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이상용(S.Y Lee),김진봉(J.B Kim),엄문광(M.K Um),김태욱(T.K Kim),신정우(J.W Shin) 대한기계학회 2008 대한기계학회 춘추학술대회 Vol.2008 No.5
As a part of the enhancement of functional property and commercial program, aerospace industry is constantly driving the development about the high performance structural materials. Composite materials are one such class of materials that play a significant role in current and future aerospace components. So this paper presented an overview of the design concepts of composite landing gear components. First, composite fabrication method was determined Resin Transfer Moulding (RTM) and the FE model was designed by focus on feasibility for layer pattern of RTM process. Based on the those results achieved, conceptual model was verified by comparison with the used metal torque link through nonlinear static stress analysis and carbon/epoxy composite torque link was fabricated based on the verification result.
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