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

  • 제20권3호
  • /
  • Pages.223-228
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  • 2010
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  • 1598-2785(pISSN)
  • /
  • 2287-5476(eISSN)
한국소음진동공학회 (The Korean Society for Noise and Vibration Engineering)
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항공용 마운트의 개발과 시뮬레이션

The Development & Simulation for the Isolation Mount installed in Aircraft

  • 발행 : 2010.03.20
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초록

The mount which is used in military airplane should be operated in various situations such as vibration, shock and temperature. The recent mounts cost a lot and take much time to replace when they broke down. That's why new mount was produced in domestic by reverse engineering and the product has been proved its performance through environment test regarding vibration and shock. According to simulation of dynamic characteristics on vibration and shock, the result turns out to be similar to the result of the environmental test with an error of within 10 percent. As a result this research, a draft of the military aviation mount designing program is arranged.

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참고문헌

  1. Kwon, B. H., Kim, J., Kim J. C. and Seo, S. H., 2000, “Isolation Mount Design for the Combat Computer Console Installed in Surface Ship,” Proceedings of the KSNVE Annual Spring Conference, pp.1772-1777.
  2. MIL-STD-810E, 1989, “Environmental Test Methods And Engineering Guidelines.”
  3. MIL-STD-172C, 2001, “Case; Base, Mounting; And Mounts Vibration.”
  4. “Selection Guide for BARRY CONTROLS Isolators and Mounting Systems,” Barry Controls.
  5. Engineering Handbook,” Key Bellevills. INC.
  6. Hunt, J. B., 1979, “Dynamic Vibration Absorbers,” Mechanical Engineering Publications LTD London.
  7. Harris, C. M., 1990, “Shock & Vibration Handbook,” McGraw-Hill Handbooks.