Camera suspension device for aerial photography of unmanned aerial vehicle

By combining threaded connections and a gyroscope mechanism with a counterweight design, the stability problem of drone cameras under complex motion conditions was solved, enabling stable shooting in various flight environments.

CN223891216UActive Publication Date: 2026-02-10QINGHAI YIHUA NETWORK TECH CO LTD
View PDF 0 Cites 0 Cited by

Patent Information

Application Number
CN202520709334.X
Authority / Receiving Office
CN · China
Patent Type
Utility models(China)
Current Assignee / Owner
Priority Date
2025-04-14
Filing Date
2025-04-15
Publication Date
2026-02-10
Estimated Expiration
2035-04-15

AI Technical Summary

Technical Problem

Existing drone camera suspension devices struggle to maintain camera stability under complex motion conditions, resulting in tilted and shaky footage that affects image and video quality.

Method used

The connecting seat and connecting column are connected by threads. Combined with the gyroscope mechanism and counterweight on the upper and lower rotating frame, the gyroscope effect and weight balance are used to resist changes in the flight attitude of the drone and ensure the stability of the camera.

Benefits of technology

The camera remains stable and shake is suppressed during the complex flight of the drone, meeting the requirements for high-quality aerial photography and adapting to various flight environments and missions.

✦ Generated by Eureka AI based on patent content.

Smart Images

  • Figure CN223891216U_ABST
    Figure CN223891216U_ABST
Patent Text Reader

Abstract

The utility model discloses a camera suspension device for aerial photography of an unmanned aerial vehicle, which relates to the technical field of suspension devices and comprises a connecting seat, the connecting seat is in threaded connection with an unmanned aerial vehicle body, a connecting column is in threaded connection with the connecting seat, and a suspension device is arranged below the connecting column. The suspension device comprises a left-right rotating frame and an up-down rotating frame, a gyroscope mechanism and two balancing weights are arranged on the up-down rotating frame, the two balancing weights are arranged on the two sides of the gyroscope mechanism, a camera is arranged on the gyroscope mechanism, and the gyroscope mechanism comprises a rotating disc, a clamping disc and a motor. The method can effectively resist attitude change of the unmanned aerial vehicle, restrain camera jitter and adapt to complex flight environments and tasks such as strong wind and rapid steering.
Need to check novelty before this filing date? Find Prior Art

Description

Technical Field

[0001] This utility model relates to the field of suspension device technology, specifically to a camera suspension device for drone aerial photography. Background Technology

[0002] With the rapid development of drone technology, its application areas are constantly expanding, especially in scenarios requiring high-quality image acquisition such as film and television shooting, surveying, and inspection, where drone cameras play a crucial role. However, existing drone camera mounting devices have significant limitations.

[0003] Ordinary suspension systems struggle to handle the complex movements of drones during flight. When a drone wobbles left or right or back and forth, the camera easily shakes, resulting in severe tilting and shaky footage that significantly impacts image and video quality. In film and television production, unstable footage degrades visual effects and fails to meet professional shooting requirements; in surveying, tilted images can lead to deviations in measurement data, affecting surveying accuracy; and during inspections, blurry, shaky footage hinders accurate identification of target objects.

[0004] With the market demanding increasing stability and accuracy of drone footage, it is urgent to develop a suspension device that can ensure the camera remains horizontally stable even when the drone is rotating or swaying. Utility Model Content

[0005] The purpose of this utility model is to provide a camera suspension device for drone aerial photography in order to solve the above problems.

[0006] To achieve the above objectives, this utility model specifically adopts the following technical solution:

[0007] A camera suspension device for drone aerial photography includes a connecting base that is threadedly connected to the drone body. A connecting post is threadedly connected to the connecting base, and a suspension device is disposed below the connecting post. The suspension device includes a left-right rotating frame and a right-up rotating frame. A gyroscope mechanism and two counterweights are disposed on the right-side of the gyroscope mechanism. A camera is disposed on the gyroscope mechanism, which includes a rotating disk, a locking disk, and a motor.

[0008] Furthermore, the left and right rotating frame includes a connecting horizontal tube, a first steering tube, two rotating mechanisms, and two first connecting pipe fittings. The connecting horizontal tube includes a tee pipe, two second steering tubes, and two second connecting pipe fittings. The first steering tube is fixedly installed together with the bottom of the connecting column. Each rotating mechanism includes a rotating shaft and two bearings. The two bearings on the rotating mechanism are respectively fixedly snapped into the inside of the two first connecting pipe fittings. The other ends of the two first connecting pipe fittings are respectively fixedly snapped into the first steering tube and the tee pipe.

[0009] Furthermore, the upper and lower rotating frame includes an installation tube, two third steering tubes, two third connecting pipes, and two rotating mechanisms. The third steering tubes are fixedly connected to the third connecting pipes, and each of the rotating mechanisms is disposed between the third connecting pipe and the installation tube.

[0010] Furthermore, the mounting tube has a snap-fit ​​groove, and the snap-fit ​​disc snaps into the mounting tube at the position of the snap-fit ​​groove.

[0011] Furthermore, a mounting bracket is provided on the mounting tube, and the mounting bracket and the snap-fit ​​plate are fixedly mounted on the mounting tube together by the first bolt, and the camera is snapped onto the mounting bracket.

[0012] Furthermore, a second bolt is provided on the mounting tube, and the counterweight is fixedly mounted on the mounting tube by the second bolt.

[0013] The beneficial effects of this utility model are as follows:

[0014] This invention establishes a stable and reliable connection structure between the suspension device and the UAV body through a threaded connection between the connecting seat and the connecting column, ensuring that the entire device will not easily loosen during flight and laying a solid foundation for stable camera operation. Simultaneously, the gyro mechanism and counterweight on the upper and lower rotating frames work together, utilizing the gyro effect and the weight balance of the counterweight to effectively resist various attitude changes during UAV flight, greatly enhancing camera stability. Even when the UAV performs large movements such as rolling or tilting, the camera can remain relatively stable, effectively suppressing shaking.

[0015] This invention, through the design of its suspension device, enables it to adapt to various complex flight environments and mission requirements. Whether in strong winds or when rapid turns or sudden stops are required, it ensures stable camera operation, meets the diverse needs of different industries for drone aerial photography, and promotes the in-depth application of drones in more fields.

[0016] In summary, the suspension system design effectively resists changes in the drone's attitude, suppresses camera shake, and can adapt to complex flight environments and missions such as strong winds and rapid turns. Attached Figure Description

[0017] Figure 1 This is a schematic diagram of the overall structure of this utility model;

[0018] Figure 2 This is a schematic diagram of the connector structure of this utility model;

[0019] Figure 3 This is a schematic diagram of the disassembly and assembly of the suspension device of this utility model;

[0020] Figure 4 This is a schematic diagram of the left and right rotating frame structure of this utility model;

[0021] Figure 5 This is a schematic diagram of the upper and lower rotating frame structure of this utility model;

[0022] Figure 6 This is a schematic diagram of the gyroscope mechanism of this utility model;

[0023] Figure 7 This is a schematic diagram of the disassembly and assembly of the gyroscope mechanism of this utility model.

[0024] Reference numerals: 1. Connecting seat; 2. Connecting column; 3. Suspension device; 4. Left and right rotating frame; 41. Connecting horizontal tube; 411. Second steering tube; 412. Second connecting pipe fitting; 413. T-pipe; 42. First steering tube; 43. First connecting pipe fitting; 44. Rotating mechanism; 441. Bearing; 442. Rotating shaft; 5. Upper and lower rotating frame; 51. Third steering tube; 52. Third connecting pipe fitting; 53. Mounting tube; 531. Snap-fit ​​groove; 6. Gyroscope mechanism; 61. Rotating disk; 62. Snap-fit ​​disk; 63. Motor; 7. Counterweight; 71. Second bolt; 8. Mounting frame; 81. First bolt. Detailed Implementation

[0025] To make the objectives, technical solutions, and advantages of the embodiments of this utility model clearer, the technical solutions of the embodiments of this utility model will be clearly and completely described below with reference to the accompanying drawings.

[0026] A preferred embodiment of the present invention, a camera suspension device for drone aerial photography, will be described in detail below.

[0027] Example 1, as Figures 1-7As shown, a camera suspension device 3 for drone aerial photography includes a connecting seat 1, which is threadedly connected to the drone body. A connecting post 2 is threadedly connected to the connecting seat 1. A suspension device 3 is arranged below the connecting post 2. The suspension device 3 includes a left-right rotating frame 4 and an up-down rotating frame 5. A gyroscope mechanism 6 and two counterweights 7 are arranged on the up-down rotating frame 5. The two counterweights 7 are arranged on both sides of the gyroscope mechanism 6. A camera is arranged on the gyroscope mechanism 6. The gyroscope mechanism 6 includes a rotating disk 61, a locking disk 62, and a motor 63.

[0028] During operation, the connecting seat 1 is tightly connected to the drone body via threads, providing a stable mounting base for the entire suspension system. The connecting column 2 is also threaded onto the connecting seat 1, playing a crucial role in connecting the connecting seat and the suspension system 3, ensuring a secure connection between the suspension system and the drone. To prevent camera shake due to turning, the gyro mechanism 6 and two counterweights 7 on the upper and lower rotating frame 5 are core components ensuring camera stability. The rotating disk 61 and the locking plate 62 in the gyro mechanism 6 work together, with the motor 63 providing power to the rotating disk 61, causing it to rotate at high speed. Based on the gyro effect, regardless of how the drone flies or changes its attitude, the rotating disk 61 maintains its stable direction, thereby driving the connected camera to maintain a stable shooting angle. The two counterweights 7 are distributed on both sides of the gyro mechanism 6. During drone flight, the weight of the counterweights 7 keeps the camera horizontal, reducing shaking and maintaining a relatively stable position. Even during large movements such as rolling and tilting of the drone, the counterweights effectively suppress camera shake, ensuring the stability and clarity of the captured footage, meeting the requirements of high-quality aerial photography.

[0029] It is worth noting that the left-right rotating frame 4 and the up-down rotating frame 5 provide a basis for the camera to maintain balance through the gyroscope mechanism 6 and the counterweight 7.

[0030] Example 2, as Figures 2-3 As shown, the left and right rotating frame 4 includes a connecting horizontal tube 41, a first steering tube 42, two rotating mechanisms 44, and two first connecting pipe fittings 43. The connecting horizontal tube 41 includes a tee pipe 413, two second steering tubes 411, and two second connecting pipe fittings 412. The first steering tube 42 is fixedly installed together with the bottom of the connecting column 2. Each rotating mechanism 44 includes a rotating shaft 442 and two bearings 441. The two bearings 441 on the rotating mechanism 44 are respectively fixedly snapped into the inside of the two first connecting pipe fittings 43. The other ends of the two first connecting pipe fittings 43 are respectively fixedly snapped into the first steering tube 42 and the tee pipe 413.

[0031] Example 2, as Figures 3-7As shown, the upper and lower rotating frame 5 includes a mounting pipe 53, two third steering pipes 51, two third connecting pipes 52 and two rotating mechanisms 44. The third steering pipes 51 and the third connecting pipes 52 are fixedly connected together, and each rotating mechanism 44 is arranged between the third connecting pipe 52 and the mounting pipe 53.

[0032] Furthermore, the mounting tube 53 is provided with a snap-fit ​​groove 531, and the snap-fit ​​disc 62 snaps into the mounting tube 53 at the position of the snap-fit ​​groove 531.

[0033] Furthermore, a mounting bracket 8 is provided on the mounting tube 53. The mounting bracket 8 and the snap-fit ​​plate 62 are fixedly mounted on the mounting tube 53 together by the first bolt 81, and the camera is snapped onto the mounting bracket 8.

[0034] Example 3, as Figure 7 As shown, a second bolt 71 is provided on the mounting pipe 53, and the counterweight 7 is fixedly installed on the mounting pipe 53 by the second bolt 71.

[0035] The above description of the disclosed embodiments enables those skilled in the art to make or use the present invention. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the general principles defined herein may be implemented in other embodiments without departing from the spirit or scope of the present invention. Therefore, the present invention is not to be limited to the embodiments shown herein, but is to be accorded the widest scope consistent with the principles and novel features disclosed herein.

Claims

1. A camera suspension device for drone aerial photography, comprising a connecting base (1), characterized in that, The connecting seat (1) is threadedly connected to the UAV body. A connecting post (2) is threadedly connected to the connecting seat (1). A suspension device (3) is provided below the connecting post (2). The suspension device (3) includes a left and right rotating frame (4) and an up and down rotating frame (5). A gyroscope mechanism (6) and two counterweights (7) are provided on the up and down rotating frame (5). The two counterweights (7) are provided on both sides of the gyroscope mechanism (6). A camera is provided on the gyroscope mechanism (6). The gyroscope mechanism (6) includes a rotating disk (61), a locking disk (62), and a motor (63).

2. The camera suspension device for drone aerial photography according to claim 1, characterized in that, The left and right rotating frame (4) includes a connecting horizontal tube (41), a first steering tube (42), two rotating mechanisms (44) and two first connecting pipes (43). The connecting horizontal tube (41) includes a tee pipe (413), two second steering tubes (411) and two second connecting pipes (412). The first steering tube (42) is fixedly installed together with the bottom of the connecting column (2). Each of the rotating mechanisms (44) includes a rotating shaft (442) and two bearings (441). The two bearings (441) on the rotating mechanism (44) are respectively fixedly snapped into the inside of the two first connecting pipes (43). The other ends of the two first connecting pipes (43) are respectively fixedly snapped into the first steering tube (42) and the tee pipe (413).

3. A camera suspension device for drone aerial photography according to claim 2, characterized in that, The upper and lower rotating frame (5) includes an installation tube (53), two third steering tubes (51), two third connecting pipes (52) and two rotating mechanisms (44). The third steering tubes (51) and the third connecting pipes (52) are fixedly connected together, and each of the rotating mechanisms (44) is arranged between the third connecting pipe (52) and the installation tube (53).

4. A camera suspension device for drone aerial photography according to claim 3, characterized in that, The mounting tube (53) has a snap-fit ​​groove (531) and the snap-fit ​​disc (62) snaps into the mounting tube (53) at the position of the snap-fit ​​groove (531).

5. A camera suspension device for drone aerial photography according to claim 4, characterized in that, The mounting tube (53) is provided with a mounting bracket (8), and the mounting bracket (8) and the snap-fit ​​plate (62) are fixedly mounted on the mounting tube (53) together by the first bolt (81). The camera is snapped onto the mounting bracket (8).

6. A camera suspension device for drone aerial photography according to claim 3, characterized in that, The mounting tube (53) is provided with a second bolt (71), and the counterweight (7) is fixedly mounted on the mounting tube (53) by the second bolt (71).