Integrated unmanned aerial vehicle motor electronic speed controller mounting mechanism

Abstract

The utility model relates to the technical field of motor electronic speed regulator mounting mechanisms, in particular to an integrated unmanned aerial vehicle motor electronic speed regulator mounting mechanism, which solves the problems mentioned in the background technology and comprises an electronic speed regulator, a first mounting plate and a second mounting plate, one end of the first mounting plate is provided with a slot, and the second mounting plate is inserted into the slot. The top of the first mounting plate and the top of the second mounting plate are fixedly connected with a first fixing plate and a second fixing plate respectively, the end face of the second mounting plate is provided with a threaded groove, the first mounting plate is rotationally connected with a connecting assembly which penetrates through the inserting groove and is in threaded connection with the threaded groove, and the connecting assembly is rotationally connected to the threaded groove. And the first fixing plate and the second fixing plate are close to each other or far away from each other, so that electronic speed regulators with different sizes can be adapted between the first fixing plate and the second fixing plate.

Description

Technical Field

[0001] This utility model relates to the technical field of motor ESC installation mechanism, specifically an integrated UAV motor ESC installation mechanism. Background Technology

[0002] Electronic speed controller (ESC) is a device that adjusts the speed of a motor based on a control signal. ESCs are also used in the field of drones and need to be installed on the drone motor.

[0003] Existing ESC mounting mechanisms are not very practical, cannot effectively prevent incorrect ESC installation, and cannot be adapted to various electronic speed controllers. There is room for improvement in these aspects, and solving these problems has become a hot topic. To address this, we have launched an integrated drone motor ESC mounting mechanism. Utility Model Content

[0004] (a) Technical problems to be solved

[0005] To address the shortcomings of existing technologies, this utility model provides an integrated UAV motor ESC mounting mechanism, which solves the problems mentioned in the background section.

[0006] (II) Technical Solution

[0007] To achieve the above objectives, this utility model provides the following technical solution: an integrated UAV motor ESC mounting mechanism, comprising an electronic speed controller, a first mounting plate, and a second mounting plate. One end of the first mounting plate has a slot, and the second mounting plate is inserted into the slot and slidably connected. The tops of the first mounting plate and the second mounting plate are respectively fixedly connected to a first fixing plate and a second fixing plate. The end face of the second mounting plate has a threaded groove. A through slot is rotatably connected to the first mounting plate and a connecting component is threadedly connected to the threaded groove. The connecting component is rotated on the threaded groove to bring the first fixing plate and the second fixing plate closer to or further apart from each other, for adapting electronic speed controllers of different sizes between the first fixing plate and the second fixing plate.

[0008] Furthermore, an additional part is fixedly connected to the outer wall of the second mounting plate away from the end of the first mounting plate, so that the top of the second mounting plate is coplanar with the top of the first mounting plate.

[0009] Furthermore, a first fixing strip is fixedly connected to the top of the first mounting plate, and a second fixing strip is fixedly connected to the top of the supplementary part. The first fixing strip and the second fixing strip have different shapes to distinguish the installation position of the electronic speed controller.

[0010] Furthermore, the connecting assembly includes a threaded rod, a smooth portion is provided on the side wall near one end of the threaded rod, and a rotating block is fixedly connected to the smooth portion. A rotating handle with a cross groove is installed at the upper end of the threaded rod.

[0011] Furthermore, U-shaped limiting plates are inserted into the bottom along both sides of the second mounting plate, and fixing bolts that are threadedly connected to the second mounting plate are provided on both sides of the limiting plates for limiting and fixing the electronic speed controller.

[0012] Furthermore, both the first and second mounting plates are equipped with mounting bolts for connecting the drone body.

[0013] (III) Beneficial Effects

[0014] Compared with the prior art, this utility model provides an integrated UAV motor ESC mounting mechanism, which has the following advantages:

[0015] This integrated drone motor ESC mounting mechanism has a second mounting plate inserted into a first mounting plate with a slot. The first mounting plate is rotatably connected to a connecting component that is threaded to the threaded groove of the second mounting plate. By rotating the connecting component, the overall length of the first and second mounting plates can be adjusted to accommodate ESCs of different sizes, thus improving the versatility of the device. Attached Figure Description

[0016] Figure 1 This is a three-dimensional structural diagram of the present invention;

[0017] Figure 2 This is a top view of the structure of this utility model;

[0018] Figure 3 This utility model Figure 2 Schematic diagram of the cross-sectional structure at point AA.

[0019] In the diagram: 1. Electronic speed controller; 2. First mounting plate; 3. Second mounting plate; 4. First fixing plate; 5. Second fixing plate; 6. First fixing strip; 7. Second fixing strip; 8. Threaded groove; 9. Connecting assembly; 10. Threaded rod; 11. Rotating block; 12. Rotating handle; 13. Supplementary part; 14. Mounting bolt; 15. Limiting plate; 16. Fixing bolt. Detailed Implementation

[0020] The technical solutions of the present utility model will be clearly and completely described below with reference to the accompanying drawings of the embodiments. Obviously, the described embodiments are only some embodiments of the present utility model, and not all embodiments. Based on the embodiments of the present utility model, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the protection scope of the present utility model.

[0021] Please see Figure 1-3 An integrated UAV motor ESC mounting mechanism includes an electronic speed controller 1, a first mounting plate 2, and a second mounting plate 3. One end of the first mounting plate 2 has a slot, into which the second mounting plate 3 is inserted and slidably connected. A first fixing plate 4 and a second fixing plate 5 are fixedly connected to the tops of the first mounting plate 2 and the second mounting plate 3, respectively. A threaded groove 8 is formed on the end face of the second mounting plate 3. A through slot is rotatably connected to the first mounting plate 2, and a connecting component 9 is threadedly connected to the threaded groove 8. The connecting component 9 includes a threaded rod 10, with a threaded rod 10 near one end... The side wall is provided with a smooth part, and a rotating block 11 that is rotatably connected to the smooth part is fixedly connected to the first mounting plate. The end of the threaded rod 10 is equipped with a rotating handle 12 with a cross groove. When a tool is inserted into the groove, the threaded rod is rotated in the threaded groove of the second mounting plate, which can drive the second mounting plate to slide in the slide groove of the first mounting plate to adjust the overall length of the first mounting plate and the second mounting plate so that different sizes of electronic speed controllers can be adapted to the first mounting plate and the second mounting plate. The first fixing plate and the second fixing plate clamp and fix the electronic speed controller.

[0022] The second mounting plate 3 is fixedly connected to the outer wall of the end away from the first mounting plate 2 with an additional part 13, so that the top of the second mounting plate 3 is coplanar with the top of the first mounting plate 2, so that the electronic speed controller placed on the top of the first mounting plate and the second mounting plate is stably supported.

[0023] The top of the first mounting plate 2 is fixedly connected to a first fixing strip 6, and the top of the supplementary part 13 is fixedly connected to a second fixing strip 7. The cross-section of the first fixing strip is trapezoidal, and the cross-section of the second fixing strip is rectangular, so that the first fixing strip 6 and the second fixing strip 7 have different shapes. The electronic speed controller is inserted from the side along the top of the first mounting plate and the second mounting plate to distinguish the installation position of the electronic speed controller 1 on the device, so that personnel can install it quickly.

[0024] U-shaped limiting plates 15 are inserted from the bottom along both sides of the second mounting plate 3, and fixing bolts 16 that are threadedly connected to the second mounting plate 3 are provided on both sides of the limiting plate 15 for limiting and fixing the electronic speed controller 1.

[0025] Both the first mounting plate 2 and the second mounting plate 3 are equipped with mounting bolts 14 for connecting the drone body.

[0026] In summary, when using this integrated UAV motor ESC mounting mechanism, the electronic speed controller 1 is inserted along the first fixing bar 6 and the second fixing bar 7 into the top of the first mounting plate 2 and the second mounting plate 3. The rotating handle 12 is then rotated, and the threaded rod 10 rotates in the threaded groove 8 of the second mounting plate 3, shortening the overall length of the first mounting plate 2 and the second mounting plate 3. This clamps the electronic speed controller 1 between the first fixing plate 4 and the second fixing plate 5. Then, a U-shaped limiting plate 15 is inserted into the bottom of the second mounting plate 3, and the fixing bolt 16 is rotated to fix the U-shaped limiting plate 15 on the second mounting plate 3, thus limiting the electronic speed controller 1.

[0027] Then install the device on the drone and use a tool to turn each mounting bolt 14 to fix the device and electronic speed controller 1 to the drone.

[0028] Although 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 alterations can be made to these embodiments without departing from the principles and spirit of the present invention, the scope of which is defined by the appended claims and their equivalents.

Claims

1. An integrated UAV motor ESC mounting mechanism, comprising an electronic speed controller (1), a first mounting plate (2), and a second mounting plate (3), characterized in that: The first mounting plate (2) has a slot at one end, and the second mounting plate (3) is inserted into the slot and slidably connected. The top of the first mounting plate (2) and the second mounting plate (3) are respectively fixedly connected to the first fixing plate (4) and the second fixing plate (5). The end face of the second mounting plate (3) has a threaded groove (8). The first mounting plate (2) is rotatably connected to a through slot and is threadedly connected to the threaded groove (8) to a connecting component (9). The connecting component (9) is rotated on the threaded groove (8) to make the first fixing plate (4) and the second fixing plate (5) move closer or further away from each other, which is used to adapt electronic speed controllers (1) of different sizes between the first fixing plate (4) and the second fixing plate (5).

2. The integrated UAV motor ESC mounting mechanism according to claim 1, characterized in that: The second mounting plate (3) is fixedly connected to the outer wall of the end away from the first mounting plate (2) with an additional part (13) so that the top of the second mounting plate (3) is coplanar with the top of the first mounting plate (2).

3. The integrated UAV motor ESC mounting mechanism according to claim 2, characterized in that: The top of the first mounting plate (2) is fixedly connected to a first fixing strip (6), and the top of the supplementary part (13) is fixedly connected to a second fixing strip (7). The first fixing strip (6) and the second fixing strip (7) have different shapes and are used to distinguish the installation position of the electronic speed controller (1).

4. The integrated UAV motor ESC mounting mechanism according to claim 1, characterized in that: The connecting assembly (9) includes a threaded rod (10), a smooth part is provided on the side wall near one end of the threaded rod (10), and a rotating block (11) is fixedly connected to the smooth part. A rotating handle (12) with a cross groove is installed at the upper end of the threaded rod (10).

5. The integrated UAV motor ESC mounting mechanism according to claim 1, characterized in that: The second mounting plate (3) has U-shaped limiting plates (15) inserted from the bottom along both sides, and both sides of the limiting plates (15) are provided with fixing bolts (16) that are threadedly connected to the second mounting plate (3) for limiting and fixing the electronic speed controller (1).

6. An integrated UAV motor ESC mounting mechanism according to any one of claims 1 to 5, characterized in that: Both the first mounting plate (2) and the second mounting plate (3) are equipped with mounting bolts (14) for connecting the drone body.

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