한국소음진동공학회:학술대회논문집 (Proceedings of the Korean Society for Noise and Vibration Engineering Conference)
- 한국소음진동공학회 2013년도 춘계학술대회 논문집
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- Pages.383-389
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- 2013
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- 1598-2548(pISSN)
기본임무를 수행하는 기동헬기에 적용될 무베어링 허브 복합재 구성품 피로수명 해석
Bearingless Rotor Hub Composite Component Fatigue Analysis of Utility Helicopter to perform the Basic Mission
- 발행 : 2013.04.24
초록
Rotor system is a very important part which produces lift, thrust and control force in helicopter. Component of rotor system must endure various flight load for the required life. In helicopter rotor system, bearingless rotor system is the highest technology rotor system compare with articulated and hingeless rotor system. Baaringless rotor system is not include mechanical flap hinge, lag hinge and pitch bearing. Bearingless rotor component flexbeam which made by composite material has conduct hinge and bearing role instead of mechanical flap hinge, lag hinge and pitch bearing. These characteristics has less part number and lass weight than others. In this paper, conduct safe life analysis of bearingless composite component flexbeam and torque tube applying to utility helicopter load condition.
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