Vibration Isolation System of a Large Reverberation Chamber

대형 잔향실의 방진 설계 및 검증

  • 김영기 (한국항공우주연구원 위성연구부) ;
  • 김홍배 (한국항공우주연구원 위성연구) ;
  • 이동우 (한국항공우주연구원 위성연구) ;
  • 우성현 (한국항공우주연구원 위성연구) ;
  • 문상무 (한국항공우주연구원 위성연구부)
  • Published : 2003.11.01

Abstract

A vibration isolation system fur a large reverberation chamber (1,228㎥, 1,000ton) has been installed. The reverberation chamber generates loud noise and induces high level of vibration to perform spacecraft acoustic environmental tests. The isolation system prevents vibration transfer from the chamber to enclosure buildings. This paper describes logical design process and commissioning experiments of the system. Design criteria have been induced from rigid body model of the chamber. Finite element model has been employed to select the characteristics of rubber pads. A total of 21 rubber pads have been installed between the chamber and supporting pedestals. A sand bag of 800kg was dropped on the chamber floor to measure the natural frequency of the isolation system. Absolute transmissibility has been measured while generating 145㏈ in the chamber. The natural frequency of the chamber is 10.5㎐, which is 80% of estimated value. Overall transmissibility at working frequency range (25㎐-10,000㎐) is less than -6㏈.

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