A Study on Load Spectrum for Fatigue Analysis of Helicopter Rotor Blades

헬리콥터 로터 블레이드의 피로해석을 위한 하중 스펙트럼연구

  • 오만석 (한국항공대학교 항공우주 및 기계공학부) ;
  • 김현덕 (한국항공대학교 항공우주 및 기계공학부) ;
  • 기영중 (한국항공우주연구원, KHP개발실) ;
  • 박정선 (한국항공대학교 항공우주 및 기계공학부)
  • Published : 2007.09.30

Abstract

In this paper, we deducted the missions with respect to Korea utility helicopter (KUH) and consist of the scenarios which describe proper purpose of KUH. And so developed fatigue load spectrum of KUH by applying Helix that is fatigue load spectrum for blade of articulated helicopter rotor system. The developed load spectrum is applied to fatigue analysis of blade by modeled finite element with stress-life method (S-N). And we compared the result of fatigue analysis to prior to Helix for the sake of verifying the load spectrum that we generated.

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