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Head, camera component and unmanned aerial vehicle

A technology of gimbal and components, which is applied in the field of aircraft, can solve the problems of poor vibration reduction effect of two-axis gimbal, and achieve the effect of eliminating vibration and improving vibration reduction effect

Pending Publication Date: 2018-06-01
SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

General gimbals have three-axis anti-shake, but some very small aircraft can only be equipped with two-axis anti-shake gimbals
However, the current two-axis gimbal has poor vibration reduction effect

Method used

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  • Head, camera component and unmanned aerial vehicle
  • Head, camera component and unmanned aerial vehicle
  • Head, camera component and unmanned aerial vehicle

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Experimental program
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Embodiment Construction

[0060] In order to facilitate the understanding of the present invention, the present invention will be described in more detail below in conjunction with the accompanying drawings and specific embodiments. It should be noted that when an element is said to be "fixed" to another element, it may be directly on the other element, or there may be one or more intervening elements therebetween. When an element is referred to as being "connected to" another element, it can be directly connected to the other element or one or more intervening elements may be present therebetween. The terms "vertical", "horizontal", "left", "right", "inner", "outer" and similar expressions are used in this specification for the purpose of description only.

[0061] Unless otherwise defined, all technical and scientific terms used in this specification have the same meaning as commonly understood by one of ordinary skill in the technical field of the invention. The terms used in the description of the...

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Abstract

The invention relates to the field of aerial vehicles, and provides a head, a camera component and an unmanned aerial vehicle. The head comprises a first motor, a second motor, a lens cone, a first damping component and a second damping component, wherein the first motor is used for driving a camera device to rotate around a first rotation axis; the first motor is installed in the lens cone; the second motor is installed in the lens cone and is used for driving the lens cone; the first motor and the camera device rotate around a second rotation axis; the first rotation axis and the second rotation axis are vertical; the first damping component is installed in the second motor; the second damping component is installed in the lens cone; the first damping component and the second damping component are arranged on two opposite sides of the lens cone along the second rotation axis. According to the embodiment of the invention, the first damping component and the second damping component can be cooperated to eliminate vibration transferred to the head by the unmanned aerial vehicle, and therefore, the damping effect of the head is improved.

Description

【Technical field】 [0001] The invention relates to the field of aircraft, in particular to a platform, a camera assembly with the camera assembly and an unmanned aerial vehicle with the camera assembly. 【Background technique】 [0002] Unmanned aerial vehicle, referred to as unmanned aerial vehicle (UAV), is a new concept equipment in rapid development, which has the advantages of flexible maneuvering, quick response, unmanned driving, and low operation requirements. The unmanned aerial vehicle is equipped with various types of sensors or camera devices through the gimbal, which can realize real-time image transmission and detection of high-risk areas. It is a powerful supplement to satellite remote sensing and traditional aerial remote sensing. [0003] In order to be convenient for users to carry, the miniaturization of unmanned aerial vehicles is a development trend. Miniaturization also needs to retain the functions of unmanned aerial vehicles. The gimbal is particularly...

Claims

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Application Information

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IPC IPC(8): B64D47/08B64C27/08
CPCB64U2101/30B64U30/20B64U50/19B64U20/87B64U10/14
Inventor 余春
Owner SHENZHEN AUTEL INTELLIGENT AVIATION TECH CO LTD