equivalents.

Claims

1. A UAV support pole transfer structure, characterized in that: include: poles; The wing mechanism is arranged on both sides of the strut; A support rod switching mechanism, which is arranged inside the support rod and is used for connecting the wire routing; The wing mechanism includes: Multiple wing bodies, each wing body is arranged on both sides of the strut, each wing body is fixedly connected to a wing bottom skin on one side close to the strut, one side surface of the wing bottom skin and the strut are movably connected, a wing aid is installed on the other side of each wing bottom skin, and multiple wing metal parts are installed on the other side of the wing aid, one side of the wing metal part, one side of the wing aid and one side of the wing bottom skin are all provided with matching connection holes, and one side of the wing aid and one side of the wing bottom skin are both provided with matching holes that pass through the other side.

2. The UAV support pole transfer structure according to claim 1, characterized in that: The support rod switching mechanism comprises: A support rod adapter is arranged on the inner wall of the support rod. A connecting hole is opened on one side of the support rod adapter and passes through the other side. A connecting tube is installed on the inner wall of each connecting hole. Both ends of each connecting tube pass through the support rod to the outer surface. The outer surfaces at both ends of each connecting tube are movably connected to the inner walls of multiple corresponding connecting holes.

3. The UAV support pole adapter structure according to claim 2, characterized in that: One end of the strut adapter is provided with a plurality of wire holes penetrating the other end, one side of the strut adapter and one side of the strut are provided with wire holes penetrating the other side, and the wire holes on one side of the strut adapter and the wire holes on one side of the strut and the adapter holes on one side of the wing auxiliary skin and one side of the wing bottom skin are connected.

4. The UAV support pole transfer structure according to claim 2, characterized in that: The top end of the support rod and the top end of the support rod adapter are both provided with a plurality of pin holes penetrating through the bottom end, and a quick-release pin is installed inside each pin hole.

5. The UAV support pole transfer structure according to claim 2, characterized in that: Threaded holes are provided on one side of both sides of the support rod adapter and one side of both sides of the support rod.

6. The UAV support pole transfer structure according to claim 5, characterized in that: A plurality of through holes are provided on one side of the wing auxiliary and one side of the wing bottom skin, and a bolt is provided on the inner wall of each through hole. One end of the bolt surface is screwed to the inner wall of the threaded hole on both sides of the strut adapter and the strut.

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