空军工程大学学报2024,Vol.25Issue(1) :47-51.DOI:10.3969/j.issn.2097-1915.2024.01.007

考虑温度影响的复合材料结构载荷测量方法

A Load Measurement Method for Composite Structure Considering the Effect of Temperature

李文龙 李俊 刘敬礼 唐宁
空军工程大学学报2024,Vol.25Issue(1) :47-51.DOI:10.3969/j.issn.2097-1915.2024.01.007

考虑温度影响的复合材料结构载荷测量方法

A Load Measurement Method for Composite Structure Considering the Effect of Temperature

李文龙 1李俊 1刘敬礼 1唐宁1
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作者信息

  • 1. 中国飞行试验研究院飞机所,西安,710089
  • 折叠

摘要

针对温度环境会影响应变法测量复合材料结构载荷精度的问题,提出了一种考虑温度影响的复合材料结构载荷测量方法.以某型飞机碳纤维复合材料平尾盒段结构剪力测量为例,首先,设计并完成了不同温度环境下的载荷校准试验;其次,采用多元线性回归法建立了常温下的复合材料结构载荷测量模型,并在不同温度条件下进行了载荷模型检验;最后,考虑温度影响对常温下的载荷模型进行了修正与验证.结果表明,文中方法具有可行性和较高的准确性.

Abstract

Aimed at the problem that temperature affects the load measurement accuracy of composite structure by the strain method,a load measurement method is proposed in consideration of the effect of temperature on composite structure.In this paper,taking shear force measurement of carbon fiber com-posite in horizontal tail box at a certain type of aircraft as an example,tests are to be made.Firstly,the load calibration tests under different temperature environments are designed and completed.Secondly,the multiple linear regression method is used to establish a load measurement model at room temperature,and the load model is checked under different temperature conditions.Finally,the load model at room temper-ature is modified and verified in consideration of the effect of temperature.The results show that the method in this paper is feasible and the result is accurate.

关键词

复合材料/载荷测量/温度影响/载荷校准试验

Key words

composite/load measurement/temperature effect/load calibration test

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基金项目

航空工业联合基金(6141B05030103)

出版年

2024
空军工程大学学报
空军工程大学科研部

空军工程大学学报

CSTPCD北大核心
影响因子:0.55
ISSN:2097-1915
参考文献量3
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