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http://dx.doi.org/10.5050/KSNVE.2010.20.3.223

The Development & Simulation for the Isolation Mount installed in Aircraft  

Jeon, Hee-Ho (LIG넥스원 구미연구소)
Park, Jae-Min (LIG넥스원 구미연구소)
Lee, Seung-Joon (LIG넥스원 구미연구소)
Publication Information
Transactions of the Korean Society for Noise and Vibration Engineering / v.20, no.3, 2010 , pp. 223-228 More about this Journal
Abstract
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.
Keywords
Mount; Transmissibility; Recurdye; Environment Test; Vibration Test; Shock Test;
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  • Reference
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.   과학기술학회마을
2 MIL-STD-810E, 1989, “Environmental Test Methods And Engineering Guidelines.”
3 Hunt, J. B., 1979, “Dynamic Vibration Absorbers,” Mechanical Engineering Publications LTD London.
4 Harris, C. M., 1990, “Shock & Vibration Handbook,” McGraw-Hill Handbooks.
5 MIL-STD-172C, 2001, “Case; Base, Mounting; And Mounts Vibration.”
6 “Selection Guide for BARRY CONTROLS Isolators and Mounting Systems,” Barry Controls.
7 Engineering Handbook,” Key Bellevills. INC.