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Device for arm folding and turning of multi-rotorcraft

A technology of a rotating device and a rotorcraft, which is applied in the directions of rotorcraft, motor vehicles, transportation and packaging, etc., can solve the problems of unfavorable straight-line acceleration flight and emergency deceleration, reduce the reliability of use, reduce work efficiency, etc. Improved reliability and reduced footprint

Inactive Publication Date: 2020-06-19
王会涛
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] With the improvement of people's quality of life and the development of science and technology, the field of unmanned aerial vehicles represented by multi-rotor aircraft is developing rapidly. , which makes it occupy a particularly large area, which is not suitable for fast and convenient transportation, which reduces work efficiency. The extended arm also reduces the reliability of use due to the bumpy transportation. The fixed arm is not conducive to linear acceleration flight and emergency response. slow down

Method used

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  • Device for arm folding and turning of multi-rotorcraft
  • Device for arm folding and turning of multi-rotorcraft
  • Device for arm folding and turning of multi-rotorcraft

Examples

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Embodiment Construction

[0024] A folding and rotating device for a rotorcraft is composed of a telescopic assembly 1, a motor plate assembly 2, a locking assembly 3, a main control assembly 4, and a rotating assembly 5. The motor plate assembly 2 is connected above the outer side of the telescopic assembly 1, and The inner side of the telescopic assembly 1 and the outer side of the locking assembly 3 are parallel and connected. The locking assembly 3 is fixed above the rotating assembly 5, the main control assembly 4 is fixed above the rotorcraft bottom plate, and the base of the rotating assembly 5 is fixed above the rotorcraft bottom plate, and The main control assembly 4 and the rotating assembly 5 are in a parallel relationship on the rotorcraft floor.

[0025] Further, the telescopic assembly 1 is composed of a motor-fixed rotating shaft 101, a telescopic arm 102, a telescopic rotatable shaft 103, a telescopic arm 104, a telescopic rotatable shaft 105, and a telescopic matching surface 106. One end...

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PUM

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Abstract

The invention discloses a device for arm folding and turning of a rotorcraft and belongs to the field of structural design of an unmanned rotorcraft. The device is composed of a telescopic assembly, amotor plate assembly, a locking assembly, a main control assembly and a rotating assembly, wherein the motor plate assembly is connected with an upper portion of an outer side of the telescopic assembly, an inner side of the telescopic assembly and an outer side of the locking assembly are parallel and connected together, the locking assembly is fixed above the rotating assembly, the main controlassembly is fixed above a rotorcraft bottom plate, a base of the rotating assembly is fixed above the rotorcraft bottom plate, and the main control assembly and the rotating assembly are parallel onthe rotorcraft bottom plate. The device is advantaged in that the length of vehicle arms is reduced and extended through stretching, transportation and carrying are facilitated in a reduced state, problems that the rotorcraft is large in unfolding area and inconvenient to transport and carry are solved, accelerating and decelerating effects are achieved through rotation of the vehicle arms, and problems of accelerating and decelerating in a short time and saving the electric quantity are solved.

Description

Technical field [0001] The invention relates to a device for folding the arms of a multi-rotor unmanned aerial vehicle and changing the flight mode. Specifically, it reduces the space occupied by the rotorcraft by changing the arms, and changes the flight mode by changing the angle of the arms. The field of structural design of human rotorcraft. Background technique [0002] With the improvement of people’s quality of life and the development of science and technology, the field of unmanned aerial vehicles represented by multi-rotor aircraft is developing rapidly. The application fields also involve aerial photography, electric cruise, pesticide spraying and other fields, because of the fixed shape mechanism of multi-rotor aircraft. , It occupies a particularly large area and is not suitable for fast and convenient transportation, which reduces work efficiency. The extended arm also reduces the reliability of use due to the bumps in transportation. The fixed arm is not conducive ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/30B64C27/08B64D47/08
CPCB64C1/30B64C27/08B64D47/08B64U2101/00B64U30/20B64U50/19B64U10/10
Inventor 王会涛徐健
Owner 王会涛
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