Rapidly-assembled electromagnetic sensing equipment mounting mechanism adaptive to unmanned aerial vehicle

By designing a rapid assembly electromagnetic sensing device installation mechanism adapted to drones, and utilizing clamping components and auxiliary installation components, the automated installation of electromagnetic sensing devices has been achieved, solving the problems of complex existing installation structures and manual transportation, and improving installation efficiency and stability.

CN223736272UActive Publication Date: 2025-12-30QINGDAO COLLABORATIVE INNOVATION RES INST
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Patent Information

Application Number
CN202520333376.8
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-02-27
Publication Date
2025-12-30
Estimated Expiration
2035-02-27

AI Technical Summary

Technical Problem

The existing installation structure of drones and electromagnetic sensing equipment is complex, the installation steps are cumbersome and require manual transportation, resulting in low installation efficiency.

Method used

A rapid assembly electromagnetic sensing device mounting mechanism adapted for UAVs was designed, including a clamping component and an auxiliary mounting component. The mechanism utilizes elastic springs and electromagnets to achieve automatic fixing and disassembly of the mounting base, and combines an electric push rod to assist in the movement of the device, thus simplifying the installation process.

Benefits of technology

It enables automated installation of electromagnetic sensing equipment for drones, reducing manual labor intensity, improving installation efficiency and stability, simplifying the disassembly process, and meeting the needs of rapid assembly.

✦ Generated by Eureka AI based on patent content.

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Abstract

The utility model provides a quick assembly electromagnetic sensing equipment mounting mechanism adaptive to an unmanned aerial vehicle, which comprises an unmanned aerial vehicle main body, and a mounting frame is mounted on the bottom side of the unmanned aerial vehicle main body; the device comprises a mounting frame, a clamping assembly which is mounted in the mounting frame, and an auxiliary mounting assembly which is mounted on the bottom side of an unmanned aerial vehicle main body and is used for supporting during mounting of an electromagnetic sensing equipment main body; and the mounting base is mounted in the mounting frame through a clamping assembly, and an electromagnetic sensing equipment body is mounted on the bottom side of the mounting base. Under the action of the arranged clamping assembly, the clamping assembly locks the mounting base placed in the mounting frame, automatic fixing of the mounting base is achieved, the mounting efficiency of the electromagnetic sensing equipment body is improved, mounting stability of the electromagnetic sensing equipment body is guaranteed, in the dismounting process, the mounting base and the mounting frame are conveniently separated through the clamping assembly, dismounting is easy, and the practicability is high. The operation is convenient.
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Description

TECHNICAL FIELD

[0001] The utility model relates to unmanned plane technical field, it is a kind of quick assembly electromagnetic sensing device mounting mechanism suitable for unmanned plane. BACKGROUND

[0002] Unmanned plane, as its name implies, is a kind of unmanned aircraft. It is usually composed of fuselage, power system, flight control system, navigation system and various sensors and actuators, and unmanned plane is a kind of unmanned aircraft controlled by radio remote control equipment or on-board computer program control system.

[0003] Electromagnetic sensing device plays an important role in military, civil, industrial, environmental monitoring, scientific research and transportation and logistics and other fields. The application of these devices not only improves the work efficiency and quality of various fields, but also brings more convenience and safety guarantee for people's life.

[0004] In the installation between existing unmanned plane and electromagnetic sensing device, the existing installation structure is more complex, and the installation steps are cumbersome, and manpower is needed to transport electromagnetic sensing device and unmanned plane assembly in installation, which greatly reduces installation efficiency. INVENTION CONTENTS

[0005] The utility model discloses in order to solve the technical problem that existing installation structure is more complex, installation step is cumbersome, and manpower is needed to transport electromagnetic sensing device and unmanned plane assembly in installation, greatly reduces installation efficiency, and provides a kind of quick assembly electromagnetic sensing device mounting mechanism suitable for unmanned plane.

[0006] The utility model solves the above-mentioned technical problem by the following technical scheme:

[0007] The utility model provides a kind of quick assembly electromagnetic sensing device mounting mechanism suitable for unmanned plane, the quick assembly electromagnetic sensing device mounting mechanism suitable for unmanned plane includes:

[0008] Unmanned plane main body, the installation frame is installed in the bottom side of the unmanned plane main body;

[0009] Clamping assembly, the clamping assembly is installed in installation frame, and the clamping assembly is used for the clamping installation of electromagnetic sensing device main body;

[0010] Auxiliary installation component, the auxiliary installation component is installed in the bottom side of unmanned plane main body, and the auxiliary installation component is used for supporting in electromagnetic sensing device main body installation;

[0011] Mounting seat, the mounting seat is installed in installation frame by clamping assembly, and the mounting seat bottom side is installed with electromagnetic sensing device main body.

[0012] Further, the bottom side of the mounting frame is fixedly connected with two support frames, and the two support frames are located on the opposite sides of the bottom of the mounting frame.

[0013] Further, the clamping assembly comprises a limiting groove and a magnet holder, the limiting groove is clamped in the mounting frame, the bottom end of the limiting groove is provided with a limiting seat, a moving seat is slidably connected in the limiting groove, an elastic spring is installed on the top side of the moving seat, the bottom side of the moving seat is fixedly connected with the magnet holder, and an electromagnet is installed on the top side of the mounting seat.

[0014] In the technical solution, when the mounting seat moves into the mounting frame, the elastic spring pushes the moving seat downward under the elastic effect of the elastic spring, and when the mounting seat moves, the clamping groove opened on the top side of the mounting seat is clamped with the bottom end of the magnet holder installed on the bottom end of the moving seat, so that the magnet holder is stably placed, the installation of the mounting seat is stable, in disassembly, the electromagnet is electrified, the electromagnet generates magnetism, the electromagnet repels the magnetism of the magnet holder, the magnet holder is separated from the clamping groove, and then the mounting seat is moved out, and the subsequent electromagnetic sensing device is moved out.

[0015] Further, the top side of the mounting seat is provided with a clamping groove, the magnet holder is clamped and connected with the clamping groove, and the electromagnet repels the magnetism of the magnet holder after being electrified.

[0016] Further, the number of elastic springs is several, and the several elastic springs are evenly installed between the moving seat and the limiting groove.

[0017] Further, the cross section of the mounting seat is T-shaped structure, the top end of the mounting seat is slidably connected in the inner cavity of the mounting frame, the bottom end of the mounting seat is fixedly connected with a limiting plate, and the top side of the limiting plate is slidably connected with the bottom side of the mounting frame.

[0018] Further, the auxiliary mounting assembly comprises an electric push rod and a connecting seat, the electric push rod is fixedly installed on the bottom side surface of the unmanned aerial vehicle, the output end of the electric push rod is fixedly connected with the connecting seat, the bottom side of the connecting seat is fixedly connected with a sliding frame, the inner wall of the sliding frame is fixedly connected with a roller shaft, and the surface of the roller shaft is sleeved with a roller.

[0019] In the technical solution, in the installation of the electromagnetic sensing device body, the electromagnetic sensing device body is placed on the top side of the roller, the electric push rod adjusts the moving position of the sliding frame through the connecting seat, and then the position of the electromagnetic sensing device body is adjusted, the electromagnetic sensing device body is pushed along the surface of the roller, the electromagnetic sensing device body is pushed conveniently, the installation operation of the electromagnetic sensing device body is facilitated, the installation strength of the electromagnetic sensing device body is reduced, and the installation efficiency is improved.

[0020] Further, the sliding frame is a square frame structure in plan view, and the connecting seat is fixedly connected to the top of the opposite sides of the sliding frame.

[0021] Further, the number of the rollers is several, and the several adjacent rollers are equidistantly distributed.

[0022] Further, the number of the rollers is several, and the several adjacent rollers are equidistantly distributed.

[0023] On the basis of common knowledge in the art, the above-mentioned preferred conditions can be combined arbitrarily, thereby obtaining each preferred example of the present application.

[0024] The positive progress effect of the present application lies in:

[0025] The above-mentioned quick assembly electromagnetic sensing device mounting mechanism suitable for unmanned aerial vehicles can automatically drag the electromagnetic sensing device body to move through the auxiliary mounting assembly, avoids manual carrying, reduces manual labor intensity, facilitates subsequent connection of the electromagnetic sensing device body and the mounting frame, and realizes automatic fixing of the mounting seat through locking of the mounting seat in the mounting frame by the clamping assembly, thereby improving the installation efficiency of the electromagnetic sensing device body, ensuring installation stability of the electromagnetic sensing device body, facilitating separation of the mounting seat and the mounting frame by the clamping assembly during disassembly, and achieving simple disassembly and convenient operation, which meets the installation requirements of workers and improves the installation efficiency. BRIEF DESCRIPTION OF DRAWINGS

[0026] In order to more clearly illustrate the technical solutions in the embodiments of the present application or the prior art, the drawings needed to be used in the embodiment or prior art description will be briefly introduced. Obviously, the drawings in the following description are only some embodiments of the present application.

[0027] Fig. 1 It is a perspective structural schematic view of the mounting mechanism of the present application.

[0028] Fig. 2 It is a bottom view of the mounting mechanism of the present application.

[0029] Fig. 3 It is a front view of the mounting mechanism of the present application.

[0030] EXPLANATION OF REFERENCE NUMERALS

[0031] 1, unmanned aerial vehicle body;

[0032] 2, support frame;

[0033] 3, mounting frame;

[0034] 4, clamping assembly; 41, limiting groove; 42, elastic spring; 43, moving seat; 44, magnet holder; 45, electromagnet; 46, limiting seat;

[0035] 5, mounting seat;

[0036] 6, limiting plate;

[0037] 7, electromagnetic sensing device body;

[0038] 8, auxiliary mounting assembly; 81, electric push rod; 82, connecting seat; 83, sliding frame; 84, roller shaft; 85, roller. DETAILED DESCRIPTION

[0039] In order to make the person skilled in the art better understand the scheme of the present application, the technical scheme in the embodiments of the present application will be described clearly and completely below in combination with the drawings in the embodiments of the present application. Obviously, the described embodiments are only a part of the embodiments of the present application, rather than all the embodiments. Based on the embodiments in the present application, all other embodiments obtained by the person skilled in the art without creative labor should belong to the protection scope of the present application.

[0040] It should be noted that the terms "first", "second", and the like in the specification of the present application, the claims, and the above-described drawings are used to distinguish similar objects, and do not have to be used to describe a specific order or sequence. It should be understood that the data thus used can be interchanged under appropriate circumstances, so that the embodiments of the present application described herein can be implemented. In addition, the terms "include" and "have" and any variations thereof are intended to cover non-exclusive inclusion, for example, a process, method, system, product or device that includes a series of steps or units does not have to be limited to those steps or units clearly listed, but can include other steps or units that are not clearly listed or inherent to these processes, methods, products or devices.

[0041] In the present application, the terms "up", "down", "left", "right", "front", "back", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal", and the like indicate the orientation or positional relationship based on the orientation or positional relationship shown in the drawings. These terms are mainly used to better describe the present application and its embodiments, and are not used to limit the indicated devices, elements or components to have a specific orientation, or to be constructed and operated in a specific orientation.

[0042] Also, in addition to indicating the orientation or positional relationship, the above-mentioned part of the terms can also be used to indicate other meanings, for example, the term "up" can also be used to indicate a certain dependent relationship or connection relationship in some cases. For the person skilled in the art, the specific meaning of these terms in the present application can be understood according to the specific circumstances.

[0043] In addition, the terms "mounting", "setting", "provided with", "connected", "connected", "socketed" should be broadly understood. For example, it can be fixed connection, detachable connection, or integral structure; it can be mechanical connection, or electrical connection; it can be directly connected, or indirectly connected through an intermediate medium, or internal communication between two devices, elements or components. For those skilled in the art, the specific meaning of the above terms in this application can be understood according to the specific circumstances.

[0044] It should be noted that the embodiments in the present application and the features in the embodiments can be combined with each other without conflict.

[0045] As shown in Figs. 1-3 The quick assembly electromagnetic sensing device mounting mechanism for adapting unmanned aerial vehicle includes:

[0046] An unmanned aerial vehicle body 1 is provided with a mounting frame 3 on the bottom side;

[0047] A clamping assembly 4 is installed in the mounting frame 3, and the clamping assembly 4 is used for clamping installation of the electromagnetic sensing device body 7;

[0048] An auxiliary mounting assembly 8 is installed on the bottom side of the unmanned aerial vehicle body 1, and the auxiliary mounting assembly 8 is used for supporting in the installation of the electromagnetic sensing device body 7;

[0049] A mounting seat 5 is installed in the mounting frame 3 through the clamping assembly 4, and the mounting seat 5 is provided with the electromagnetic sensing device body 7 on the bottom side.

[0050] In the installation of the electromagnetic sensing device body 7, the electromagnetic sensing device body 7 is placed on the auxiliary mounting assembly 8, and the electromagnetic sensing device body 7 is automatically dragged to move by the auxiliary mounting assembly 8, avoiding manual carrying, reducing labor intensity, facilitating subsequent connection of the electromagnetic sensing device body 7 and the mounting frame 3, and locking the mounting seat 5 in the mounting frame 3 by the action of the clamping assembly 4, realizing automatic fixing of the mounting seat 5, improving the installation efficiency of the electromagnetic sensing device body 7, and guaranteeing the installation stability of the electromagnetic sensing device body 7. In disassembly, the clamping assembly 4 can separate the mounting seat 5 from the mounting frame 3, which is simple and convenient to operate, meets the installation needs of workers, and improves the installation efficiency.

[0051] The bottom side of the mounting frame 3 is fixedly connected with two support frames 2, and the two support frames 2 are located on the opposite sides of the bottom of the mounting frame 3.

[0052] The support frame 2 is provided, which is convenient for subsequent stable placement of the unmanned aerial vehicle.

[0053] The clamping assembly 4 comprises a limiting groove 41 and a magnet holder 44, the limiting groove 41 is clamped in the mounting frame 3, the bottom end of the limiting groove 41 is provided with a limiting seat 46, the movable seat 43 is slidably connected in the limiting groove 41, the movable seat 43 is provided with an elastic spring 42 on the top side, the movable seat 43 is fixedly connected with the magnet holder 44 on the bottom side, and the mounting seat 5 is provided with an electromagnet 45 on the top side.

[0054] When the mounting seat 5 moves into the mounting frame 3, the elastic spring 42 pushes the movable seat 43 to move downward under the elastic effect, and the clamping groove provided on the top side of the mounting seat 5 is clamped with the bottom end of the magnet holder 44 installed on the bottom end of the movable seat 43, so that the magnet holder 44 is stably placed, the installation of the mounting seat 5 is stable, and in disassembly, the electromagnet 45 generates magnetism by being electrified, the electromagnet 45 repels the magnet holder 44, the magnet holder 44 is separated from the clamping groove, and then the mounting seat 5 is conveniently removed, and the subsequent electromagnetic sensing device is conveniently removed.

[0055] The mounting seat 5 is provided with a clamping groove on the top side, the magnet holder 44 is clamped and connected with the clamping groove, and the electromagnet 45 repels the magnet holder after being electrified.

[0056] The number of the elastic springs 42 is several, and the several elastic springs 42 are evenly installed between the movable seat 43 and the limiting groove 41.

[0057] The mounting seat 5 is in T-shaped structure, the mounting seat 5 is slidably connected in the inner cavity of the mounting frame 3, the bottom end surface of the mounting seat 5 is fixedly connected with a limiting plate 6, and the top side of the limiting plate 6 is slidably connected with the bottom side of the mounting frame 3.

[0058] The auxiliary mounting assembly 8 comprises an electric push rod 81 and a connecting seat 82, the electric push rod 81 is fixedly installed on the bottom side surface of the unmanned aerial vehicle, the output end of the electric push rod 81 is fixedly connected with the connecting seat 82, the bottom side of the connecting seat 82 is fixedly connected with a sliding frame 83, the inner wall of the sliding frame 83 is fixedly connected with a roller shaft 84, and the surface of the roller shaft 84 is sleeved with a roller 85.

[0059] In the installation of the electromagnetic sensing device body 7, the electromagnetic sensing device body 7 is placed on the top side of the roller 85, the electric push rod 81 adjusts the moving position of the sliding frame 83 through the connecting seat 82, and then the position of the electromagnetic sensing device body 7 is adjusted, the electromagnetic sensing device body 7 is pushed along the surface of the roller 85, the pushing is convenient, the installation operation of the electromagnetic sensing device body 7 is facilitated, the installation strength of the electromagnetic sensing device body 7 is reduced, and the installation efficiency is improved.

[0060] The sliding frame 83 is in square frame structure in plan view, and the connecting seat 82 is fixedly connected to the top of the opposite two sides of the sliding frame 83.

[0061] The number of the rollers 84 is several, and several adjacent rollers 84 are equidistantly distributed.

[0062] The number of the rollers 84 is several, and several adjacent rollers 84 are equidistantly distributed.

[0063] The circuit and electronic components and modules are all prior art, and those skilled in the art can realize them without further description, and the content protected by the application does not involve improvement of software and methods.

[0064] The utility model is not limited to the above-mentioned embodiment, no matter makes any change in its shape or structure, all falls in the protection scope of the utility model. The protection scope of the utility model is defined by the appended claims, those skilled in the art can make various changes or modifications to these embodiments without departing from the principles and essence of the utility model, but these changes and modifications all fall into the protection scope of the utility model.

Claims

1. A quick assembly electromagnetic sensing device mounting mechanism for drones, characterized in that, The quick assembly electromagnetic sensing device mounting mechanism of the adaptive unmanned aerial vehicle comprises: An unmanned aerial vehicle body (1) is provided with a mounting frame (3) on the bottom side; A clamping assembly (4) is installed in the mounting frame (3), and is used for clamping and mounting an electromagnetic sensing device body (7); An auxiliary mounting assembly (8) is installed on the bottom side of the unmanned aerial vehicle body (1), and is used for supporting the electromagnetic sensing device body (7) during installation; A mounting seat (5) is installed in the mounting frame (3) through the clamping assembly (4), and the bottom side of the mounting seat (5) is provided with the electromagnetic sensing device body (7).

2. The quick assembly electromagnetic sensing device mounting mechanism for adapting drones of claim 1, wherein: Two support frames (2) are fixedly connected to the bottom side of the mounting frame (3), and are located on the opposite sides of the bottom of the mounting frame (3).

3. The quick assembly electromagnetic sensing device mounting mechanism for adapting drones of claim 1, wherein: The clamping assembly (4) comprises a limiting groove (41) and a magnet holder (44), the limiting groove (41) is clamped in the mounting frame (3), the bottom end of the limiting groove (41) is provided with a limiting seat (46), a moving seat (43) is slidably connected in the limiting groove (41), the top side of the moving seat (43) is provided with an elastic spring (42), the bottom side of the moving seat (43) is fixedly connected with the magnet holder (44), and the top side of the mounting seat (5) is provided with an electromagnet (45).

4. The quick assembly electromagnetic sensing device mounting mechanism for adapting drones of claim 2, wherein: The top side of the mounting seat (5) is provided with a clamping groove, the magnet holder (44) is clamped and connected with the clamping groove, and the electromagnet (45) repels the magnet seat after being electrified.

5. The quick assembly electromagnetic sensing device mounting mechanism for adapting drones of claim 3, wherein: The number of the elastic springs (42) is several, and the several elastic springs (42) are evenly installed between the moving seat (43) and the limiting groove (41).

6. The quick assembly electromagnetic sensing device mounting mechanism for adapting drones of claim 2, wherein: The cross section of the mounting seat (5) is T-shaped structure, the top end of the mounting seat (5) is slidably connected in the inner cavity of the mounting frame (3), the bottom end of the mounting seat (5) is fixedly connected with a limiting plate (6), and the top side of the limiting plate (6) is slidably connected with the bottom side of the mounting frame (3).

7. The quick assembly electromagnetic sensing device mounting mechanism for adapting drones of claim 1, wherein: The auxiliary mounting assembly (8) comprises an electric push rod (81) and a connecting seat (82), the electric push rod (81) is fixedly installed on the bottom surface of the unmanned aerial vehicle, the output end of the electric push rod (81) is fixedly connected with the connecting seat (82), the bottom side of the connecting seat (82) is fixedly connected with a sliding frame (83), the inner wall of the sliding frame (83) is fixedly connected with a roller shaft (84), and the surface of the roller shaft (84) is sleeved with a roller (85).

8. The quick assembly electromagnetic sensing device mounting mechanism adapted for drones of claim 7, wherein: The cross section of the sliding frame (83) is a square box structure, and the connecting seat (82) is fixedly connected to the top of the opposite sides of the sliding frame (83).

9. The quick assembly electromagnetic sensing device mounting mechanism for adapting drones of claim 7, wherein: The number of the roller shafts (84) is several, and the adjacent roller shafts (84) are equidistantly distributed.

10. The quick assembly electromagnetic sensing device mounting mechanism for adapting drones of claim 7, wherein: The number of the rollers (85) is equal to that of the roller shafts (84), the rollers (85) are rotatably sleeved on the surfaces of the roller shafts (84), and the rollers (85) are located below the electromagnetic sensing device body (7).