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Method and device for measuring longitudinal center of gravity of a coaxial helicopter

A coaxial helicopter and center of gravity technology, which is applied in the direction of measuring devices, machine/structural component testing, static/dynamic balance testing, etc., can solve problems affecting the horizontal center of gravity measurement results, measurement center of gravity error, and complicated preparations, etc. Achieve the effect of saving complex work, reducing large errors and reducing workload

Active Publication Date: 2022-07-19
深圳联合飞机科技有限公司
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  • Abstract
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Problems solved by technology

[0007] The purpose of the embodiments of the present invention is to provide a method and device for measuring the longitudinal center of gravity of a coaxial helicopter, which is used to solve the complicated and laborious preparation work before measuring the center of gravity in the prior art, and will affect the measurement result of the horizontal center of gravity, resulting in measurement There is a technical problem with a large error in the center of gravity

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  • Method and device for measuring longitudinal center of gravity of a coaxial helicopter
  • Method and device for measuring longitudinal center of gravity of a coaxial helicopter
  • Method and device for measuring longitudinal center of gravity of a coaxial helicopter

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Embodiment Construction

[0058] The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to 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, but not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by those of ordinary skill in the art without creative efforts shall fall within the protection scope of the present invention.

[0059] In view of the fact that the preparation work before measuring the center of gravity in the prior art is complicated, time-consuming and laborious, and the measurement error will be magnified several times on the basis of the measurement error of the horizontal center of gravity, resulting in a large error in the measured longitudinal center of gravity, the embodiment of the present invention provides a The method and device for...

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Abstract

Embodiments of the present invention provide a method and device for measuring the longitudinal center of gravity of a coaxial helicopter, wherein the method can directly use a horizontal center of gravity measurement tool or three or more platform scales to measure the horizontal center of gravity, so as to calculate the longitudinal center of the coaxial helicopter. Compared with the prior art, the center of gravity does not require a wedge-shaped spacer, which saves the complicated work of installing and leveling the wedge-shaped spacer, and reduces the workload of preparation. Moreover, based on the relatively accurate horizontal center of gravity, the obtained longitudinal center of gravity is relatively accurate. The further determined longitudinal center of gravity of the coaxial helicopter is more accurate. In this way, on the basis that the horizontal center of gravity is relatively accurate, the accuracy of the measured longitudinal center of gravity is improved, and the larger error that may be introduced by the longitudinal center of gravity compared with the prior art is reduced.

Description

technical field [0001] The invention relates to the technical field of longitudinal center of gravity measurement, in particular to a method and device for measuring the longitudinal center of gravity of a coaxial helicopter. Background technique [0002] In the field of helicopter flight performance calculation and flight control design, data such as the center of gravity of the helicopter are often required. These data play a key role in the accuracy of helicopter flight performance calculation and the correctness of flight control design. [0003] At present, the center of gravity of the coaxial helicopter in the helicopter can generally be measured by the following steps: [0004] Put the coaxial helicopter on the horizontal center of gravity measurement tool, put the landing gear of the coaxial helicopter on the four known pressure sensors at the relative positions of the horizontal center of gravity measurement tool, and read the value of each pressure sensor. Using t...

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): G01M1/12
CPCG01M1/125
Inventor 顾海贝李进峰左秀韩述宏彭俊树李闯
Owner 深圳联合飞机科技有限公司
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