Hanging mechanism and unmanned aerial vehicle

By designing a drone mounting mechanism including electric push rods and motors, the problem of cumbersome distance between load bearing plates and the need for special tools in the existing technology is solved, and convenient disassembly and installation is achieved, and practicality is improved.

CN222682693UActive Publication Date: 2025-03-28TIANJIN EUROPE TOUR TECH CO LTD
View PDF 1 Cites 0 Cited by

Patent Information

Application Number
CN202421535502.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2024-07-02
Publication Date
2025-03-28
Estimated Expiration
2034-07-02

AI Technical Summary

Technical Problem

The existing drone mounting mechanism is complicated when adjusting the distance between the bearing plates, increasing labor force, and the connecting plate needs to be connected to the bottom of the drone through bolts. Disassembly and installation requires special tools to reduce practicality.

Method used

A mounting mechanism including a connecting assembly and a mounting assembly is designed. The connecting plate and the bearing plate can be easily disassembled and installed through an electric push rod and a motor. The rotation of the bidirectional screw makes the distance between the bearing plates adjustable.

Benefits of technology

It realizes convenient disassembly and installation of the connecting plate and the bearing plate, simplifies the process of adjusting the distance between the bearing plates, reduces labor, and improves the practicality of the drone.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN222682693U_ABST
    Figure CN222682693U_ABST
Patent Text Reader

Abstract

The utility model provides a mounting mechanism and an unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles. The mounting mechanism comprises a connecting assembly and a mounting assembly, the electric push rod is correspondingly arranged on one side of the unmanned aerial vehicle body, the connecting base is arranged on one side of the unmanned aerial vehicle body, the output end of the electric push rod is connected to one side of the connecting base in a penetrating mode, and the output end of the electric push rod penetrates through a connecting plate and is separated from the connecting plate, so that the connecting plate can be disassembled and assembled; the connecting plate can be disassembled and assembled without a special tool, use is convenient and fast, the two-way screw is rotated through the motor, the two bearing plates can move relatively through rotation of the two-way screw, goods of different sizes can be fixed, and the practicability is high. And meanwhile, the distance between the two bearing plates can be conveniently adjusted, so that the distance between the two bearing plates can be conveniently adjusted, the labor force is reduced, meanwhile, the connecting plate can be conveniently disassembled and assembled, and the practicability is improved.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] The present application relates to the field of unmanned aerial vehicles (UAVs), and more specifically, to a mounting mechanism and an unmanned aerial vehicle (UAV). Background Art

[0002] A drone refers to an unmanned aircraft controlled by a radio remote control device and a self-contained program control device. With the continuous development of civil drone technology, pesticide drones, food delivery drones, express delivery drones and photography drones have emerged. Basically, they are all based on the original drones and are realized by mounting different functional components through a bottom mounting mechanism. For example, a drone mounting mechanism with Chinese patent application number CN202322773200.8 includes a hanging connecting plate, a limiting hole is penetrated at the bottom of the connecting plate, a positioning nut is installed at the end of the mounting threaded rod, a positioning hole is penetrated at the end of the mounting threaded rod, the positioning hole is opened at the top of the receiving plate, the receiving plate penetrates the stabilizing window, the stabilizing window is penetrated and opened at one end of the top positioning plate, a side bolt is installed with a horizontal thread on one side of the top positioning plate, a track window is penetrated on the top positioning plate, a top bolt is penetrated and installed in the track window, a top nut is installed on the top of the top bolt, and the bottom end of the top bolt is connected and fixed to the top surface of the side blocking plate. The mounting mechanism of the UAV adopts a new structural design. It uses a split adjustable mounting structure to quickly fix functional components that do not have a matching connection structure. It can adapt to functional components of different widths, lengths and heights. The components that make up the mounting structure are all universal parts, and the production and maintenance costs are low.

[0003] However, the above solution still has certain defects: first, it is cumbersome to adjust the distance between the two bearing plates, which increases the labor force; second, the connecting plate needs to be connected to the bottom of the drone by bolts, and disassembly and installation require the use of special tools, which is cumbersome, thereby reducing practicality. Utility Model Content

[0004] In order to make up for the above shortcomings, the present application provides a mounting mechanism and a UAV, aiming to improve the problem in the related technology that adjusting the distance between the two bearing plates is cumbersome and increases labor. Secondly, the connecting plate needs to be connected to the bottom of the UAV by bolts, and disassembly and installation require the use of special tools, which is cumbersome, thereby reducing practicality.

[0005] In a first aspect, an embodiment of the present application provides a mounting mechanism including a connecting component and a mounting component.

[0006] The connecting component includes a drone body, an electric push rod and a connecting seat, the electric push rod is correspondingly arranged on one side of the drone body, the connecting seat is arranged on one side of the drone body, the output end of the electric push rod is connected through one side of the connecting seat, the mounting component includes a concave plate, a connecting plate, a motor, a bidirectional screw and a bearing plate, the connecting plate is fixedly connected to the concave plate, the connecting plate is slidably connected to the connecting seat, the output end of the electric push rod is slidably connected to the connecting plate, the motor is arranged at one end of the concave plate, the bidirectional screw is rotatably connected to the concave plate, the bidirectional screw is fixedly connected to the output end of the motor, the bearing plate is correspondingly arranged on one side of the bidirectional screw, and the bearing plate is slidably connected to the concave plate.

[0007] In a specific implementation manner, a fixing ring is correspondingly provided on one side of the drone body, and the electric push rod is fixedly connected to the fixing ring.

[0008] In the above implementation process, a fixing ring is correspondingly provided on one side of the drone body, and the fixing ring can play a connecting role.

[0009] In a specific implementation, an insertion rod is provided at the output end of the electric push rod, and the insertion rod penetrates and is connected to one side of the connecting seat.

[0010] In the above implementation process, an insertion rod is provided at the output end of the electric push rod, and the insertion rod can play a connecting role.

[0011] In a specific embodiment, a sliding rod is correspondingly arranged on one side of the concave plate.

[0012] In the above implementation process, a sliding rod is correspondingly provided on one side of the concave plate, and the sliding rod can play a role of limiting.

[0013] In a specific embodiment, holes and grooves are provided on both sides of the connecting plate, and the insertion rod is slidably connected to the holes and grooves.

[0014] In the above implementation process, holes and grooves are provided on both sides of the connection plate, and the holes and grooves can play a connecting role.

[0015] In a specific implementation, a movable plate is provided at one end of the supporting plate, a thread groove is provided on one side of the movable plate, the bidirectional screw is threadedly connected to the thread groove, a through hole is correspondingly provided on one side of the movable plate, and the sliding rod is slidably connected to the through hole.

[0016] In the above implementation process, the thread groove and the through hole can play a connecting role, so that the carrying plate can move.

[0017] In a specific embodiment, a protective pad is provided on one side of the carrying plate.

[0018] In the above implementation process, a protective pad is provided on one side of the load-bearing plate, and the protective pad can protect the goods.

[0019] In a second aspect, the utility model further provides a drone, comprising the above-mentioned mounting mechanism.

[0020] Compared with the prior art, the beneficial effects of the present application are: first, the connecting plate can be disassembled and installed by passing the output end of the electric push rod through the connecting plate and separating from the connecting plate. The connecting plate can be disassembled and installed without using special tools, and it is more convenient to use; secondly, the bidirectional screw is rotated by the motor, and the rotation of the bidirectional screw can make the two supporting plates move relative to each other, so that goods of different sizes can be fixed, and at the same time, it is convenient to adjust the distance between the two supporting plates, thereby making it more convenient to adjust the distance between the two supporting plates, reducing labor and facilitating the disassembly and installation of the connecting plate, thereby improving practicality. BRIEF DESCRIPTION OF THE DRAWINGS

[0021] In order to more clearly illustrate the technical solutions of the implementation methods of the present application, the drawings required for use in the implementation methods will be briefly introduced below. It should be understood that the following drawings only show certain embodiments of the present application and therefore should not be regarded as limiting the scope. For ordinary technicians in this field, other related drawings can be obtained based on these drawings without paying creative work.

[0022] Figure 1 This is a schematic diagram of a mounting mechanism and a UAV structure provided in an embodiment of the present application;

[0023] Figure 2 A schematic diagram of the structure of the drone provided in the embodiment of the present application;

[0024] Figure 3 A schematic diagram of the concave plate structure provided in an embodiment of the present application;

[0025] Figure 4 A schematic diagram of the structure of a carrier plate provided in an embodiment of the present application.

[0026] In the figure: 100-connecting assembly; 110-UAV body; 111-fixing ring; 120-electric push rod; 121-insertion rod; 130-connecting seat; 200-mounting assembly; 210-concave plate; 211-sliding rod; 220-connecting plate; 221-hole groove; 230-motor; 240-bidirectional screw; 250-carrying plate; 251-moving plate; 252-thread groove; 253-through hole; 254-protective pad. DETAILED DESCRIPTION

[0027] The technical solutions in the embodiments of the present application will be described below in conjunction with the drawings in the embodiments of the present application.

[0028] In order to make the purpose, technical solutions and advantages of the implementation methods of this application clearer, the technical solutions in the implementation methods of this application will be clearly and completely described below in conjunction with the drawings in the implementation methods of this application. Obviously, the described implementation methods are part of the implementation methods of this application, not all of the implementation methods. Based on the implementation methods in this application, all other implementation methods obtained by ordinary technicians in this field without creative work are within the scope of protection of this application.

[0029] See also Figure 1-4 The present application provides a mounting mechanism including a connecting component 100 and a mounting component 200. The connecting component 100 can play a fixing role, and the mounting component 200 can fix goods of different sizes.

[0030] See also Figure 1-2 The connection assembly 100 includes a drone body 110, an electric push rod 120 and a connecting seat 130. The electric push rod 120 is correspondingly arranged on one side of the drone body 110, and the connecting seat 130 is arranged on one side of the drone body 110. The output end of the electric push rod 120 is connected to one side of the connecting seat 130. A fixing ring 111 is correspondingly arranged on one side of the drone body 110. The electric push rod 120 is fixedly connected to the fixing ring 111. The setting of the fixing ring 111 can play a connecting role. The output end of the electric push rod 120 is provided with a plug rod 121. The plug rod 121 is connected to one side of the connecting seat 130. The setting of the plug rod 121 can play a connecting role.

[0031] See also Figure 1 , Figure 3 and Figure 4 The mounting assembly 200 includes a concave plate 210, a connecting plate 220, a motor 230, a bidirectional screw 240 and a bearing plate 250. The connecting plate 220 is fixedly connected to the concave plate 210, the connecting plate 220 is slidably connected to the connecting seat 130, the output end of the electric push rod 120 is slidably connected to the connecting plate 220, the motor 230 is arranged at one end of the concave plate 210, the bidirectional screw 240 is rotatably connected to the concave plate 210, the bidirectional screw 240 is fixedly connected to the output end of the motor 230, the bearing plate 250 is correspondingly arranged on one side of the bidirectional screw 240, the bearing plate 250 is slidably connected to the concave plate 210, and a sliding rod 211 is correspondingly arranged on one side of the concave plate 210. The setting of the sliding rod 211 can play a role in limiting.

[0032] In some specific embodiments, holes and grooves 221 are provided on both sides of the connecting plate 220, and the insertion rod 121 is slidably connected to the holes and grooves 221. The holes and grooves 221 can serve as a connection. A movable plate 251 is provided at one end of the supporting plate 250, and a thread groove 252 is provided on one side of the movable plate 251. The bidirectional screw 240 is threadedly connected to the thread groove 252. A through hole 253 is correspondingly provided on one side of the movable plate 251, and the sliding rod 211 is slidably connected to the through hole 253. The thread groove 252 and the through hole 253 can serve as a connection, so that the supporting plate 250 can be moved. A protective pad 254 is provided on one side of the supporting plate 250. The protective pad 254 can protect the goods.

[0033] The utility model further provides a drone, comprising the above-mentioned mounting mechanism.

[0034] The working principle of the mounting mechanism and the UAV is as follows: the user can start the electric push rod 120, and the output end of the electric push rod 120 drives the insertion rod 121 to be inserted into the hole groove 221 to fix the connecting plate 220, and the insertion rod 121 is separated from the hole groove 221 to disassemble the connecting plate 220, that is, the connecting plate 220 can be disassembled and installed, and the connecting plate 220 can be disassembled and installed without using special tools, which is convenient to use. Secondly, the bidirectional screw rod 240 is rotated by the motor 230, and the rotation of the bidirectional screw rod 240 can make the two movable plates 251 move, so that the two supporting plates 250 can move relative to each other, and goods of different sizes can be fixed. At the same time, it is convenient to adjust the distance between the two supporting plates 250, and then it is more convenient to adjust the distance between the two supporting plates 250, which reduces labor and facilitates the disassembly and installation of the connecting plate 220, thereby improving practicality.

[0035] It should be noted that the specific models and specifications of the drone body 110, the electric push rod 120 and the motor 230 need to be selected and determined according to the actual specifications of the device, and the specific selection calculation method adopts the existing technology in this field, so it will not be described in detail.

[0036] The power supply and principle of the drone body 110, the electric push rod 120 and the motor 230 are clear to those skilled in the art and will not be described in detail here.

[0037] The above description is only an embodiment of the present application and is not intended to limit the scope of protection of the present application. For those skilled in the art, the present application may have various changes and variations. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present application should be included in the scope of protection of the present application. It should be noted that similar reference numerals and letters represent similar items in the following drawings, so once an item is defined in one drawing, it does not need to be further defined and explained in the subsequent drawings.

[0038] The above is only a specific implementation of the present application, but the protection scope of the present application is not limited thereto. Any technician familiar with the technical field can easily think of changes or substitutions within the technical scope disclosed in the present application, which should be included in the protection scope of the present application. Therefore, the protection scope of the present application should be based on the protection scope of the claims.

Claims

1. A mounting mechanism, characterized in that: include A connection assembly (100), the connection assembly (100) comprising an unmanned aerial vehicle body (110), an electric push rod (120) and a connection seat (130), the electric push rod (120) being arranged correspondingly on one side of the unmanned aerial vehicle body (110), the connection seat (130) being arranged on one side of the unmanned aerial vehicle body (110), and an output end of the electric push rod (120) being connected through one side of the connection seat (130); A mounting assembly (200), the mounting assembly (200) comprising a concave plate (210), a connecting plate (220), a motor (230), a bidirectional screw (240) and a bearing plate (250), the connecting plate (220) being fixedly connected to the concave plate (210), the connecting plate (220) being slidably connected to the connecting seat (130), the output end of the electric push rod (120) being slidably connected to the connecting plate (220), the motor (230) being arranged at one end of the concave plate (210), the bidirectional screw (240) being rotatably connected to the concave plate (210), the bidirectional screw (240) being fixedly connected to the output end of the motor (230), the bearing plate (250) being correspondingly arranged at one side of the bidirectional screw (240), and the bearing plate (250) being slidably connected to the concave plate (210).

2. A mounting mechanism according to claim 1, characterized in that: A fixing ring (111) is correspondingly arranged on one side of the drone body (110), and the electric push rod (120) is fixedly connected to the fixing ring (111).

3. A mounting mechanism according to claim 1, characterized in that: The output end of the electric push rod (120) is provided with an insertion rod (121), and the insertion rod (121) penetrates and is connected to one side of the connection seat (130).

4. A mounting mechanism according to claim 1, characterized in that: A sliding rod (211) is correspondingly arranged on one side of the concave plate (210).

5. A mounting mechanism according to claim 3, characterized in that: Holes (221) are provided on both sides of the connection plate (220), and the insertion rod (121) is slidably connected to the holes (221).

6. A mounting mechanism according to claim 4, characterized in that: A movable plate (251) is provided at one end of the bearing plate (250), a thread groove (252) is provided at one side of the movable plate (251), the bidirectional screw rod (240) is threadedly connected to the thread groove (252), a through hole (253) is correspondingly provided at one side of the movable plate (251), and the sliding rod (211) is slidably connected to the through hole (253).

7. A mounting mechanism according to claim 1, characterized in that: A protection pad (254) is provided on one side of the carrying plate (250).

8. A drone, characterized in that include A mounting mechanism as described in any one of claims 1 to 7.

Citation Information

Patent Citations

  • Hanging mechanism of unmanned aerial vehicle

    CN220786165U