Arm folding device of multi-axial air vehicle

A multi-axis aircraft and folding device technology, which is applied to aircraft, aircraft control, aircraft parts, etc., can solve the problems of increasing the weight of the aircraft, the workload of maintenance personnel, and the inconvenient operation, etc., and achieve novel structure, fast and convenient folding, saving effect of space

Inactive Publication Date: 2016-05-04
NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Although folding parts for aircraft arms folding have appeared on the market, this type of aircraft folding parts is not easy to operate

Method used

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  • Arm folding device of multi-axial air vehicle
  • Arm folding device of multi-axial air vehicle
  • Arm folding device of multi-axial air vehicle

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Embodiment Construction

[0034] Below in conjunction with accompanying drawing, technical scheme of the present invention is described in further detail:

[0035] Such as Figure 1 to Figure 5 As shown, the present invention discloses an arm folding device for a multi-axis aircraft, comprising a first frame, a second frame, a fixed shaft, a rotating shaft, a telescopic module and an arm tube;

[0036] The arm pipe includes an arm connection sleeve, a first clip and a second clip;

[0037] One end of the arm connection sleeve is open and the other end is closed, which is used to fix the arm of the multi-axis aircraft;

[0038] The first clip and the second clip are distributed in parallel in a sheet shape, and one end is fixedly connected to the closed end of the connecting sleeve of the machine arm, and the other end is provided with two vertically symmetrical openings connected to the machine arm. Circular grooves facing away from the socket opening;

[0039] Both the first clip and the second cli...

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Abstract

The invention discloses an arm folding device of a multi-axial air vehicle. The arm folding device comprises a first frame, a second frame, a fixing shaft, a rotating shaft, a telescopic module and an arm tube. The arm tube is connected with the first frame and the second frame through the rotating shaft, and the telescopic module is installed between the two frames and fixed through the fixing shaft. When an arm is folded or unfolded, the telescopic module plays a role in clamping round grooves in the arm tube. An arm folding part is connected with a vehicle body and the arm, limiting is achieved through the telescopic module and the grooves in the arm tube, and then folding of the arm is achieved. After the arm folding device is installed on the vehicle body of the air vehicle, no auxiliary tool is needed in the folding process; the arm folding device is simple and reliable in structure and convenient to use and solves the problems that a multi-axial air vehicle is difficult to carry as arms of the multi-axial air vehicle can not be folded, and auxiliary tools are needed when folding is carried out through an existing folding device.

Description

technical field [0001] The invention relates to the technical field of aircraft design, in particular to an arm folding device of a multi-axis aircraft. Background technique [0002] With the wide application of multi-rotor aircraft in civil and military applications, people have put forward requirements for the portability of aircraft. Although folding parts for folding aircraft arms have appeared on the market, such folding parts for aircraft are not easy to operate and require auxiliary tools, which increases the weight of the aircraft and the workload of maintenance personnel to a certain extent. Contents of the invention [0003] The technical problem to be solved by the present invention is to provide an arm folding device for a multi-axis aircraft in view of the defects involved in the background technology. [0004] The present invention adopts the following technical solutions for solving the problems of the technologies described above: [0005] An arm folding ...

Claims

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Application Information

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IPC IPC(8): B64C27/08B64C1/30
CPCB64C1/30B64C27/08
Inventor 陈辉陈亚扣陈岩叶星
Owner NANJING UNIV OF AERONAUTICS & ASTRONAUTICS
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