CN215371736U

CN215371736U - Triaxial unmanned aerial vehicle cloud platform

Info

Publication number: CN215371736U
Application number: CN202121784057.7U
Authority: CN
Inventors: 屈鹏
Original assignee: Individual
Current assignee: Individual
Priority date: 2021-08-02
Filing date: 2021-08-02
Publication date: 2021-12-31
Anticipated expiration: 2031-08-02

Abstract

The utility model discloses a three-axis unmanned aerial vehicle holder, which comprises: the cloud platform control panel is used for being connected and installed with the unmanned aerial vehicle main body, and a damping frame is connected below the cloud platform control panel; the first rotating frame is rotatably arranged below the shock absorption frame, and a second rotating frame is connected below the first rotating frame; the third rotating frame is arranged at the lower end of the second rotating frame and comprises a first fixing frame, a second fixing frame and a bearing; and the camera is arranged in the middle of the inner side of the third rotating frame and is respectively connected with the first fixing frame and the second fixing frame in a rotating manner. This three-axis unmanned aerial vehicle cloud platform sets up a plurality of shock rings can help servo motor to carry out the shock attenuation at the during operation to in the stability of improvement camera when the angle modulation, be favorable to reducing the rocking of taking the picture, in addition through additional counter weight metal cover on the camera, can increase the weight of camera, further improve the stability of camera.

Description

Triaxial unmanned aerial vehicle cloud platform

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to a three-axis unmanned aerial vehicle holder.

Background

The unmanned aerial vehicle cloud platform is that unmanned aerial vehicle is used for the support equipment of task load such as installation, fixed camera. The unmanned aerial vehicle cloud platform on the existing market is relatively poor to the fixed steadiness of camera in the use, and is not convenient for carry out the shock attenuation to unmanned aerial vehicle's angle accommodate motor, leads to the camera to rock obvious problem at shooting in-process picture, for this reason, we provide a triaxial unmanned aerial vehicle cloud platform.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a three-axis unmanned aerial vehicle holder, which solves the problems that the unmanned aerial vehicle holder in the existing market has poor fixing stability on a camera in the use process, and is inconvenient to absorb shock of an angle adjusting motor of an unmanned aerial vehicle, so that the camera obviously shakes in the shooting process.

In order to achieve the purpose, the utility model provides the following technical scheme: a three-axis unmanned aerial vehicle pan-tilt, comprising:

the cloud platform control panel is used for being connected and installed with the unmanned aerial vehicle main body, and a damping frame is connected below the cloud platform control panel;

the first rotating frame is rotatably arranged below the shock absorption frame, and a second rotating frame is connected below the first rotating frame;

the rotating frame III is arranged at the lower end of the rotating frame II and comprises a first fixing frame, a second fixing frame and a bearing, the left side of the first fixing frame is connected with the second fixing frame in a clamping mode, and the bearing is arranged inside the second fixing frame;

and the camera is arranged in the middle of the inner side of the third rotating frame and is respectively connected with the first fixing frame and the second fixing frame in a rotating manner.

Preferably, the shock-absorbing mount further comprises:

the shock absorption balls are arranged at four corners inside the shock absorption frame;

and the connecting frame is arranged above the middle part of the damping frame and penetrates through the upper surface of the holder control plate.

Preferably, the first rotating frame further comprises:

the first servo motor is installed inside the first rotating frame, the outer wall of the first servo motor is fixed to the inner wall of the connecting frame, and the output end of the first servo motor is fixed to the second rotating frame.

Preferably, the second rotating frame further comprises:

and the second servo motor is arranged inside the second rotating frame, and the output end of the second servo motor is fixed with the three phases of the rotating frame.

Preferably, the camera further comprises:

the transparent cover is arranged on the front end face of the camera;

the counterweight lens front cover is arranged inside the rear side of the camera and is made of zinc alloy;

a lens plate mounted on a rear side of the counterweight lens front cover;

a third servo motor which is arranged inside the counterweight lens front cover;

and the counterweight lens rear cover is arranged on the rear side of the servo motor III and is made of zinc alloy.

Preferably, the method further comprises the following steps:

and the damping rings are respectively sleeved between the joints of the first servo motor and the first rotating frame and between the joints of the second servo motor and the second rotating frame.

Compared with the prior art, the utility model has the beneficial effects that:

this triaxial unmanned aerial vehicle cloud platform sets up the setting through the rotating turret of three not equidirectional, can drive the camera and carry out the ascending angular rotation adjustment of triaxial side, the shock attenuation ball of setting effectively helps the shock attenuation frame to carry out the shock attenuation, be favorable to maintaining the stability of unmanned aerial vehicle camera when flight, a plurality of shock attenuation circles that set up simultaneously can help servo motor to carry out the shock attenuation at the during operation, so as to improve the stability of camera when the angular adjustment, be favorable to reducing rocking of taking the picture, in addition through additional zinc alloy counter weight metal lid on the camera, can increase the weight of camera, further improve the stability of camera.

Drawings

FIG. 1 is a schematic perspective view of the present invention;

FIG. 2 is a schematic front view of the present invention;

FIG. 3 is a right side view of the present invention;

FIG. 4 is an exploded view of the present invention;

FIG. 5 is an exploded view of the first and second turrets of the present invention;

fig. 6 is an exploded view of the second fixing frame and the camera of the present invention.

In the figure: 1. a cradle head control panel; 2. a shock-absorbing mount; 21. a shock absorbing ball; 22. a connecting frame; 3. a first rotating frame; 31. a first servo motor; 4. a second rotating frame; 41. a servo motor II; 5. a rotating frame III; 51. a first fixing frame; 52. a second fixing frame; 53. a bearing; 6. a camera; 61. a transparent cover; 62. a counterweight lens front cover; 63. a lens plate; 64. a servo motor III; 65. a rear cover of the counterweight lens; 7. a damping ring.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-6, the present invention provides a technical solution: a three-axis unmanned aerial vehicle pan-tilt, comprising:

the cloud platform control panel 1 is used for being connected and installed with the unmanned aerial vehicle main body, and a damping frame 2 is connected below the cloud platform control panel 1;

the rotating frame I3 is rotatably arranged below the shock absorption frame 2, and a rotating frame II 4 is connected below the rotating frame I3;

the rotating frame III 5 is installed at the lower end of the rotating frame II 4, the rotating frame III 5 comprises a first fixed frame 51, a second fixed frame 52 and a bearing 53, the left side of the first fixed frame 51 is connected with the second fixed frame 52 in a clamping mode, and the bearing 53 is installed inside the second fixed frame 52;

the camera 6 is arranged at the middle position of the inner side of the rotating frame III 5 and is respectively and rotatably connected with the fixing frame I51 and the fixing frame II 52, the arrangement of the rotating frame in three different directions can drive the camera 6 to carry out angular rotation adjustment in the three-axis direction,

shock attenuation frame 2 still including:

the damping balls 21 are arranged at four corners inside the damping frame 2, and the damping balls 21 effectively help the damping frame 2 to damp, so that the stability of the camera 6 during the flying of the unmanned aerial vehicle is maintained;

a connecting frame 22 which is arranged at the upper position of the middle part of the damping frame 2 and penetrates through the upper surface of the tripod head control plate 1,

the first rotating frame 3 further comprises:

the first servo motor 31 is arranged inside the first rotating frame 3, the outer wall of the first servo motor 31 is fixed with the inner wall of the connecting frame 22, the output end of the first servo motor 31 is fixed with the second rotating frame 4,

the second rotating frame 4 further comprises:

a second servo motor 41 which is arranged inside the second rotating frame 4, the output end of the second servo motor 41 is fixed with the third rotating frame 5,

the camera 6 further comprises:

a transparent cover 61 attached to a front end surface of the camera 6;

a counterweight lens front cover 62 which is installed inside the rear side of the camera 6 and is made of zinc alloy;

a lens plate 63 which is arranged at the rear side of the counterweight lens front cover 62, wherein a screw instrument can be arranged on the lens plate 63 to control the lens stability of pitching, rolling and course;

a third servo motor 64 mounted inside the counterweight lens front cover 62;

the counterweight lens rear cover 65 is arranged at the rear side of the servo motor III 64 and is made of zinc alloy, the counterweight lens front cover 62 and the counterweight lens rear cover 65 are both supported by zinc alloy, the weight of the whole lens is increased, the use stability is improved,

the utility model provides a triaxial unmanned aerial vehicle cloud platform, still including:

the damping rings 7 are respectively sleeved between the joints of the first servo motor 31 and the first rotating frame 3 and between the joints of the second servo motor 41 and the second rotating frame 4, and the damping rings 7 can help the servo motors to damp during working so as to improve the stability of the camera 6 during angle adjustment and reduce the shaking of a shot picture.

The working principle is as follows: for the three-axis unmanned aerial vehicle holder, firstly, the whole device is assembled with the unmanned aerial vehicle through the holder control panel 1, the shock absorption ball 21 can help the shock absorption frame 2 to absorb shock, the tail end of the servo motor I31 is fixed with the connecting frame 22, when the angle of the camera 6 needs to be adjusted, the servo motor I31 is started firstly, the servo motor I31 drives the rotating frame II 4 to rotate relative to the rotating frame I3, the servo motor II 41 is started, the servo motor II 41 drives the rotating frame III 5 to rotate relative to the rotating frame II 4, the servo motor III 64 is started, the servo motor III 64 drives the camera 6 to rotate relative to the fixing frame I51 and the fixing frame II 52 and rotates inside the bearing 53, the weight of the camera 6 is increased by the counterweight lens front cover 62 and the counterweight lens rear cover 65, the stability of the camera 6 is improved, the screw instrument can be configured on the lens plate 63 to control pitching and rolling, the camera lens stability of course, transparent cover 61 protects the camera lens front end, and damping ring 7 can help servo motor carry out the shock attenuation at the during operation to improve the stability of camera 6 when the angle modulation, be favorable to reducing the rocking of taking the picture, accomplish the use of whole triaxial unmanned aerial vehicle cloud platform just so.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the utility model, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides a triaxial unmanned aerial vehicle cloud platform which characterized in that includes:

the cloud platform control panel (1) is used for being connected and installed with the unmanned aerial vehicle main body, and a damping frame (2) is connected below the cloud platform control panel (1);

the rotating frame I (3) is rotatably arranged below the shock absorption frame (2), and a rotating frame II (4) is connected below the rotating frame I (3);

the rotating frame III (5) is installed at the lower end of the rotating frame II (4), the rotating frame III (5) comprises a first fixing frame (51), a second fixing frame (52) and a bearing (53), the left side of the first fixing frame (51) is connected with the second fixing frame (52) in a clamping mode, and the bearing (53) is installed inside the second fixing frame (52);

and the camera (6) is arranged in the middle position of the inner side of the third rotating frame (5) and is respectively in rotating connection with the first fixing frame (51) and the second fixing frame (52).

2. The three-axis UAV pan/tilt head according to claim 1, wherein the shock absorbing mount (2) further comprises:

shock absorption balls (21) which are installed at four inner corners of the shock absorption frame (2);

the connecting frame (22) is arranged above the middle of the damping frame (2) and penetrates through the upper surface of the holder control plate (1).

3. The three-axis UAV pan/tilt head of claim 2, wherein the first turret (3) further comprises:

the first servo motor (31) is installed inside the first rotating frame (3), the outer wall of the first servo motor (31) is fixed to the inner wall of the connecting frame (22), and the output end of the first servo motor (31) is fixed to the second rotating frame (4).

4. The three-axis UAV pan/tilt head of claim 1, wherein the second turret (4) further comprises:

and the second servo motor (41) is arranged inside the second rotating frame (4), and the output end of the second servo motor (41) is fixed with the third rotating frame (5).

5. The three-axis UAV pan/tilt head according to claim 1, wherein the camera (6) further comprises:

a transparent cover (61) attached to the front end surface of the camera (6);

a counterweight lens front cover (62) which is arranged inside the rear side of the camera (6) and is made of zinc alloy;

a lens plate (63) mounted on a rear side of the counterweight lens front cover (62);

a third servo motor (64) mounted inside the counterweight lens front cover (62);

and a counterweight lens rear cover (65) which is arranged at the rear side of the servo motor III (64) and is made of zinc alloy.

6. The three-axis UAV pan/tilt head of claim 4, further comprising:

and the damping rings (7) are respectively sleeved between the joints of the first servo motor (31) and the first rotating frame (3) and between the joints of the second servo motor (41) and the second rotating frame (4).