Cabin structure of unmanned aerial vehicle

Abstract

The utility model discloses an unmanned aerial vehicle cabin body structure which comprises a conical top cover, a cabin body, a base and a foot stool, and the conical top cover is fixedly arranged at the top of the cabin body through screws; the foot stool is fixedly arranged at the bottom of the cabin body through a base; the cabin body and the foot stool are connected with the base through screws; the cabin body is composed of a cabin body and a sealing cover plate. An inner cavity of the cabin body is divided and molded into a plurality of cabin grids with different specifications so that different functional modules can be independently installed. According to the utility model, the structure is compact and small, the research and development purposes of rapid replacement, disassembly and assembly are realized, and the cabin body is of a semi-closed isolation cabin frame structure, so that an independent installation space is provided for the installation of each functional module, and the strength of the whole machine body can be effectively improved.

Description

Technical Field

[0001] The utility model belongs to the technical field of unmanned aerial vehicles (UAVs), and in particular relates to a UAV cabin structure. Background Art

[0002] The drone industry has experienced rapid growth in recent years. To better meet the needs of drones in various fields (such as photography, entertainment, inspections, and agricultural production), a wide range of expansion modules (e.g., miniature cameras, measuring instruments, and gripping devices) have emerged. These modules, when fixedly connected to the drone itself, can empower the drone with diverse functions (e.g., miniature cameras for aerial video recording, various measuring instruments for high-altitude detection, and gripping devices for high-altitude object dropping), thereby meeting diverse user needs.

[0003] Therefore, how to achieve a detachable connection between the drone body and the drone expansion module and ensure strength has become a problem that technicians in this field must solve. Utility Model Content

[0004] In view of the problems existing in the prior art, the purpose of the present invention is to provide an unmanned aerial vehicle cabin structure.

[0005] In order to solve the above problems, the present invention adopts the following technical solutions:

[0006] A drone cabin structure comprises a conical top cover, a cabin, a base and a tripod, wherein the conical top cover is fixed to the top of the cabin by screws; the tripod is fixed to the bottom of the cabin by the base; the cabin and the tripod are both connected to the base by screws; the cabin consists of a cabin body and a closed cover; the inner cavity of the cabin body is divided and formed into a plurality of compartments of different specifications for independently installing different functional modules.

[0007] Preferably, there are at least four compartments, namely, the antenna and GPS compartment, the electric adjustment module compartment, the flight control module compartment, and the lithium battery compartment.

[0008] Preferably, each of the compartments is provided with a closed cover.

[0009] Preferably, the closed cover plate and the compartment are a slot-embedded push-pull quick-release structure.

[0010] Preferably, the base has a reserved mounting position for an arm, and the arm mounted on the base can be adjusted in an angle within a range of 90°.

[0011] Preferably, an arm deployment hole is provided on the tripod corresponding to the installation position of the arm.

[0012] Preferably, the position of the closing cover is restricted and fixed by a conical top cover fixed on the top of the cabin body.

[0013] Compared with the prior art, the advantages of the present invention are:

[0014] 1. The utility model has a compact structure, and the cabin body is a semi-enclosed isolation cabin frame structure, which not only provides independent installation space for the installation of each functional module, but also effectively improves the strength of the entire fuselage;

[0015] 2. The base has a reserved mounting position for the arms. The arms mounted on the base can be adjusted within a 90° range. The 90° adjustment means that the arms can be lowered and stored inside the tripod, or raised and deployed for launch. This design facilitates storage, transportation, and carrying. After replacing the tail attachment, the four arms can be automatically deployed, and then launched with the canister launcher.

[0016] 3. Each independent compartment is closed with a slot-embedded push-pull quick-release structure, which facilitates the installation, assembly, inspection, maintenance and data update of the present invention. When disassembling, only the conical top cover needs to be removed, and the closing cover of each compartment can be pushed out separately, thus realizing quick replacement and disassembly. BRIEF DESCRIPTION OF THE DRAWINGS

[0017] Figure 1 This is an exploded view of the utility model;

[0018] Figure 2 This is a schematic diagram of the utility model equipped with an arm in an expanded state;

[0019] Figure 3 This is a schematic diagram of the storage state of the utility model equipped with an organic arm;

[0020] Figure 4 and Figure 5 They are all partial structural schematic diagrams of the present utility model;

[0021] Figure 6 It is a structural schematic diagram of the cabin body of the present utility model. DETAILED DESCRIPTION

[0022] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the embodiments described are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without making creative efforts are within the scope of protection of the present invention.

[0023] like Figure 1-6As shown, the utility model provides a technical solution: an unmanned aerial vehicle cabin structure, which is mainly composed of a conical top cover 1, a cabin 2, a base 3 and a tripod 4. The various components are connected and assembled with each other by screws, that is, the conical top cover 1 is fixed to the top of the cabin 2 by screws, and the tripod 4 is fixed to the bottom of the cabin 2 by the base 3, wherein the cabin 2 and the tripod 4 are both connected to the base 3 by screws.

[0024] The key technical aspect of the present invention is that the cabin 2 comprises a cabin body 20 and a closed cover 21. The interior of the cabin body 20 is divided and formed into at least four compartments 22 of varying sizes for independently installing different functional modules, such as the antenna and GPS compartment, the ESC module compartment, the flight control module compartment, and the lithium battery compartment, to ensure the normal operation of the drone. A detailed design allows for a secure and fast detachable connection. Specifically, the closed cover 21 and compartments 22 utilize a slotted, push-pull, quick-release structure, with each compartment 22 equipped with a closed cover 21. During assembly and disassembly, simply remove the conical top cover 1 and push out the corresponding closed cover 21, allowing for quick replacement and assembly. The closed cover 21 is fixed in position by the conical top cover 1 fixed to the top of the cabin 2. When the conical top cover 1 is screwed to the top of the cabin 2, the closed cover 21 is locked in place in all directions, ensuring a secure assembly without affecting normal operation.

[0025] It is worth mentioning that the base 3 has a reserved installation position for the arm. The arm assembled on the base 3 can be adjusted in an angle within a range of 90°. An arm deployment hole 40 is opened on the tripod 4 corresponding to the installation position of the arm, so that the arm can be extended after being deployed. At the same time, the tripod 4 can still serve as a support to facilitate the launch of the drone.

[0026] The utility model has a compact structure, which achieves the research and development purpose of rapid replacement and disassembly, and the cabin body 20 is a semi-enclosed isolation cabin frame structure, which not only provides independent installation space for the installation of each functional module, but also can effectively improve the strength of the entire fuselage.

[0027] 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 these embodiments without departing from the principles and spirit of the present invention, and the scope of the present invention is defined by the appended claims and their equivalents.

Claims

1. An unmanned aerial vehicle cabin structure, characterized in that: The invention comprises a conical top cover (1), a cabin (2), a base (3) and a tripod (4), wherein the conical top cover (1) is fixed to the top of the cabin (2) by screws; the tripod (4) is fixed to the bottom of the cabin (2) by the base (3); the cabin (2) and the tripod (4) are both connected to the base (3) by screws; the cabin (2) is composed of a cabin body (20) and a closed cover plate (21); the inner cavity of the cabin body (20) is divided and formed into a plurality of compartments (22) of different specifications so as to independently install different functional modules.

2. The unmanned aerial vehicle cabin structure according to claim 1, characterized in that: There are at least four compartments (22), namely, an antenna and GPS compartment, an electric control module compartment, a flight control module compartment, and a lithium battery compartment.

3. The unmanned aerial vehicle cabin structure according to claim 1, characterized in that: Each compartment (22) is equipped with a closed cover (21).

4. The unmanned aerial vehicle cabin structure according to claim 3, characterized in that: The closed cover plate (21) and the compartment (22) are a slot-embedded push-pull quick-release structure.

5. The unmanned aerial vehicle cabin structure according to claim 1, characterized in that: The base (3) has a reserved mounting position for an arm, and the arm mounted on the base (3) can be adjusted in angle within a range of 90°.

6. The unmanned aerial vehicle cabin structure according to claim 1, characterized in that: An arm deployment hole (40) is provided on the tripod (4) corresponding to the mounting position of the arm.

7. The unmanned aerial vehicle cabin structure according to claim 1, characterized in that: The position of the closing cover plate (21) is restricted and fixed by a conical top cover (1) fixed on the top of the cabin body (2).

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