Helicopter balancing apparatus mounted on tail wing rod

A balancing device and helicopter technology, applied in aircraft parts, aircraft control, aircraft stability and other directions, can solve the problems of helicopter loss of balance and uneven load, and achieve the effect of easy balance adjustment

Inactive Publication Date: 2017-05-31
王丽萍
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0003] The object of the present invention is to provide a helicopter balance device installed on the tail bar, aiming to solve the

Method used

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  • Helicopter balancing apparatus mounted on tail wing rod
  • Helicopter balancing apparatus mounted on tail wing rod
  • Helicopter balancing apparatus mounted on tail wing rod

Examples

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Embodiment Construction

[0012] In order to make the object, technical solution and advantages of the present invention clearer, the present invention will be further described in detail below in conjunction with the accompanying drawings.

[0013] see figure 1 As shown in -3, a helicopter balance device installed on the tail bar includes two clamping units that are movably connected by a hinge 7, and one clamping unit includes a clamping part 1 and a handle 4 connected to the clamping part The other clamping unit includes a clamping part 2 and a handle 5 connected to the clamping part; a compression spring 6 is arranged between the two handles 4, 5; the clamping parts 1, 2 of the clamping unit A circular cavity 3 is formed after relative fastening, and the circular cavity 3 is clamped on the tail bar of the helicopter.

[0014] Wherein, the clamping parts 1 and 2 are arc-shaped, and the two clamping parts 1 and 2 are relatively buckled together to form a circular cavity 3 for the helicopter tail rod...

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PUM

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Abstract

The invention discloses a helicopter balancing apparatus mounted on a tail wing rod. The helicopter balancing apparatus includes two clamping units which are movably connected. Each clamping unit includes a clamping part and a grab handle connected to the clamping part. A compressed spring is arranged between the two grab handles. The clamping parts of the two clamping unit are oppositely buckled and clamped on the tail wing rod of a helicopter. The helicopter balancing apparatus is mounted on the tail wing rod of the helicopter, so that by adjusting the position of the apparatus on the tail wing rod, balance adjustment on an on-load helicopter can be achieved easily.

Description

technical field [0001] The invention relates to a helicopter balancing device, which is used for being installed on the tail bar of the helicopter and performing balance adjustment on the helicopter after the helicopter is loaded. Background technique [0002] After the unmanned helicopter is loaded, the uneven load often causes the helicopter to lose its balance during flight, seriously affecting the normal function of the helicopter, and sometimes even more serious problems. Contents of the invention [0003] The purpose of the present invention is to provide a helicopter balance device installed on the tail bar, aiming to solve the problem that the unmanned helicopter loses balance during flight due to uneven load after the unmanned helicopter is loaded. [0004] To achieve the above object, the technical scheme adopted in the present invention is as follows: [0005] A helicopter balance device installed on the tail bar, comprising two movably connected clamping units...

Claims

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Application Information

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IPC IPC(8): B64C5/08
CPCB64C5/08
Inventor 王丽萍
Owner 王丽萍
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