Fatigue testing of a composite propeller blade using fiber-optic strain sensors

被引:31
|
作者
Zetterlind, VE [1 ]
Watkins, SE
Spoltman, MW
机构
[1] USAF, Res Labs, Munit Directorate, Eglin AFB, FL 32542 USA
[2] Univ Missouri, Dept Elect & Comp Engn, Rolla, MO 65409 USA
[3] Hartzell Propeller Co, Piqua, OH 45356 USA
关键词
aerospace systems; fatigue testing; fiber-optic strain sensors; smart structures;
D O I
10.1109/JSEN.2003.815795
中图分类号
TM [电工技术]; TN [电子技术、通信技术];
学科分类号
0808 ; 0809 ;
摘要
The performance of surface-mounted extrinsic Fabry-Perot interferometric (EFPI) sensors during a seventeen-million-cycle, high-strain fatigue test is reported. Fiber-optic strain measurements did not degrade during the test. The sensors were applied to a composite propeller blade subject to a constant axial load and a cyclic bending load. Strain measurements were taken at four blade locations using two types of EFPI sensors and co-located electrical resistance strain gages. Static and dynamic strain measurements were taken daily during the 65 days of this standard propeller-blade test. All fiber-optic sensors survived the fatigue test while most of the resistive gages failed. The suitability of fiber-optic monitoring for fatigue testing and other high-cycle monitoring is demonstrated.
引用
收藏
页码:393 / 399
页数:7
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