直升机技术2024,Issue(3) :60-63,68.

直升机桨叶扭转角测量方法

Measurement Method of Helicopter Blade Torsion Angle

张俊愿 虞路长
直升机技术2024,Issue(3) :60-63,68.

直升机桨叶扭转角测量方法

Measurement Method of Helicopter Blade Torsion Angle

张俊愿 1虞路长1
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作者信息

  • 1. 中国直升机设计研究所,江西 景德镇 333001
  • 折叠

摘要

针对直升机桨叶扭转角测量方法进行了深入研究,包括技术背景、传统测量方法介绍、测量方法改进和试验结果分析等;提出了基于数字图像相关法的直升机桨叶扭转角测量方法,克服了传统激光三角法无法精确跟踪桨叶测量剖面上变形前后同一点的位移等各种弊端.

Abstract

This paper aimed at the further research on measurement method of helicopter blade tor-sional angle,including technical background,traditional measurement methods and improvement,a-nalysis of test results and so on.Proposed measurement method for helicopter blade torsion angle which based digital image correlation method.It Overcame the disadvantages that the traditional la-ser triangulation method could not accurately track the displacement of the same point before and af-ter the deformation on the blade measurement section.

关键词

直升机/桨叶/扭转角/数字图像相关/测量方法

Key words

helicopter/blade/torsional angle/digital image correlation/measurement method

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出版年

2024
直升机技术
江西省国防科工办

直升机技术

影响因子:0.12
ISSN:1673-1220
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