CN216734804U

CN216734804U - Unmanned aerial vehicle shock attenuation cloud platform

Info

Publication number: CN216734804U
Application number: CN202121712485.9U
Authority: CN
Inventors: 孙天瑞; 龙进; 张柱
Original assignee: Shenzhen Funsnap Technology Co ltd
Current assignee: Shenzhen Funsnap Technology Co ltd
Priority date: 2021-07-27
Filing date: 2021-07-27
Publication date: 2022-06-14
Anticipated expiration: 2031-07-27

Abstract

An unmanned aerial vehicle shock attenuation cloud platform, it relates to unmanned aerial vehicle technical field. It includes: the cradle head hanging frame is arranged in the unmanned aerial vehicle body and is fixedly assembled with the unmanned aerial vehicle; the holder assembly is fixedly arranged on the holder hanger and is used for realizing the shooting function of the holder; the first damping ball is arranged on one side, close to the head of the unmanned aerial vehicle body, of the holder hanger, one end of the first damping ball is assembled with the holder hanger, and the other end of the first damping ball is assembled with the inner wall of the head of the unmanned aerial vehicle body; and the second damping balls are arranged on two sides of the head of the unmanned aerial vehicle body, far away from the cradle head hanger, and are assembled on the cradle head hanger, and the other end of the cradle head hanger is assembled on the inner wall of the unmanned aerial vehicle body. Adopt above-mentioned technical scheme's unmanned aerial vehicle shock attenuation cloud platform has that the shock attenuation is effectual, shoots stably, structural design is ingenious advantage.

Description

Unmanned aerial vehicle shock attenuation cloud platform

Technical Field

The utility model relates to the technical field of unmanned aerial vehicles, in particular to an unmanned aerial vehicle damping 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 existing unmanned aerial vehicle is easy to be disturbed by air in the flying process due to small size and light weight, so that the attitude of the unmanned aerial vehicle in the air is unstable, and the shooting equipment installed on the unmanned aerial vehicle holder shakes in the shooting process, so that the shot video picture shakes. Therefore, improvements are desired.

SUMMERY OF THE UTILITY MODEL

The utility model aims to overcome the defects and shortcomings of the prior art, and provides an unmanned aerial vehicle damping cradle head.

In order to achieve the purpose, the utility model adopts the technical scheme that: an unmanned aerial vehicle shock attenuation cloud platform includes: the cradle head hanging frame is arranged in the unmanned aerial vehicle body and is fixedly assembled with the unmanned aerial vehicle; the holder assembly is fixedly arranged on the holder hanger and is used for realizing the shooting function of the holder; the first damping ball is arranged on one side, close to the head of the unmanned aerial vehicle body, of the holder hanger, one end of the first damping ball is assembled with the holder hanger, and the other end of the first damping ball is assembled with the inner wall of the head of the unmanned aerial vehicle body; and the second damping balls are arranged on two sides of the head of the unmanned aerial vehicle body, far away from the cradle head hanger, and are assembled on the cradle head hanger, and the other end of the cradle head hanger is assembled on the inner wall of the unmanned aerial vehicle body.

Furthermore, a first mounting part is arranged at the front end of the cradle head hanger on one side of the head of the unmanned aerial vehicle body, and the first damping ball is arranged between the first mounting part and the inner wall of the head of the unmanned aerial vehicle body; the cloud platform gallows is kept away from the rear end both sides of one side of unmanned aerial vehicle body head are provided with the second installation department, second shock attenuation ball is located the second installation department with between the unmanned aerial vehicle body inner wall.

Furthermore, the number of the first damping balls is one, the number of the second damping balls is two, and the number of the first damping balls and the number of the second damping balls are arranged in a triangular mode.

Further, the first damping ball includes: the fixing part, the first damping part and the first assembling part; the fixed part with the inside wall of unmanned aerial vehicle body head passes through the fix with screw, first assembly portion with cloud platform gallows fixed connection, first shock attenuation portion is connected the fixed part with first assembly portion.

Furthermore, the number of the first damping parts is two, and the number of the fixing parts is two; the first assembling part is arranged between the two first damping parts, and the two first damping parts are integrally formed respectively; the two fixing parts are respectively arranged on the two first damping parts and far away from one side of the first assembling part, and the two first damping parts are integrally formed.

Furthermore, waist-shaped through holes are formed in the two first damping parts.

Further, be provided with the joint on the first installation department, be provided with the joint hole on the first assembly portion, the joint hole be used for with the joint.

Further, the second damping ball includes: the clamping part, the second damping part and the second assembling part are arranged on the base; the clamping part is fixedly clamped with the inner side wall of the unmanned aerial vehicle body; the second assembling part is fixedly connected with the cradle head hanging bracket; the second damping portion is connected with the clamping portion and the second assembling portion.

Further, be provided with the installation piece on the inner wall of unmanned aerial vehicle body, be provided with U type groove on the installation piece, joint portion is T type piece, T type piece be used for with U type groove joint.

Further, the second mounting portion is mounted to the second mounting portion in a manner selected from the group consisting of: any one of bonding, clamping, screw fixing connection, splicing and riveting.

After the technical scheme is adopted, the utility model has the beneficial effects that: it is through setting up first shock attenuation ball and second shock attenuation ball between cloud platform gallows and unmanned aerial vehicle body to reduce the shake of unmanned aerial vehicle body to cloud platform assembly when shooing, guarantee the stability of shooting process, it is effectual to have the shock attenuation, shoots stably, structural design is ingenious advantage.

Drawings

In order to more clearly illustrate the embodiments of the present invention or the technical solutions in the prior art, the drawings used in the embodiments or the description of the prior art will be briefly described below, it is obvious that the drawings in the following description are only some embodiments of the present invention, and for those skilled in the art, other drawings can be obtained according to the drawings without creative efforts.

FIG. 1 is a schematic view of the overall structure of embodiment 1;

FIG. 2 is an enlarged view corresponding to detail A in FIG. 1;

FIG. 3 is a schematic structural view of the cradle, the first damping ball and the second damping ball after explosion in example 1;

fig. 4 is a schematic structural view of a cloud deck hanger, a first damping ball and a second damping ball in embodiment 2.

Description of reference numerals: 100. a cradle head hanger; 110. a first mounting portion; 111. a clamping head; 120. a second mounting portion; 200. a holder assembly; 300. a first damping ball; 301. a clamping groove; 302. a waist-shaped through hole; 310. a fixed part; 320. a first damper section; 330. a first fitting portion; 340. a plug-in part; 350. a third damper portion; 360. a connecting portion; 400. a second damping ball; 401. a waist-shaped groove; 410. a clamping part; 420. a second damper portion; 421. a boss; 430. a second fitting portion; 500. an unmanned aerial vehicle body; 501. a U-shaped groove; 510. clamping the column; 520. mounting blocks; 530. and (6) mounting the column.

Detailed Description

The present invention will be described in further detail with reference to the accompanying drawings.

The present embodiment is only for explaining the present invention, and it is not limited to the present invention, and those skilled in the art can make modifications of the present embodiment as necessary without making a contribution thereto after reading the present specification, but all are protected by patent laws within the scope of the claims of the present invention.

Example 1:

this embodiment relates to an unmanned aerial vehicle shock attenuation cloud platform, as shown in fig. 1-3, include: cloud platform gallows 100, cloud platform assembly 200, first shock attenuation ball 300 and second shock attenuation ball 400.

Specifically, cloud platform gallows 100 sets up in unmanned aerial vehicle body 500 and with unmanned aerial vehicle body 500 fixed mounting. The cradle head assembly 200 is fixedly installed on the cradle head hanger 100, and the cradle head assembly 200 is used for realizing the shooting function of the cradle head. First shock attenuation ball 300 sets up in cloud platform gallows 100 and is close to the head one side of unmanned aerial vehicle body 500. First shock attenuation ball 300 one end assembles with cloud platform gallows 100, the inner wall assembly of the other end and unmanned aerial vehicle body 500 head. Second shock attenuation ball 400 sets up in cloud platform gallows 100 and keeps away from the head both sides of unmanned aerial vehicle body 500. Second shock attenuation ball 400 cloud platform gallows 100 assembly, the other end and the assembly of the inner wall of unmanned aerial vehicle body 500. Obviously, this scheme is through setting up first shock attenuation ball 300 and second shock attenuation ball 400 between cloud platform gallows 100 and unmanned aerial vehicle body 500 to reduce the shake of unmanned aerial vehicle body 500 to cloud platform assembly 200 when shooing, guarantee the stability of shooting process.

Further, as shown in fig. 1 to 3, a first mounting portion 110 is disposed at a front end of the cradle head hanger 100 on one side of the head of the unmanned aerial vehicle body 500, and a first damping ball 300 is disposed between the first mounting portion 110 and an inner wall of the head of the unmanned aerial vehicle body 500. The rear end both sides of one side that unmanned aerial vehicle body 500 head was kept away from to cloud platform gallows 100 are provided with second installation department 120, and second shock attenuation ball 400 is located between second installation department 120 and the unmanned aerial vehicle body 500 inner wall.

Preferably, there are one first damping ball 300 and two second damping balls 400 symmetrically. One first damping ball 300 and two second damping balls 400 are arranged in a triangle.

Further, as shown in fig. 1 to 3, the first shock-absorbing ball 300 includes: a fixing part 310, a first damping part 320, and a first assembling part 330. Specifically, be provided with joint groove 301 on the fixed part 310, it is fixed through joint post 510 with the inside wall of unmanned aerial vehicle body 500 head. The first mounting portion 330 is fixedly connected to the cradle head suspension 100, and the first damping portion 320 connects the fixing portion 310 and the first mounting portion 330. First shock-absorbing part 320 is used for reducing or eliminating unmanned aerial vehicle body 500 earthquake to effectively reduce rocking of unmanned aerial vehicle body 500 and transmit cloud platform assembly 200.

Preferably, as shown in fig. 1 to 3, the first shock absorbing part 320 is provided in two, and the fixing part 310 is provided in two. The first assembling portion 330 is disposed between the two first shock absorbing portions 320, and the two first shock absorbing portions 320 are integrally formed. The two fixing portions 310 are respectively disposed on the two first shock absorbing portions 320 at a side away from the first assembling portion 330, and are integrally formed on the two first shock absorbing portions 320. Waist-shaped through holes 302 are formed in both of the first shock absorbing members 320. The first mounting portion 110 is provided with a clamping joint 111, the first assembling portion 330 is provided with a clamping hole, and the clamping hole is used for being clamped with the clamping joint 111. In the present embodiment, only one of the card connectors 111 is provided.

Further, as shown in fig. 1 to 3, the second shock-absorbing ball 400 includes: a clamping portion 410, a second shock absorbing portion 420, and a second assembling portion 430. Specifically, joint portion 410 is fixed with the inside wall joint of unmanned aerial vehicle body 500. The second fitting portion 430 is fixedly connected to the cradle head suspension 100. The second cushioning portion 420 connects the chucking portion 410 and the second mounting portion 430.

Further, as shown in fig. 1-3, an installation block 520 is arranged on the inner wall of the unmanned aerial vehicle body 500, a U-shaped groove 501 is arranged on the installation block 520, the clamping portion 410 is a T-shaped block, and the T-shaped block is used for being clamped with the U-shaped groove 501. The second fitting portion 430 is fitted to the second mounting portion 120 in a manner selected from the group consisting of: any one of bonding, clamping, screw fixing connection, splicing and riveting.

In this embodiment, the second mounting portion 430 is snap-fitted to the second mounting portion 120. The second shock absorbing portion 420 is also provided with a kidney-shaped hole, and a boss 421 is provided on the inner wall of the kidney-shaped hole near the second assembling portion 430, and the boss 421 has a trapezoidal cross section and extends toward the side where the clamping portion 410 is located. When deformation takes place for the waist type hole receives the impact, boss 421 is used for with the inner wall butt of waist type hole opposite side to effectively prevent the excessive deformation of second shock attenuation portion 420, guarantee second shock attenuation ball 400's life.

Example 2:

the difference between this embodiment and embodiment 1 mainly lies in that, in this embodiment, as shown in fig. 4, the inner wall of the unmanned aerial vehicle body 500 is provided with a mounting post 530, and the first damping ball 300 includes: a socket part 340, a third damping part 350, and a connection part 360. The erection column 530 sets up at the unmanned aerial vehicle front end, and is the symmetry and is provided with two. The two inserting parts 340 are arranged, and the two inserting parts 340 are arranged on two sides and are respectively inserted and assembled with the mounting column 530. The two ends of the connecting portion 360 are respectively assembled with the two insertion portions 340, and three clamping holes are formed in the connecting portion 360. Two third vibration attenuating portions 350 are provided. And are all integrally formed with the connecting portion 360. The third damping portion 350 extends to a side away from the cradle head suspension bracket 100, and the two third damping portions 350 and the three clamping holes are alternately arranged. Correspondingly, the three card connectors 111 are arranged on the card connecting portion 410, and the three card connecting holes are used for being connected with the three card connectors 111 in a clamping manner.

The above description is only for the purpose of illustrating the technical solutions of the present invention and not for the purpose of limiting the same, and other modifications or equivalent substitutions made by those skilled in the art to the technical solutions of the present invention should be covered by the claims of the present invention without departing from the spirit and scope of the technical solutions of the present invention.

Claims

1. The utility model provides an unmanned aerial vehicle shock attenuation cloud platform which characterized in that includes:

the cradle head hanging bracket (100), the cradle head hanging bracket (100) is arranged in the unmanned aerial vehicle body (500) and is fixedly assembled with the unmanned aerial vehicle;

the holder assembly (200), the holder assembly (200) is fixedly installed on the holder hanger (100), and the holder assembly (200) is used for realizing the shooting function of the holder;

the first damping ball (300) is arranged on one side, close to the head of the unmanned aerial vehicle body (500), of the cradle head hanger (100), and one end of the first damping ball (300) is assembled with the cradle head hanger (100) while the other end of the first damping ball is assembled with the inner wall of the head of the unmanned aerial vehicle body (500); and the number of the first and second groups,

second shock attenuation ball (400), second shock attenuation ball (400) set up in cloud platform gallows (100) are kept away from the head both sides of unmanned aerial vehicle body (500), second shock attenuation ball (400) cloud platform gallows (100) assembly, the other end with the inner wall assembly of unmanned aerial vehicle body (500).

2. The unmanned aerial vehicle shock attenuation cloud platform of claim 1, characterized in that, the cloud platform gallows (100) is provided with first installation department (110) at the front end of one side of the unmanned aerial vehicle body (500) head, the first shock attenuation ball (300) is provided between the first installation department (110) and the inner wall of the unmanned aerial vehicle body (500) head; cloud platform gallows (100) are kept away from the rear end both sides of one side of unmanned aerial vehicle body (500) head are provided with second installation department (120), second shock attenuation ball (400) are located second installation department (120) with between unmanned aerial vehicle body (500) inner wall.

3. An unmanned aerial vehicle shock attenuation cloud platform of claim 2, characterized in that, there is one first shock attenuation ball (300) that is provided with, and the second shock attenuation ball (400) is provided with two symmetrically, and one first shock attenuation ball (300) and two second shock attenuation balls (400) are arranged in a triangle.

4. An unmanned aerial vehicle shock absorbing pan/tilt head according to claim 3, wherein the first shock absorbing ball (300) comprises: a fixing part (310), a first damper part (320), and a first mounting part (330); the fixing part (310) with the inside wall of unmanned aerial vehicle body (500) head passes through the fix with screw, first assembly part (330) with cloud platform gallows (100) fixed connection, first shock attenuation portion (320) are connected fixed part (310) with first assembly part (330).

5. The unmanned aerial vehicle shock attenuation cloud platform of claim 4, characterized in that, the first shock attenuation portion (320) is provided with two, the fixed part (310) is provided with two; the first assembling part (330) is arranged between the two first shock absorption parts (320), and the two first shock absorption parts (320) are integrally formed; the two fixing parts (310) are respectively arranged on one sides, far away from the first assembling part (330), of the two first shock absorption parts (320), and are integrally formed on the two first shock absorption parts (320).

6. An unmanned aerial vehicle shock attenuation cloud platform of claim 5, characterized in that, be provided with waist type through-hole (302) on two first shock attenuation portions (320).

7. The unmanned aerial vehicle shock attenuation cloud platform of claim 5, characterized in that, be provided with joint (111) on first installation department (110), be provided with the joint hole on first assembly department (330), the joint hole be used for with joint (111) joint.

8. An unmanned aerial vehicle shock absorbing pan and tilt head according to claim 7, wherein the second shock absorbing ball (400) comprises: a clamping part (410), a second damping part (420) and a second assembling part (430); the clamping part (410) is fixedly clamped with the inner side wall of the unmanned aerial vehicle body (500); the second assembling part (430) is fixedly connected with the cradle head hanger (100); the second shock absorbing part (420) connects the clamping part (410) and the second assembling part (430).

9. The unmanned aerial vehicle shock attenuation cloud platform of claim 8, characterized in that, be provided with installation piece (520) on the inner wall of unmanned aerial vehicle body (500), be provided with U type groove (501) on installation piece (520), joint portion (410) is T type piece, T type piece be used for with U type groove (501) joint.

10. The unmanned aerial vehicle shock attenuation cloud platform of claim 9, characterized in that, the mounting means between second installation department (430) and the second installation department (120) is selected from: any one of bonding, clamping, screw fixing connection, splicing and riveting.