CN219008124U

CN219008124U - Installation quick detach structure of unmanned aerial vehicle module

Info

Publication number: CN219008124U
Application number: CN202223246900.3U
Authority: CN
Inventors: 雷进; 韩恒刚; 易剑南
Original assignee: Henan Yunhuan Netlink Uav Technology Co ltd
Current assignee: Henan Yunhuan Netlink Uav Technology Co ltd
Priority date: 2022-12-05
Filing date: 2022-12-05
Publication date: 2023-05-12
Anticipated expiration: 2032-12-05

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an installation quick-release structure of an unmanned aerial vehicle module, which comprises a main body and a module body, wherein the module body is installed on the main body through a connecting component, the connecting component comprises an installation box and installation frames positioned at two ends of the installation box, and the installation frames are provided with installation holes. The utility model has the advantages of simple structure and convenient and quick disassembly.

Description

Installation quick detach structure of unmanned aerial vehicle module

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an installation quick-release structure of an unmanned aerial vehicle module.

Background

Along with the development of science and technology, unmanned aerial vehicle technology rapidly develops and prevails, and both military and civil unmanned aerial vehicles have great progress and are widely applied to various industries, such as military investigation, agricultural pesticide spraying, aerial photography, remote control toys and the like.

At present, unmanned aerial vehicle module adopts the connection form of screw fastening generally, and the superior performance of large-scale unmanned aerial vehicle makes its material selection material attach importance to the lightweight of spare part fairly. Therefore, the unmanned aerial vehicle has the advantages that the unmanned aerial vehicle is required to be lost, the fuselage screws are extremely light and are not easy to detach frequently due to the fact that materials are selected, otherwise, the problems of slipping and the like occur easily, flight work is affected, flight safety is reduced, and therefore the unmanned aerial vehicle module is required to be installed and quickly detached.

Disclosure of Invention

In order to solve the technical problems, the utility model adopts the following technical scheme.

The utility model provides an installation quick detach structure of unmanned aerial vehicle module, includes fuselage main part and module body, the module body passes through coupling assembling and installs in the fuselage main part, coupling assembling includes the mounting bracket at mounting box both ends with being located the mounting bracket be equipped with the mounting hole on the mounting bracket.

Preferably, the top of module body is equipped with coupling assembling complex connecting portion, connecting portion include the connecting block and be located the fixed plate at connecting block both ends, the fixed plate passes through fixing bolt to be fixed on the module body.

Preferably, the top of connecting block is equipped with the constant head tank offer the socket on the both sides wall of constant head tank the buckling groove with constant head tank matched with is offered to the bottom of mounting box the opening has been offered respectively on the both sides wall that the buckling groove is relative be located the both sides inner wall punishment that is close to the open-ended in the buckling groove be equipped with the movable block respectively the bottom of movable block is equipped with the fixture block that corresponds the complex with the socket be connected with the clamp plate on the movable block of fixture block below, the clamp plate extends the opening be located the both ends of movable block respectively in the buckling groove be equipped with the separate piece separate be connected with compression spring between the both ends of separate piece and every movable block respectively.

Preferably, the separation block is in a T-shaped arrangement and is fixed in the buckling groove through a mounting bolt.

Preferably, the outer end surface of the clamping block is obliquely arranged.

Preferably, the fixing plate and the mounting frame are respectively provided with a lightening hole.

The utility model has the beneficial effects that:

according to the utility model, the module body is fixedly arranged on the main body of the machine body through the connecting assembly fixed on the main body of the machine body, and the clamping block is clamped in the socket through the matching of the sleeved buckling groove and the positioning groove, the clamping block, the socket, the compression spring and the pressing plate, so that the purpose of quick assembly and disassembly of the module body is realized; the quick-release structure does not occupy the original mounting of the aircraft, is convenient for boxing and transferring operation, reduces the traditional screw connection mode, and frequently disassembles the structure affecting the aircraft.

Drawings

FIG. 1 is a schematic view of the mounting structure of a module body and a fuselage body;

FIG. 2 is a schematic overall construction of the structure of the present utility model;

FIG. 3 is a schematic top view of the present utility model;

FIG. 4 is a schematic structural view of the connection assembly;

FIG. 5 is a schematic view of the internal structure of the connection assembly;

FIG. 6 is a schematic view of the mounting structure of the module body and the connection portion;

the reference numerals in the figures are: the device comprises a mounting box 1, a mounting frame 2, a mounting hole 3, a weight reducing hole 4, a fixing plate 5, a machine body 6, an opening 7, a pressing plate 8, a connecting block 9, a module body 10, a moving block 11, a clamping block 12, a separating block 13, a compression spring 14, a buckling groove 15, a positioning groove 16 and a jack 17.

Detailed Description

The preferred embodiments of the present utility model will be described below with reference to the accompanying drawings, it being understood that the preferred embodiments described herein are for illustration and explanation of the present utility model only, and are not intended to limit the present utility model.

Example 1

The utility model provides an unmanned aerial vehicle module's installation quick detach structure, as shown in fig. 1 through 6, includes fuselage main part 6 and module body 10, and module body 10 passes through coupling assembling and installs on fuselage main part 6, and coupling assembling includes mounting box 1 and is located mounting bracket 2 at mounting box 1 both ends, is equipped with mounting hole 3 on mounting bracket 2, can fix mounting bracket 2 on fuselage main part 6 through the mounting hole.

The top of the module body 10 is provided with a connecting part matched with the connecting component, the connecting part comprises a connecting block 9 and fixing plates 5 positioned at two ends of the connecting block 9, and the fixing plates 5 are fixed on the module body 10 through fixing bolts.

In order to relieve the flight pressure, weight reducing holes 4 are respectively formed in the fixing plate 5 and the mounting frame 2.

The top of connecting block 9 is equipped with constant head tank 16, socket 17 has been seted up on the both sides wall of constant head tank 16, the buckling groove 15 with constant head tank 16 matched with has been seted up in the bottom of mounting box 1, open-ended 7 has been seted up respectively on the both sides wall that buckling groove 15 is relative, be located the both sides inner wall punishment of next opening 7 in buckling groove 15 and be equipped with movable block 11, be equipped with the fixture block 12 with socket 17 corresponding matched with in the bottom of movable block 11, the outer terminal surface slope setting of fixture block 12, be connected with clamp plate 8 on the movable block 11 of fixture block 12 below, clamp plate 8 extends open-ended 7, both ends that are located movable block 11 in buckling groove 15 are equipped with separately separating block 13, separating block 13 is T shape setting, and fix in buckling groove 15 through the mounting bolt. Compression springs 14 are respectively connected between both ends of the separation block 13 and each of the moving blocks 11. When the module body 10 is installed, the positioning groove 16 is placed in the buckling groove 15, the module body 10 is pressed downwards slightly with force, then the socket 17 moves downwards along the inclined plane of the clamping block 12, so that the clamping block 12 is clamped into the socket 17, and the module body 10 is quickly installed on the connecting assembly.

The working mode of the utility model is as follows: before installation, the installation frame 2 is installed on the body 10 through the installation hole 3; when the module body 10 is installed, the positioning groove 16 is downwards aligned with the buckling groove 15, so that the module body is inserted into the buckling groove 15, then the module body is slightly pressed downwards with force, when the outer wall of the positioning groove 16 is in contact with the clamping block 8, the outer wall of the positioning groove 16 extrudes the clamping block 8, the compression spring 14 is compressed until the clamping block 8 is clamped into the socket 7, and the compression spring 14 is reset at the moment, so that the connecting block 15 is clamped with the installation box 1, the module body 10 is installed on a connecting assembly, and the module body 10 is installed on the body 10; when the module is disassembled, the two pressing plates 8 are pinched by hands, the compression springs 14 are in a compressed state, the clamping blocks 8 are separated from the insertion openings 7, the buckling grooves 15 and the positioning grooves 16 are separated from the clamping relation, and the module body 10 is taken out, so that the module body 10 can be quickly disassembled and assembled.

Finally, it should be noted that: the foregoing description is only a preferred embodiment of the present utility model, and is not intended to limit the present utility model, but although the present utility model has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that modifications may be made to the technical solutions described in the foregoing embodiments, or equivalents may be substituted for some of the technical features thereof; any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present utility model should be included in the protection scope of the present utility model.

Claims

1. The utility model provides an unmanned aerial vehicle module's installation quick detach structure, includes fuselage main part (6) and module body (10), its characterized in that, module body (10) are installed on fuselage main part (6) through coupling assembling, coupling assembling includes mounting box (1) and is located mounting bracket (2) at mounting box (1) both ends be equipped with mounting hole (3) on mounting bracket (2);

the top of the module body (10) is provided with a connecting part matched with the connecting component, the connecting part comprises a connecting block (9) and fixing plates (5) positioned at two ends of the connecting block (9), and the fixing plates (5) are fixed on the module body (10) through fixing bolts;

the top of connecting block (9) is equipped with constant head tank (16) jack (17) have been seted up on the both sides wall of constant head tank (16) the bottom of mounting box (1) seted up with constant head tank (16) matched with buckling groove (15) open-ended (7) have been seted up respectively on the both sides wall that buckling groove (15) are relative buckling groove (15) are located the both sides inner wall department of next opening (7) and are equipped with movable block (11) respectively the bottom of movable block (11) is equipped with fixture block (12) corresponding to jack (17) be connected with clamp plate (8) on movable block (11) of fixture block (12) below, clamp plate (8) extend opening (7) be located the both ends of movable block (11) in buckling groove (15) are equipped with separately separating block (13) be connected with compression spring (14) respectively between the both ends of separating block (13) and every movable block (11).

2. The unmanned aerial vehicle module mounting and quick-release structure of claim 1, wherein: the separation block (13) is T-shaped and is fixed in the buckling groove (15) through a mounting bolt.

3. The unmanned aerial vehicle module mounting and quick-release structure of claim 1, wherein: the outer end face of the clamping block (12) is obliquely arranged.

4. The unmanned aerial vehicle module mounting and quick-release structure of claim 2, wherein: weight reducing holes (4) are respectively formed in the fixing plate (5) and the mounting frame (2).