Quick disassembly and assembly structure of unmanned aerial vehicle

Abstract

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle quick disassembly and assembly structure which comprises an unmanned aerial vehicle, a flying platform, a button and a lock catch. The flying platform is arranged at the bottom of the unmanned aerial vehicle, the button is pressed down, the lock catch pops up and is clamped to the bottom of the unmanned aerial vehicle, so that the unmanned aerial vehicle is fixed to the flying platform, the lock catch is pressed down, the button pops up and resets, the unmanned aerial vehicle is detached from the flying platform, and through cooperative use of the lock catch and the button, the unmanned aerial vehicle and the flying platform can be rapidly disassembled and assembled. The unmanned aerial vehicle and the flying platform can be quickly assembled without tools, tools such as screwdrivers are not needed, and the problems that an existing unmanned aerial vehicle and an existing flying platform need to be disassembled and assembled according to the use basis, and operation is troublesome are solved.

Description

Technical Field

[0001] The utility model relates to the technical field of unmanned aerial vehicles, in particular to a quick-disassembly and quick-assembly structure of an unmanned aerial vehicle. Background Art

[0002] With the development of science and technology, drone technology has rapidly developed and popularized. Both military and civilian drones have made great progress and are widely used in various industries, such as military reconnaissance, agricultural pesticide spraying, aerial photography, remote control toys, etc.

[0003] In order to ensure the convenience and safety of storage and transportation, drone products generally adopt a modular design, that is, the entire drone can be disassembled into multiple modules such as the fuselage, wings, tail, flight platform, and payload. During use, rapid assembly and disassembly can be achieved by operating the relevant disassembly and locking mechanisms.

[0004] Currently, the common quick disassembly and assembly structures on the market mainly include threaded locking, axle pins or butterfly locks. The disassembly and installation between the flight platform of the drone and the drone require the use of tools such as screwdrivers, which is rather troublesome. Utility Model Content

[0005] The utility model aims to provide a quick disassembly and assembly structure for a UAV, aiming to solve the problem that the disassembly and assembly of the existing UAV and the flight platform requires use of a base and is troublesome to operate.

[0006] To achieve the above-mentioned purpose, the utility model provides a UAV quick-disassembly and quick-assembly structure, comprising a UAV, a flight platform, a button and a lock; the flight platform is arranged at the bottom of the UAV, the button is arranged on one side of the flight platform, and the lock is arranged on one side of the flight platform.

[0007] The button includes a button body and a first spring. The button body is slidably connected to the flying platform and passes through the flying platform. The first spring is sleeved on the outside of the button body.

[0008] Among them, the lock includes a lock body, a slide plate and a second spring. The lock body is slidably connected to the flying platform and passes through the flying platform. The slide plate is fixedly connected to the lock body and is located in the flying platform. The second spring is arranged on the side of the slide plate away from the lock body.

[0009] Wherein, the flying platform has a groove, and the groove is located on one side of the flying platform.

[0010] The utility model discloses a quick-disassembly and quick-assembly structure for a UAV, wherein the flight platform is arranged at the bottom of the UAV, and the user presses the button, the lock pops out and is engaged with the bottom of the UAV, so that the UAV is fixed on the flight platform, and the lock is pressed, the button pops out and resets, and the UAV is removed from the flight platform. The UAV and the flight platform can be quickly disassembled and assembled by the coordinated use of the lock and the button. The quick-disassembly and quick-assembly structure is tool-free and does not require the use of tools such as screwdrivers, and can realize the quick assembly and assembly of the UAV and the flight platform, thereby solving the problem that the existing UAV and the flight platform need to be disassembled and assembled using a base and are cumbersome to operate. BRIEF DESCRIPTION OF THE DRAWINGS

[0011] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art are briefly introduced below.

[0012] Figure 1 The utility model is a structural schematic diagram of a quick-disassembly and quick-assembly structure of an unmanned aerial vehicle.

[0013] Figure 2 The utility model is a bottom view of a UAV quick-disassembly and quick-assembly structure without the UAV.

[0014] Figure 3 The utility model is a top view of a UAV quick-disassembly and quick-assembly structure without the UAV.

[0015] Figure 4 The utility model is a schematic diagram of a UAV and a flight platform with a UAV quick-disassembly and quick-assembly structure.

[0016] In the figure: 1-unmanned aerial vehicle, 2-flying platform, 3-button, 4-lock, 5-button body, 6-first spring, 7-lock body, 8-slide plate, 9-second spring, 10-groove. DETAILED DESCRIPTION

[0017] The embodiments of the present invention are described in detail below, and examples of the embodiments are shown in the accompanying drawings, wherein the same or similar reference numerals throughout represent the same or similar elements or elements having the same or similar functions. The embodiments described below with reference to the accompanying drawings are exemplary and are intended to be used to explain the present invention, and should not be construed as limiting the present invention.

[0018] See also Figures 1 to 4 The utility model provides a quick-disassembly and quick-assembly structure of a UAV, comprising a UAV 1, a flight platform 2, a button 3 and a lock 4; the flight platform 2 is arranged at the bottom of the UAV 1, the button 3 is arranged on one side of the flight platform 2, and the lock 4 is arranged on one side of the flight platform 2.

[0019] In this embodiment, the flying platform 2 is arranged at the bottom of the drone 1. When the user presses the button 3, the lock 4 pops out and is locked at the bottom of the drone 1, so that the drone 1 is fixed on the flying platform 2. When the lock 4 is pressed, the button 3 pops out and resets, and the drone 1 is removed from the flying platform 2. Through the coordinated use of the lock 4 and the button 3, the drone 1 and the flying platform 2 can be quickly disassembled and assembled. The quick-disassembly and quick-assembly structure is tool-free and does not require the use of tools such as screwdrivers. The drone 1 and the flying platform 2 can be quickly assembled and assembled, which solves the problem that the existing drones and flying platforms need to be disassembled and assembled with a tool and are cumbersome to operate.

[0020] Furthermore, the button 3 includes a button body 5 and a first spring 6 . The button body 5 is slidably connected to the flying platform 2 and passes through the flying platform 2 . The first spring 6 is sleeved on the outside of the button body 5 .

[0021] In this embodiment, the button body 5 is pressed, and the button body 5 compresses the first spring 6 and extends out from the through hole of the lock buckle 4. At this time, the lock buckle 4 pops out and clamps the bottom of the drone 1, thereby fixing the drone 1 and the flight platform 2, that is, installing the drone 1. At this time, the lock buckle 4 also limits the button body 5.

[0022] Furthermore, the lock 4 includes a lock body 7, a slide plate 8 and a second spring 9. The lock body 7 is slidably connected to the flying platform 2 and passes through the flying platform 2. The slide plate 8 is fixedly connected to the lock body 7 and is located in the flying platform 2. The second spring 9 is arranged on the side of the slide plate 8 away from the lock body 7.

[0023] In this embodiment, the lock body 7 is pressed down to make the slide plate 8 slide and squeeze the second spring 9. At the same time, the lock body 7 removes the clamping connection with the bottom of the drone 1 and also removes the limit on the button body 5. At this time, the first spring 6 is reset, so that the button body 5 pops out of the flight platform 2 and resets.

[0024] Furthermore, the flying platform 2 has a groove 10 , and the groove 10 is located on one side of the flying platform 2 .

[0025] In this embodiment, the groove 10 is provided to clamp the bottom of the drone 1 and enhance the stability of the installation and fixation of the flying platform 2 and the drone 1 .

[0026] When the UAV 1 and the flying platform 2 are disassembled and assembled, the user presses the button body 5 to compress the first spring 6 and extend it out from the through hole of the lock body 7. At this time, the lock body 7 pops out and clamps the bottom of the UAV 1, thereby fixing the UAV 1 and the flying platform 2, that is, installing the UAV 1. The user presses the lock body 7 with his hand to make the slide 8 slide and squeeze the second spring 9. At the same time, the lock body 7 removes the clamping connection with the bottom of the UAV 1 and also removes the limit of the button body 5. At this time, the first spring 6 is reset, so that the button body 5 pops out of the flying platform 2 and resets, and the UAV 1 is removed from the flying platform 2.

[0027] The above disclosure is only a preferred embodiment of the quick-disassembly and quick-assembly structure of a drone of the present application, and cannot be used to limit the scope of rights of the present application. Ordinary technicians in this field can understand that all or part of the processes of implementing the above embodiments and equivalent changes made according to the claims of the present application are still within the scope covered by the present application.

Claims

1. A quick-disassembly and quick-assembly structure for a drone, characterized in that: Including drones, flying platforms, buttons and locks; The flying platform is arranged at the bottom of the UAV, the button is arranged at one side of the flying platform, and the lock is arranged at one side of the flying platform.

2. The quick-disassembly and quick-assembly structure of a drone as claimed in claim 1, characterized in that: The button comprises a button body and a first spring. The button body is slidably connected to the flying platform and penetrates the flying platform. The first spring is sleeved on the outer side of the button body.

3. The quick-disassembly and quick-assembly structure of a drone as claimed in claim 2, characterized in that: The lock includes a lock body, a slide plate and a second spring. The lock body is slidably connected to the flying platform and passes through the flying platform. The slide plate is fixedly connected to the lock body and is located in the flying platform. The second spring is arranged on the side of the slide plate away from the lock body.

4. The quick-disassembly and quick-assembly structure of a drone as claimed in claim 1, characterized in that: The flying platform has a groove, and the groove is located at one side of the flying platform.

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