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应变解耦增敏式FBG温度传感器的设计与应用 被引量:4
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作者 李五一 闫楚良 刘力宏 《振动.测试与诊断》 EI CSCD 北大核心 2020年第5期916-922,1023,共8页
为了实现飞机载荷谱飞行实测中对温度参数的精确测量,设计了一种应变解耦增敏式光纤光栅(fiber Bragg grating,简称FBG)温度传感器。通过力学建模分析设计新的传感器结构,对传感器的光纤光栅进行增敏处理,选取铝7075-T6为基底进行全覆... 为了实现飞机载荷谱飞行实测中对温度参数的精确测量,设计了一种应变解耦增敏式光纤光栅(fiber Bragg grating,简称FBG)温度传感器。通过力学建模分析设计新的传感器结构,对传感器的光纤光栅进行增敏处理,选取铝7075-T6为基底进行全覆盖式封装,提出光纤光栅封装位置与结构件之间无直接接触方式,排除结构形变对温度传感器带来的影响。经标定测试传感器温度灵敏速度为40.4pm/℃,是普通光纤光栅的4倍。搭建实验系统进行其性能探究以及在拉伸实验机上进行解耦特性验证,拉伸实验件的变形对该温度传感器没有影响,与理论分析相符,最终将传感器贴于飞机座舱中进行实际工程应用。实验表明,传感器测得的温度差最大不超过±1℃,表明设计的传感器可以用于实际温度测量中,满足在飞机载荷谱飞行实测中温度参数精确测量的需求。 展开更多
关键词 飞行实测 应变解耦 增敏 光纤光栅 温度传感器
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Application of ultrasonic fatigue technology in very-high-cycle fatigue testing of aviation gas turbine engine blade materials:A review
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作者 ZHAO JiuCheng WAN Jie +2 位作者 ZHANG ShiZhong yan chuliang ZHAO HongWei 《Science China(Technological Sciences)》 SCIE EI CAS CSCD 2024年第5期1317-1363,共47页
The need for very-high-cycle fatigue(VHCF)testing up to 1010cycles of aviation gas turbine engine blade materials under combined mechanical loads and complex environments has encouraged the development of VHCF testing... The need for very-high-cycle fatigue(VHCF)testing up to 1010cycles of aviation gas turbine engine blade materials under combined mechanical loads and complex environments has encouraged the development of VHCF testing instrumentation and technology.This article begins with a comprehensive review of the existing available techniques that enable VHCF testing.Recent advances in ultrasonic fatigue testing(UFT)techniques are highlighted,containing their new capabilities and methods for single load,multiaxial load,variable amplitude fatigue,and combined cycle fatigue.New techniques for conducting UFT in high-temperature,humid environments,and corrosive environments are summarized.These developments in mechanical loading and environmental building techniques provide the possibility of laboratory construction for real service conditions of blade materials.New techniques that can be used for in situ monitoring of VHCF damage are summarized.Key issues in the UFT field are presented,and countermeasures are collated.Finally,the existing problems and future trends in the field are briefly described. 展开更多
关键词 aviation gas turbine engine blade materials ultrasonic fatigue very-high-cycle fatigue high-temperature complex stress in situ testing
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Theory of Economic Life Prediction and Reliability Assessment of Aircraft Structures 被引量:35
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作者 yan chuliang LIU Kege 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2011年第2期164-170,共7页
关键词 life prediction model of economic life fatigue scatter factor full scale test RELIABILITY
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