Magnetic material assembling clamp for unmanned aerial vehicle

By designing a magnetic assembly fixture for drones, and utilizing a combination structure of a base and a magnet carrier, the problems of poor positioning accuracy and unreliable bonding of magnetic blocks in drones were solved, achieving high-precision magnetic block assembly and reliable bonding.

CN224027500UActive Publication Date: 2026-03-24XINYANG YEN SONIC TECH CO LTD
View PDF 0 Cites 0 Cited by

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Filing Date
2025-03-24
Publication Date
2026-03-24

AI Technical Summary

Technical Problem

Problems with poor positioning accuracy and unreliable bonding of magnetic blocks during the assembly of magnetic materials for drones.

Method used

A magnetic material assembly fixture for UAVs was designed, including a base and a magnet carrier. The base is provided with a positioning post and a push-fit assembly, and the magnet carrier is provided with a positioning hole and an L-shaped stop. The push-fit assembly is moved and locked by a quick clamp, so as to achieve precise positioning and clamping of the magnetic block.

Benefits of technology

This technology enables rapid pressing and bonding of magnetic blocks, improving positioning accuracy and bonding reliability during assembly.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN224027500U_ABST
    Figure CN224027500U_ABST
Patent Text Reader

Abstract

The magnetic material assembling clamp for the unmanned aerial vehicle comprises a base and a magnet carrier, the magnet carrier is rectangular, L-shaped blocking edges are arranged on the two connected side edges of the magnet carrier, and magnetic block containing grooves are formed in the inner sides of the L-shaped blocking edges. The base is further provided with a pushing assembly and a first rapid pressing clamp. The base is further provided with a second rapid pressing clamp corresponding to the short edge of the L-shaped flange, and a pressing rod of the second rapid pressing clamp is used for abutting against the end of the combined magnet. According to the magnetic material assembling clamp for the unmanned aerial vehicle, the magnet carrier and the pushing assembly are installed on the base, the L-shaped blocking edge is arranged on the magnet carrier, the pushing assembly is driven by the first rapid pressing clamp to move and be locked, the end of the combined magnet is pressed and locked through the second rapid pressing clamp, pressing and bonding of the combined magnet can be rapidly completed, and the assembling efficiency is improved. In the assembling process, the magnetic blocks are high in positioning precision and reliable in bonding.
Need to check novelty before this filing date? Find Prior Art

Description

TECHNICAL FIELD

[0001] The utility model relates to magnet assembling technology especially a magnetic material assembling clamp for unmanned plane. BACKGROUND

[0002] Magnet is a kind of widely used basic electronic component and electrical component, mainly applied to computer, mobile phone, TV, communication, toy, sound, automation equipment, nuclear magnetic resonance imaging etc. At present, neodymium-iron-boron magnet is widely used as high-performance permanent magnet;In electronic product, diaphragm (vibrating diaphragm of microphone, earphone, loudspeaker etc.), electroacoustic equipment production and processing, some equipment needs magnet not rectangular or round and other conventional shapes, according to product processing requirements, magnet needs to be combined into the shape and size suitable for the equipment.

[0003] A combined magnet used in unmanned plane is composed of three irregular flat magnetic blocks, and magnetic block pressing and bonding processes are needed in assembling process, and the existing magnet assembling jig has the problems of poor positioning accuracy of magnetic block and unreliable bonding in pushing and bonding process. UTILITY MODEL CONTENTS

[0004] The utility model aims at providing a kind of magnetic material assembling clamp for unmanned plane, to solve the problem of poor positioning accuracy of magnetic block and unreliable bonding in the existing magnetic material assembling process for unmanned plane.

[0005] To solve the above problems, the utility model provides a kind of magnetic material assembling clamp for unmanned plane, including base and magnet carrier, the base is equipped with positioning column, the magnet carrier is equipped with the positioning hole corresponding with the positioning column, the magnet carrier is installed on the base by the positioning column, the magnet carrier is rectangular, L-shaped baffle is equipped on two connected sides of the magnet carrier, magnetic block placing groove is formed in the inner side of L-shaped baffle, magnetic block positioning line of demarcation is further equipped on the upper surface of the short side of L-shaped baffle;The base is further equipped with the push assembly corresponding with the long side of L-shaped baffle and first quick pressing clamp, the push rod of push assembly is used to push and compress the magnetic block in the magnetic block placing groove to the long side of L-shaped baffle, and the first quick pressing clamp is used to drive the push assembly to move and lock the push assembly in preset position;The base is further equipped with the second quick pressing clamp corresponding with the short side of L-shaped baffle, and the pressing rod of second quick pressing clamp is used to top pressure end of combined magnet.

[0006] The utility model provides a kind of magnetic material assembling clamp for unmanned plane further has the following technical features:

[0007] Further, the inner edge shape of the long side of L-shaped baffle is adapted to the outer contour of the magnetic block to be pushed and bonded.

[0008] Further, the upper part of the push assembly is provided with two parallel push rods, and the end part of each push rod is matched with the outer contour of the magnetic block to be pushed and bonded.

[0009] Further, the base is further provided with a sliding rail, and the bottom of the push assembly is provided with a sliding block matched with the sliding rail.

[0010] Further, the base is further provided with two parallel sliding rails.

[0011] Further, the push assembly comprises a push rod, a push rod mounting block and a push rod cover plate, the push rod mounting block is provided with two parallel insertion holes, the push rod is inserted into the insertion hole, the end of the push rod close to the push rod cover plate is provided with a positioning stopper, and the push rod mounting block is provided with a clamping groove matched with the positioning stopper; and the push rod cover plate is mounted on the push rod mounting block and used for blocking the insertion hole and clamping the positioning stopper.

[0012] Further, the push rod cover plate is further provided with a spring mounting groove matched with the end of the push rod, and a compression spring abutting against the end of the push rod is mounted in the spring mounting groove.

[0013] Further, the magnetic block placing groove is further provided with a ventilation hole penetrating through the magnet carrier and close to the long side of the L-shaped stopper.

[0014] The unmanned aerial vehicle magnetic material assembling clamp has the following beneficial effects: the unmanned aerial vehicle magnetic material assembling clamp can quickly complete the pressing and bonding of the combined magnet, and the positioning precision of the magnetic block is high and the bonding is reliable during the assembling process. BRIEF DESCRIPTION OF DRAWINGS

[0015] Figure 1 FIG. 1 is a structural schematic view of the unmanned aerial vehicle magnetic material assembling clamp in the utility model;

[0016] Figure 2 FIG. 2 is another view of the structural schematic view of the unmanned aerial vehicle magnetic material assembling clamp in the utility model; Figure 1

[0017] FIG. 3 is a top view of the unmanned aerial vehicle magnetic material assembling clamp in the utility model; Figure 3 Figure 1 FIG. 4 is a sectional view of the unmanned aerial vehicle magnetic material assembling clamp in the utility model in A-A direction;

[0018] Figure 4 Figure 3 FIG. 5 is a sectional view of the unmanned aerial vehicle magnetic material assembling clamp in the utility model in B-B direction;

[0019] Figure 5 ​​The structure diagram of the magnet carrier in the embodiment of the utility model. DETAILED DESCRIPTION

[0020] The utility model will be explained in detail below with reference to the drawings and in combination with the embodiments. It should be noted that the embodiments in the utility model and the features in the embodiments can be combined with each other without conflict.

[0021] As Figures 1 to 5 The embodiment of the magnetic material assembling clamp for unmanned aerial vehicle of the utility model, the magnetic material assembling clamp for unmanned aerial vehicle includes base 10 and magnet carrier 20, the base 10 is equipped with locating column 11, the magnet carrier 20 is equipped with the locating hole 21 corresponding with locating column 11, the magnet carrier 20 is installed on the base 10 through locating column 11 to be convenient for dismounting, the magnet carrier 20 is rectangular, the two sides of the magnet carrier 10 are equipped with L-shaped baffle 22, the inside of L-shaped baffle 22 is formed with magnetic block placing groove, the upper surface of the short side 221 of L-shaped baffle 22 is also equipped with magnetic block locating line 223;The base 10 is also equipped with the push combination component 30 and the first quick pressure clamp 41 corresponding with the long side 222 of L-shaped baffle 22, the push rod 31 of push combination component 30 is used to push and compress the magnetic block 501, magnetic block 502, magnetic block 503 in the magnetic block placing groove to the long side 222 of L-shaped baffle 22, and the first quick pressure clamp 41 is used to drive push combination component 30 to move and lock push combination component 30 in the preset position;The base 10 is also equipped with the second quick pressure clamp 42 corresponding with the short side 221 of L-shaped baffle 22, and the pressing rod of the second quick pressure clamp 42 is used to press the end of the combined magnet.

[0022] The above unmanned aerial vehicle magnetic material assembly clamp of the present application is used in the following manner: first, the magnetic blocks to be pressed and bonded are sequentially loaded into the predetermined positions in the magnetic block placing grooves of the magnet carrier 20, glue is applied to the bonding surfaces of the magnetic blocks, and then the handle of the first rapid pressing clamp 41 is swung to drive the pushing assembly 30 to move on the base 10 towards the magnet carrier 20, the pushing rod 31 of the pushing assembly 30 pushes the magnetic block 503 towards the long edge 222 of the L-shaped stop edge 22 during the movement of the pushing assembly 30, when the magnetic block 503, the magnetic block 502 and the magnetic block 501 sequentially abut against each other, the handle of the first rapid pressing clamp 41 is swung to the locked position, and the end of the pushing rod 31 of the pushing assembly 30 presses the magnetic block 503, the magnetic block 502 and the magnetic block 501 between the pushing rod 31 and the long edge 222; then the handle of the second rapid pressing clamp 42 is swung to make the pressing rod of the second rapid pressing clamp 42 extend towards the short edge 221 of the L-shaped stop edge 22, when the end of the pressing rod of the second rapid pressing clamp 42 abuts against and presses the end of the magnetic block 503, the magnetic block 502 and the magnetic block 501, the handle of the first rapid pressing clamp 41 is swung to the locked position; after the glue is cured, the handles of the first rapid pressing clamp 41 and the second rapid pressing clamp 42 are swung in the opposite direction to unlock the combined magnet, and the combined magnet after being pressed and bonded is taken out of the magnet carrier 20, thereby completing the pressing and bonding of the magnetic block 503, the magnetic block 502 and the magnetic block 501.

[0023] The above unmanned aerial vehicle magnetic material assembly clamp of the present application is used in the following manner: first, the magnetic blocks to be pressed and bonded are sequentially loaded into the predetermined positions in the magnetic block placing grooves of the magnet carrier 20, glue is applied to the bonding surfaces of the magnetic blocks, and then the handle of the first rapid pressing clamp 41 is swung to drive the pushing assembly 30 to move on the base 10 towards the magnet carrier 20, the pushing rod 31 of the pushing assembly 30 pushes the magnetic block 503 towards the long edge 222 of the L-shaped stop edge 22 during the movement of the pushing assembly 30, when the magnetic block 503, the magnetic block 502 and the magnetic block 501 sequentially abut against each other, the handle of the first rapid pressing clamp 41 is swung to the locked position, and the end of the pushing rod 31 of the pushing assembly 30 presses the magnetic block 503, the magnetic block 502 and the magnetic block 501 between the pushing rod 31 and the long edge 222; then the handle of the second rapid pressing clamp 42 is swung to make the pressing rod of the second rapid pressing clamp 42 extend towards the short edge 221 of the L-shaped stop edge 22, when the end of the pressing rod of the second rapid pressing clamp 42 abuts against and presses the end of the magnetic block 503, the magnetic block 502 and the magnetic block 501, the handle of the first rapid pressing clamp 41 is swung to the locked position; after the glue is cured, the handles of the first rapid pressing clamp 41 and the second rapid pressing clamp 42 are swung in the opposite direction to unlock the combined magnet, and the combined magnet after being pressed and bonded is taken out of the magnet carrier 20, thereby completing the pressing and bonding of the magnetic block 503, the magnetic block 502 and the magnetic block 501.

[0024] In an embodiment of the present application, preferably, the inner edge of the long edge 222 of the L-shaped stop edge 22 is shaped to match the outer contour of the magnetic blocks to be pushed and bonded; the pushing assembly 30 is provided with two parallel pushing rods 31, the ends of the two pushing rods 31 are shaped to match the outer contour of the magnetic blocks to be pushed and bonded; as shown in Figures 1 to 3 the magnetic block 501, the magnetic block 502 and the magnetic block 503 are irregularly shaped, one end of each magnetic block is thicker and the other end is thinner, the inner edge of the long edge 222 of the L-shaped stop edge 22 is shaped to match the outer contour of the magnetic block 501; the ends of the two pushing rods 31 are shaped to match the shape of the magnetic block 503, and the shape of the inner edge of the L-shaped stop edge 22 and the shape of the ends of the pushing rods 31 are optimized by referring to the outer contour of the magnetic blocks to be pushed and bonded, so that each magnetic block is accurately positioned during the pushing and assembling process.

[0025] In one embodiment of the present application, preferably, the base 10 is further provided with a sliding rail 12, and the bottom of the push-fit assembly 30 is provided with a sliding block matched with the sliding rail 12; preferably, the base 10 is further provided with two parallel sliding rails 12, and the bottom of the push-fit assembly 30 is correspondingly provided with two sliding blocks, so that the push-fit assembly 30 can slide on the base reliably.

[0026] In one embodiment of the present application, preferably, the push-fit assembly 30 comprises a push rod 31, a push rod mounting block 32 and a push rod cover plate 33, the push rod mounting block 32 is provided with two parallel insertion holes, the push rod 31 is inserted into the insertion holes, one end of the push rod 31 close to the push rod cover plate 33 is provided with a positioning stopper 311, and the push rod mounting block 32 is provided with a clamping groove corresponding to the positioning stopper 311; the push rod cover plate 33 is mounted on the push rod mounting block 32 to block the insertion holes and press the positioning stopper 311, so that the push rod is convenient to mount, reliable to position and convenient to disassemble and replace.

[0027] In one embodiment of the present application, preferably, the push rod cover plate 33 is further provided with a spring mounting groove 331 corresponding to the end of the push rod 31, and a compression spring 34 is mounted in the spring mounting groove 331 to abut against the end of the push rod 31, so that the push rod 31 can elastically slide in the insertion hole of the push rod mounting block 32 under the action of the compression spring 34, and the compression spring 34 can provide buffering when the end of the push rod 31 abuts against the magnetic block to be pushed and compressed, so as to slow down the collision of the end of the push rod and the magnetic block and ensure that the push rod can reliably compress the magnetic block to be bonded.

[0028] In one embodiment of the present application, preferably, the long edge 222 of the L-shaped stop edge 22 is further provided with a ventilation hole 23 penetrating downward through the magnet carrier 20, and specifically, when the magnetic blocks 501, 502 and 503 to be compressed and bonded are compressed against the long edge 222 of the L-shaped stop edge 22, the ventilation hole 23 is located at the bottom of the combined magnet, so as to facilitate the glue of the bonding seam of the magnetic blocks to contact with air and solidify quickly.

[0029] Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present application, but not to limit them; although the present application has been described in detail with reference to the foregoing embodiments, those skilled in the art should understand that the technical solutions recorded in the foregoing embodiments can still be modified, or some technical features can be replaced equivalently; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the spirit and scope of the technical solutions of the embodiments of the present application.

Claims

1. A magnetic material assembly fixture for unmanned aerial vehicles (UAVs), comprising a base and a magnetic carrier, wherein the base is provided with positioning posts, and the magnetic carrier is provided with positioning holes corresponding to the positioning posts, and the magnetic carrier is mounted on the base via the positioning posts, characterized in that... The magnet carrier is rectangular, with L-shaped baffles on two connected sides. A magnetic block placement groove is formed on the inner side of each L-shaped baffle, and a magnetic block positioning line is provided on the upper surface of the shorter side of the L-shaped baffle. The base also includes a push-fit assembly corresponding to the longer side of the L-shaped baffle and a first quick-pressing clamp. The push rod of the push-fit assembly pushes and presses the magnetic block in the placement groove toward the longer side of the L-shaped baffle. The first quick-pressing clamp drives the push-fit assembly to move and locks it in a preset position. The base also includes a second quick-pressing clamp corresponding to the shorter side of the L-shaped baffle, with a pressing rod pressing against the end of the assembled magnet.

2. The magnetic material assembly fixture for UAVs according to claim 1, characterized in that: The inner edge shape of the long side of the L-shaped stop is adapted to the outer contour of the magnetic block to be pushed and bonded.

3. The magnetic material assembly fixture for UAVs according to claim 1, characterized in that: The push-fit assembly is provided with two parallel push rods, the end shapes of which are adapted to the outer contours of the magnetic blocks to be pushed and bonded.

4. The magnetic material assembly fixture for UAVs according to claim 1, characterized in that: The base is also provided with a slide rail, and the bottom of the push-fit assembly is provided with a slider that is adapted to the slide rail.

5. The magnetic material assembly fixture for UAVs according to claim 4, characterized in that: The base is also provided with two parallel slide rails.

6. The magnetic material assembly fixture for UAVs according to claim 1, characterized in that: The push-fit assembly includes a push rod, a push rod mounting block, and a push rod cover plate. The push rod mounting block has two parallel insertion holes, and the push rod is inserted into the insertion holes. A positioning stop is provided at one end of the push rod near the push rod cover plate. The push rod mounting block has a slot corresponding to the positioning stop. The push rod cover plate is installed on the push rod mounting block to block the insertion holes and clamp the positioning stop.

7. The magnetic material assembly fixture for UAVs according to claim 6, characterized in that: The push rod cover plate is also provided with a spring mounting groove corresponding to the end of the push rod, and a compression spring that abuts against the end of the push rod is installed in the spring mounting groove.

8. The magnetic material assembly fixture for UAVs according to claim 1, characterized in that: The long side of the magnetic block placement groove near the L-shaped stop is also provided with a vent hole that penetrates downward through the magnet carrier.