Transactions of the Korean Society for Noise and Vibration Engineering (한국소음진동공학회논문집)

The Korean Society for Noise and Vibration Engineering (한국소음진동공학회)
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Comparisons of Isolation Performances for the SMA Mesh Washer Isolator with the Variation of Pre-compressed Displacement

초기압축변위에 따른 형상기억합금 메쉬 와셔 절연계의 절연 성능 비교

  • 윤세현 (한국항공우주연구원 발사체구조팀) ;
  • 정호경 (한국항공우주연구원 발사체구조팀) ;
  • 한재흥 (한국과학기술원 항공우주공학)
  • Received : 2010.12.02
  • Accepted : 2011.01.25
  • Published : 2011.02.20
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Abstract

Launch vehicles and satellites experience severe vibration and pyroshock during the flight phase. These severe dynamic loading could result in the malfunction of electric devices which equipped in the launch vehicle and satellite. In this paper, mesh washer isolators are applied to attenuate these severe shock and vibration and isolation performances are enhanced by applying pseudoelasitic SMA wire material. Through random vibration and ground pyroshock tests, outstanding isolation performances are studied. Especially, comparison of isolation performances due to the change of pre-compressive displacement of mesh washer itself are suggested and applicablity to the adaptive vibration control are confirmed.

Keywords

References

  1. Moening, C. J., 1985, Pyrotechnic ShockFlight Failures, Institute of Environmenatal SciencesPyrotechnic Shock Tutorial Program, 31st AnnualTechnical Meeting, Institution of EnvironmentalScience.
  2. Mercer, C. A. and Rees, P. L., 1971, AnOptimum Shock Isolator, Journal of Sound andVibration, Vol. 18, No. 4, pp. 511-520. https://doi.org/10.1016/0022-460X(71)90102-7
  3. Youn, S.-H., Jang, Y.-S. and Han, J.-H., 2010,Comperssed Mesh Washer Isolators Using thePseudoelasticity of SMA for Pyroshock Attenuation,Journal of Intelligent Material Systems andStructures, Vol. 21, pp. 407-421. https://doi.org/10.1177/1045389X09355665
  4. Duerig, T. W., Melton, K. N., Stockel, D. andWayman, C. M., 1990, Engineering Aspects of ShapeMemory Alloys, Butterworth Heinemann, London.
  5. http://www.nitinol.com/
  6. Predki, W. and Kloenne, M., 2002, Dampingof Superelastic NiTi-alloys under Torsional Loading,Shape Memory and Superelastic Technologies andShape Memory Materials, pp. 115-119.
  7. Yiu, Y. C. and Regelbrugge, M. E. 1995.Shape-memory Alloy Isolators for VibrationSuppression in Space Applications, Structures,Structural Dynamics and Materials, AIAA-95-1120-CP, pp. 3390-3398.
  8. Kim, H.-B., Oh, J.-H., Moon, S.-M., Woo,S.-H. and Lee, S.-S., 2000, Development of ShockTesting M/C to Simulate Pyro-technic DeviceExplosion of Space Vehicle, Proceedings of theKSNVE Annual Spring Conference, pp. 581-586.

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