Journal of Aerospace System Engineering (항공우주시스템공학회지)
- Volume 8 Issue 3
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- Pages.6-13
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- 2014
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- 1976-6300(pISSN)
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- 2508-7150(eISSN)
DOI QR Code
Derivation of Numerical Equivalent Model of Vibration Isolator using Pseudoelastic SMA Mesh Washer
의탄성 형상기억합금 메쉬 와셔가 적용된 수동형 진동절연기의 수학적 등가모델 도출
- Kwon, Sung-Cheol (Dept. of Aerospace Engineering, Chosun University) ;
- Jeon, Su-Hyeon (Dept. of Aerospace Engineering, Chosun University) ;
- Oh, Hyun-Ung (Dept. of Aerospace Engineering, Chosun University)
- Received : 2014.09.18
- Accepted : 2014.09.27
- Published : 2014.09.30
Abstract
A passive launch and on-orbit vibration isolator using SMA(Shape Memory Alloy) washer for both the structural safety of the micro-vibration source by attenuating the transmitted force under launch loads and the micro-vibration isolation during their on-orbit operation has been proposed, which does not require the additional launch locking mechanism. To measure the characteristics of SMA mesh washer, we performed compressive loading tests with a single SMA mesh washer and a vibration isolator using SMA mesh washer. The numerical equivalent model of vibration isolator using SMA mesh washer composed of two spring and viscous damping elements has been verified that both stiffness and viscous damping varied with respect to compressed deformations. In addition, the effectiveness of launch loads and micro-vibration reduction has been investigated through the dynamic characteristics measurement test of cooler assembly combined with passive vibration isolator.
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