A remote controller for a drone

By using an electromagnet to drive the spindle in the drone remote controller to automatically press the power button, the problem of manual power on/off in existing remote controllers has been solved, achieving automatic power on/off and improving convenience and emergency response capabilities.

CN224341933UActive Publication Date: 2026-06-09GUANGZHOU IMAPCLOUD INTELLIGENT TECH CO LTD

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
GUANGZHOU IMAPCLOUD INTELLIGENT TECH CO LTD
Filing Date
2025-05-19
Publication Date
2026-06-09

AI Technical Summary

Technical Problem

Existing drone remote controllers require manual operation to turn the drone on and off, which may increase the burden of use or delay the start-up or shutdown of the drone in frequent use or emergency situations.

Method used

A drone remote controller was designed, which uses an electromagnet and a movable spindle structure. By energizing the spindle, it moves toward the power switch to achieve automatic power on and off.

Benefits of technology

It enables automatic power on/off functionality for drone remote controllers, reducing the burden of manual operation and improving ease of use and response speed in emergency situations.

✦ Generated by Eureka AI based on patent content.

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Abstract

The application provides a kind of unmanned plane remote controller, it is related to unmanned plane remote control technical field.The unmanned plane remote controller includes fixed frame, remote controller body and electromagnet, remote controller body is set on fixed frame, and key is arranged on remote controller body, electromagnet includes electromagnet body and movable core shaft that is arranged in electromagnet body, electromagnet body is used to drive core shaft to move towards key in the state of energization, and the unmanned plane remote controller can realize automatic on-off.
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Description

Technical Field

[0001] This application relates to the field of unmanned aerial vehicle (UAV) remote control technology, and more specifically, to a UAV remote controller. Background Technology

[0002] With the rapid development of drone technology, drones are increasingly being used in aerial photography, agriculture, logistics, surveying and mapping, and other fields. As the core device for controlling drones, the functionality and ease of use of the drone remote controller directly impact the user experience.

[0003] Existing drone remote controllers typically use physical buttons or switches to turn the drone on and off, requiring users to manually press the switch or button to start or stop the remote. While this method is simple and direct, it can be inconvenient in certain situations. For example, when users need to frequently turn the remote on and off, manual operation may increase the burden of use; or in emergency situations, manual operation may delay the drone's start-up or shutdown.

[0004] Furthermore, as drone applications become more diverse and complex, users' demands for intelligent remote controllers are constantly increasing. Automatic power-on / off functionality, as part of this intelligent feature, can improve the ease of use and user experience. However, currently, automatic power-on / off functionality is not yet available in the drone remote controller field, and users still need to rely on manual operation to turn the drone on and off. Utility Model Content

[0005] The purpose of this application includes, for example, providing a drone remote controller capable of automatically turning on and off.

[0006] The embodiments of this application can be implemented as follows:

[0007] An embodiment of this application provides a drone remote controller, which includes a fixed frame, a remote controller body, and an electromagnet. The remote controller body is disposed on the fixed frame and has an on / off switch. The electromagnet includes an electromagnet body and a spindle movably disposed through the electromagnet body. The electromagnet body is used to drive the spindle toward the on / off switch when energized.

[0008] Optionally, a resilient pressure block is provided at the end of the mandrel facing the switch.

[0009] Optionally, the elastic block is made of polyurethane material.

[0010] Optionally, a return spring is provided inside the electromagnet body, and the return spring is connected to the spindle to drive the spindle to return to its original position.

[0011] Optionally, the mounting bracket includes a first bracket and a second bracket connected to each other, with the remote control body disposed on the first bracket and the electromagnet body disposed on the second bracket.

[0012] Optionally, the first bracket and the second bracket are detachably connected.

[0013] Optionally, the second bracket includes a first plate, a second plate, and a connecting plate connected between the first plate and the second plate. The first plate and the connecting plate are perpendicular to each other, as are the second plate and the connecting plate. The first plate is connected to the electromagnet body, and the second plate is connected to the first bracket.

[0014] Optionally, the first plate has a first through hole, the second plate has a second through hole, the first plate has a first screw, the second plate has a second screw, the first screw passes through the first through hole and is connected to the electromagnet body, and the second screw passes through the second through hole and is connected to the first bracket.

[0015] Optionally, both the first through hole and the second through hole are oblong holes, and the extension direction of the first through hole is perpendicular to the extension direction of the second through hole.

[0016] Optionally, at least one reinforcing rib is provided between the first plate and the connecting plate, and between the second plate and the connecting plate.

[0017] The beneficial effects of the drone remote controller provided in this application include, for example, in order to realize automatic power on and off, a drone remote controller is designed. The drone remote controller includes a fixed frame, a remote controller body and an electromagnet. The remote controller body is set on the fixed frame and is provided with a power switch. The electromagnet includes an electromagnet body and a spindle that is movably inserted through the electromagnet body. The electromagnet body is used to drive the spindle to move toward the power switch when energized.

[0018] When the drone remote controller needs to be turned on, the electromagnet is powered on. When the electromagnet is powered on, it drives the spindle to move toward the power switch. When the power switch is pressed, the drone is turned on. When the drone remote controller needs to be turned off, the electromagnet is powered on again. When the electromagnet is powered on, it drives the spindle to move toward the power switch again. When the power switch is pressed, the drone is turned off. This achieves automatic power on and off of the drone remote controller. Attached Figure Description

[0019] To more clearly illustrate the technical solutions of the embodiments of this application, the accompanying drawings used in the embodiments will be briefly introduced below. It should be understood that the following drawings only show some embodiments of this application and should not be regarded as a limitation of the scope. For those skilled in the art, other related drawings can be obtained based on these drawings without creative effort.

[0020] Figure 1 This is a schematic diagram of the first-view perspective of the drone remote controller in an embodiment of this application;

[0021] Figure 2 This is a schematic diagram of the second view of the drone remote controller in an embodiment of this application;

[0022] Figure 3 This is a schematic diagram of the second bracket in an embodiment of this application;

[0023] Figure 4 This is a schematic diagram of the electromagnet in an embodiment of this application.

[0024] Icons: 100-Fixed bracket; 110-First bracket; 120-Second bracket; 121-First plate; 1211-First through hole; 122-Second plate; 1221-Second through hole; 123-Connecting plate; 124-Reinforcing rib; 200-Remote control body; 210-Power switch; 300-Electromagnet; 310-Electromagnet body; 320-Mandrel; 321-Elastic pressure block. Detailed Implementation

[0025] To make the objectives, technical solutions, and advantages of the embodiments of this application clearer, the technical solutions of the embodiments of this application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of this application, and not all embodiments. The components of the embodiments of this application described and shown in the accompanying drawings can generally be arranged and designed in various different configurations.

[0026] Therefore, the following detailed description of the embodiments of this application provided in the accompanying drawings is not intended to limit the scope of the claimed application, but merely to illustrate selected embodiments of the application. All other embodiments obtained by those skilled in the art based on the embodiments of this application without inventive effort are within the scope of protection of this application.

[0027] It should be noted that similar labels and letters in the following figures indicate similar items. Therefore, once an item is defined in one figure, it does not need to be further defined and explained in subsequent figures.

[0028] In the description of this application, it should be noted that if terms such as "upper," "lower," "inner," or "outer" are used to indicate the orientation or positional relationship based on the orientation or positional relationship shown in the accompanying drawings, or the orientation or positional relationship that the utility model product is usually placed in during use, they are only for the convenience of describing this application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this application.

[0029] Furthermore, the terms "first" and "second" are used only to distinguish descriptions and should not be interpreted as indicating or implying relative importance.

[0030] It should be noted that, where there is no conflict, the features in the embodiments of this application can be combined with each other.

[0031] As disclosed in the background section, existing drone remote controllers typically use physical buttons or switches to power on / off, requiring users to manually press the switch or button to start or stop the remote controller. While this method is simple and direct, manual operation can increase the burden of use when users need to frequently turn the remote controller on and off; or in emergency situations, manual operation may delay the start-up or shutdown of the drone. Embodiments of this application provide a drone remote controller capable of automatic power on / off.

[0032] Please refer to Figures 1-4 The drone remote controller provided in the embodiments of this application includes a fixed frame 100, a remote controller body 200, and an electromagnet 300. The remote controller body 200 is disposed on the fixed frame 100 and has an on / off switch 210. The electromagnet 300 includes an electromagnet body 310 and a spindle 320 movably disposed through the electromagnet body 310. The electromagnet body 310 is used to drive the spindle 320 to move toward the on / off switch 210 when energized.

[0033] When the remote control body 200 is in the off state, pressing the power button 210 will turn the remote control body 200 on; when the remote control body 200 is in the on state, pressing the power button 210 will turn the remote control body 200 off.

[0034] The electromagnet body 310 can be powered by an external power source via a relay. When the electromagnet body 310 is energized, it drives the spindle 320 to move toward the switch 210.

[0035] When the drone remote controller needs to be turned on, the electromagnet body 310 is powered by an external power source. When the electromagnet body 310 is powered on, it drives the spindle 320 to move toward the power switch 210. The power switch 210 is then pressed to complete the power-on process. When the drone remote controller needs to be turned off, the electromagnet body 310 is powered on again by an external power source. When the electromagnet body 310 is powered on, it drives the spindle 320 to move toward the power switch 210 again. The power switch 210 is then pressed to complete the power-off process. This achieves automatic power-on and power-off for the drone remote controller.

[0036] In this embodiment, an elastic pressure block 321 is provided at the end of the spindle 320 facing the switch 210.

[0037] By providing an elastic pressure block 321 at one end of the spindle 320 facing the switch 210, when the spindle 320 moves toward the switch 210, the elastic pressure block 321 contacts and presses the switch 210, which is less likely to cause damage to the switch 210.

[0038] In this embodiment, the elastic pressure block 321 is made of polyurethane material.

[0039] Polyurethane is a high-performance elastic material, and the elastic block 321 made from it causes minimal damage to the switch 210 when it comes into contact with the switch 210. In other embodiments, the elastic block 321 may also be made of thermoplastic elastomer (TPE) or rubber, and there is no limitation thereto.

[0040] In this embodiment, a reset spring is provided inside the electromagnet body 310. The reset spring is connected to the spindle 320 to drive the spindle 320 to reset.

[0041] When the electromagnet body 310 is energized, the electromagnet body 310 drives the spindle 320 to move toward the switch 210. After the elastic block 321 presses down the switch 210 to turn the machine on or off, the electromagnet body 310 is de-energized, and the spindle 320 is reset under the action of the return spring.

[0042] In this embodiment, the mounting bracket 100 includes a first bracket 110 and a second bracket 120 connected to each other. The remote control body 200 is disposed on the first bracket 110, and the electromagnet body 310 is disposed on the second bracket 120.

[0043] The remote control body 200 is supported on the first bracket 110, and the bottom of the remote control body 200 is fixed to the first bracket 110 by bolts. The power switch 210 is located on the front of the remote control body 200, and the second bracket 120 is roughly Z-shaped and extends away from the front of the remote control body 200.

[0044] In this embodiment, the first bracket 110 and the second bracket 120 are detachably connected.

[0045] For example, the detachable connection methods of the first bracket 110 and the second bracket 120 include, but are not limited to, screwing, bonding or snap-fit ​​connection.

[0046] In this embodiment, the second support 120 includes a first plate 121, a second plate 122, and a connecting plate 123 connected between the first plate 121 and the second plate 122. The first plate 121 and the connecting plate 123, as well as the second plate 122 and the connecting plate 123, are perpendicular to each other. The first plate 121 is connected to the electromagnet body 310, and the second plate 122 is connected to the first support 110.

[0047] The first plate 121 and the second plate 122 are parallel to each other. The second plate 122 is located on the side of the remote control body 200, and the first plate 121 extends toward the front away from the remote control body 200.

[0048] By configuring the second bracket 120 to include a first plate 121, a second plate 122, and a connecting plate 123 connected between the first plate 121 and the second plate 122, it is convenient to connect to the first bracket 110 on the one hand, and convenient to align the spindle 320 in the electromagnet 300 with the switch 210 on the other hand.

[0049] In this embodiment, a first through hole 1211 is provided on the first plate 121, and a second through hole 1221 is provided on the second plate 122. A first screw (not shown) is provided on the first plate 121, and a second screw (not shown) is provided on the second plate 122. The first screw passes through the first through hole 1211 and is connected to the electromagnet body 310, and the second screw passes through the second through hole 1221 and is connected to the first bracket 110.

[0050] Optionally, there are two first through holes 1211 and two second through holes 1221, and correspondingly, there are two first screws and two second screws; the two first screws pass through the two first through holes 1211 respectively and are connected to the electromagnet body 310, and the two second screws pass through the two second through holes 1221 respectively and are connected to the first bracket 110.

[0051] It is understandable that the number of the first through hole 1211 and the second through hole 1221 can be more than three, and the number of the first screw and the second screw can also be more than three; there is no limitation on this.

[0052] In this embodiment, both the first through hole 1211 and the second through hole 1221 are oblong holes, and the extension direction of the first through hole 1211 is perpendicular to the extension direction of the second through hole 1221.

[0053] When both the first through hole 1211 and the second through hole 1221 are oblong holes, the extension direction of the first through hole 1211 is the height direction of the remote control body 200, and the extension direction of the second through hole 1221 is the width direction of the remote control body 200.

[0054] Since both the first through hole 1211 and the second through hole 1221 are oblong holes, during the installation of the electromagnet body 310, the position of the electromagnet body 310 can be adjusted along the height and width directions of the remote control body 200 until the relative height and relative distance between the elastic pressure block 321 and the switch 210 are adjusted to a suitable state.

[0055] In this embodiment, at least one reinforcing rib 124 is provided between the first plate 121 and the connecting plate 123, and between the second plate 122 and the connecting plate 123.

[0056] Optionally, along the height direction of the remote control body 200, two reinforcing ribs 124 are provided between the first plate 121 and the connecting plate 123, and two reinforcing ribs 124 are provided between the second plate 122 and the connecting plate 123, so that deformation is less likely to occur between the first plate 121 and the connecting plate 123 and between the second plate 122 and the connecting plate 123.

[0057] It is understandable that the number of reinforcing ribs 124 between the first plate 121 and the connecting plate 123, and between the second plate 122 and the connecting plate 123, can be one or more, and there is no limitation on this.

[0058] This application embodiment provides a drone remote controller with the following working principle: When the drone remote controller needs to be turned on, an external power source powers the electromagnet body 310. Under this powered state, the electromagnet body 310 drives the spindle 320 to move towards the power switch 210 until the power switch 210 is pressed down by the elastic block 321, completing the power-on process. Then, the power to the electromagnet body 310 is de-energized, and the spindle 320 resets under the action of the return spring. When the drone remote controller needs to be turned off, an external power source powers the electromagnet body 310 again. Under this powered state, the electromagnet body 310 drives the spindle 320 to move towards the power switch 210 again until the power switch 210 is pressed down by the elastic block 321, completing the power-off process. Then, the power to the electromagnet body 310 is de-energized, and the spindle 320 resets under the action of the return spring, thus achieving automatic power-on and power-off for the drone remote controller.

[0059] In summary, this application provides a drone remote controller, which includes a mounting frame 100, a remote controller body 200, and an electromagnet 300. The electromagnet 300 includes an electromagnet body 310 and a spindle 320 movably disposed within the electromagnet body 310. When the drone remote controller needs to be turned on or off, the electromagnet body 310 is energized by an external power source. In the energized state, the electromagnet body 310 drives the spindle 320 to move toward the power switch 210 until the power switch 210 is pressed by the elastic pressure block 321 to complete the power-on or power-off operation, thereby realizing the automatic power-on and power-off of the drone remote controller.

[0060] The above description is merely a specific embodiment of this application, but the scope of protection of this application is not limited thereto. Any variations or substitutions that can be easily conceived by those skilled in the art within the technical scope disclosed in this application should be included within the scope of protection of this application. Therefore, the scope of protection of this application should be determined by the scope of the claims.

Claims

1. A drone remote controller, characterized in that, The device includes a mounting frame, a remote control body, and an electromagnet. The remote control body is mounted on the mounting frame and has an on / off switch. The electromagnet includes an electromagnet body and a spindle movably inserted through the electromagnet body. The electromagnet body is used to drive the spindle toward the on / off switch when energized.

2. The drone remote controller according to claim 1, characterized in that, An elastic pressure block is provided at the end of the spindle facing the switch.

3. The drone remote controller according to claim 2, characterized in that, The elastic pressure block is made of polyurethane material.

4. The drone remote controller according to claim 1, characterized in that, A reset spring is provided inside the electromagnet body, and the reset spring is connected to the spindle to drive the spindle to reset.

5. The drone remote controller according to claim 1, characterized in that, The mounting bracket includes a first bracket and a second bracket connected to each other. The remote control body is mounted on the first bracket, and the electromagnet body is mounted on the second bracket.

6. The drone remote controller according to claim 5, characterized in that, The first bracket and the second bracket are detachably connected.

7. The drone remote controller according to claim 5, characterized in that, The second bracket includes a first plate, a second plate, and a connecting plate connected between the first plate and the second plate. The first plate and the connecting plate are perpendicular to each other, as are the second plate and the connecting plate. The first plate is connected to the electromagnet body, and the second plate is connected to the first bracket.

8. The drone remote controller according to claim 7, characterized in that, The first plate has a first through hole, and the second plate has a second through hole. The first plate has a first screw, and the second plate has a second screw. The first screw passes through the first through hole and is connected to the electromagnet body, and the second screw passes through the second through hole and is connected to the first bracket.

9. The drone remote controller according to claim 8, characterized in that, Both the first through hole and the second through hole are oblong holes, and the extension direction of the first through hole is perpendicular to the extension direction of the second through hole.

10. The drone remote controller according to claim 7, characterized in that, At least one reinforcing rib is provided between the first plate and the connecting plate, and between the second plate and the connecting plate.