한국해양공학회지 (Journal of Ocean Engineering and Technology)

한국해양공학회 (Korean Society of Ocean Engineers)
권호 표지

항공기용 가스터빈 재료의 열처리에 따른 크리프 특성

Creep Properties of Aircraft Gas Turbine Materials in relation to Heat Treatment

  • 공유식 (부경대학교 대학원 학연기계공학과) ;
  • 오세규 (부경대학교 기계.자동차 공학부) ;
  • 박노광 (한국기계연구원)
  • 발행 : 1999.11.30
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초록

In this paper, the creep properties and creep life prediction by Larson-Miller Parameter method for Udimet 720 to be used for aircraft gas turbine engines or other high temperature components were presented at the elevated temperatures of 538, 649 and $704^{\circ}C$. It was confirmed experimentally and quantitatively that a creep life predictive equation at such various high temperatures was well derived by LMP.

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