Flight control assembly and unmanned aerial vehicle

A technology for unmanned aerial vehicles and components, applied in the field of aircraft, can solve the problems of high difficulty in assembly, high requirements on the softness and hardness of shock-absorbing materials, damping and other parameters, and achieve the effect of easy assembly

Active Publication Date: 2016-04-20
SZ DJI TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Due to the relatively small self-weight of the inertial measurement module, the requirements for parameters such as softness, hardness and damping of the shock-absorbing material of the inertial measurement module are relat

Method used

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  • Flight control assembly and unmanned aerial vehicle
  • Flight control assembly and unmanned aerial vehicle
  • Flight control assembly and unmanned aerial vehicle

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[0034] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings in the embodiments of the present invention. Obviously, the described embodiments are only a part of the embodiments of the present invention, rather than all the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present invention.

[0035] It should be noted that when a component is said to be "fixed to" another component, it can be directly on the other component or a central component may also exist. When a component is considered to be "connected" to another component, it can be directly connected to another component or there may be a centered component at the same time. When a component is considered to be "installed on" another component, it can be directly in...

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Abstract

The invention provides a flight control assembly. The flight control assembly comprises a flight control board, and further comprises damping structures connected to the flight control assembly; the flight control assembly is connected with a supporting body through the damping structures; the damping structures are used for damping vibration of the flight control assembly from the supporting body to realize overall damping of the flight control assembly. The invention further relates to an unmanned aerial vehicle employing the flight control assembly.

Description

technical field [0001] The invention relates to the field of aircraft, in particular to a flight control component and an unmanned aircraft. Background technique [0002] The inertial measurement module of the flight control component needs to take shock-absorbing measures to reduce the impact of external vibrations on the inertial measurement module, and often when the inertial measurement module is assembled on the circuit board of the flight control component Provide shock-absorbing material between. Due to the relatively small self-weight of the inertial measurement module, the requirements for parameters such as softness, hardness and damping of the shock-absorbing material of the inertial measurement module are relatively high; and because the inertial measurement module and the circuit need to be considered during assembly The assembly accuracy requirements between the plate and the shock absorbing material make the assembly difficult. Contents of the invention ...

Claims

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Application Information

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IPC IPC(8): G01C21/18
CPCG01C21/18
Inventor 冯建刚唐尹潘国秀石仁利
Owner SZ DJI TECH CO LTD
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