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Stress Analysis of Plate-Spring-Type Landing Gear Materials

판스프링형 랜딩기어의 재질에 따른 응력 해석

  • 김경환 (충남대학교 기계설계공학과) ;
  • 이영신 (충남대학교 기계설계공학과) ;
  • 한재도 ((주)한얼시스템)
  • Received : 2012.12.28
  • Accepted : 2014.02.04
  • Published : 2014.03.01

Abstract

Aircraft are an indispensable mode of modern transportation. They are also used as in a wide variety of other fields. For example, aircraft are used for accommodating passengers, carrying freight, and for military reconnaissance. Aircraft ground operations include landing and taking off. During landing, a higher load is applied to the landing gear than during takeoff. The landing gear should absorb impact energy and prevent damage to the main body of the aircraft in the case of an accident. In this study, simulations were performed for two types of plate-spring-type landing gear: that made of composite materials and that constructed with aluminum. The structural safety of landing gear made of each material was also evaluated.

Keywords

Landing Gear;Plate Spring;Composite Material;Margin of Safety

References

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Cited by

  1. Study on the Linear Static Structural Analysis Error of Helical Compression Springs vol.40, pp.2, 2016, https://doi.org/10.3795/KSME-A.2016.40.2.237