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Unmanned aerial vehicle camera damping device

A technology of a shock absorption device and a camera, which is applied in the field of shock absorption devices, can solve problems such as complex mechanisms, and achieve the effect of accurate shock absorption

Inactive Publication Date: 2018-11-09
芜湖翼讯飞行智能装备有限公司
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0004] Although the above solution connects the casing through the bracket and various functional components that need shock absorption through the silicone sleeve, the impact of external airflow and motor vibration on the aircraft during operation is reduced, but the mechanism is complicated and cannot be directly and clearly solved. vibration problem

Method used

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  • Unmanned aerial vehicle camera damping device
  • Unmanned aerial vehicle camera damping device

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specific Embodiment approach

[0017] see figure 1 , a camera damping device on an unmanned aerial vehicle, comprising a fuselage or a body 1, a bracket 2, a stage 3, a tripod bracket 5, a tripod 6 and a camera damping device, one end of the bracket 2 is fixedly connected to the aircraft platform 1. The other end is fixedly connected to the stage 3. One end of the tripod bracket 5 is fixed on the lower end of the stage 3, and the other end is fixed on the tripod 6. The shock absorbing device for the camera includes a spring 40 and a damper 41 , the camera installation platform 42 and the camera 4, the spring 4 is coaxially connected with the damper 41, the upper end of the camera installation platform 42 is fixedly connected with the damper 41, and the upper end surface of the camera installation platform 42 is contacted and connected with the spring 40, so The lower surface of the camera installation platform 42 is connected to the camera 4, the tripod bracket 5 is made of elastic material, the camera 4 is...

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Abstract

The invention discloses an unmanned aerial vehicle camera damping device. The unmanned aerial vehicle camera damping device includes a vehicle frame or vehicle body, supports, an objective table, footstand brackets, a foot stand and the camera damping device; one ends of the supports are fixedly connected to an aircraft platform, and the other ends of the supports are connected to the objective table; one ends of the foot stand brackets are fixed on the lower end of the objective table, and the other ends of the foot stand brackets are fixed on a foot stand; the camera damping device includessprings, dampers, a camera installation platform and a camera; the springs and the dampers are in coaxial connection; the upper end of the camera installation platform is fixedly connected to the dampers; the upper end face of the camera installation platform is connected to the springs in a contact manner; and the lower end face of the camera installation platform is connected to the camera. Thecamera is not liable to suffer vibration caused by the rotation of rotors during flying through a simple and exquisite structure, and accurate damping on the parts needing shock absorption can be realized.

Description

technical field [0001] The invention relates to a shock absorbing device, in particular to a camera shock absorbing device on an unmanned aerial vehicle. Background technique [0002] When the aircraft is flying, due to its own and airflow, the camera installed at the bottom of the aircraft will shake, resulting in poor picture quality captured by the camera. However, the current technology has revealed the effect of camera shock absorption, and it is also very susceptible to the influence of airflow. [0003] In order to solve the above problems, the Chinese application number is 201620687336.4 utility model patent, and the utility model proposes an aircraft. The aircraft described in the utility model includes a housing, and various functional components located in the housing, wherein a bracket connected to the housing is provided in the housing, and the functional components requiring shock absorption are fixedly installed on the bracket; The bracket is provided with s...

Claims

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Application Information

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IPC IPC(8): B64D47/08
CPCB64D47/08B64U2101/30B64U10/10
Inventor 赵雪冬孙晓伟金晶
Owner 芜湖翼讯飞行智能装备有限公司
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