항공기 브레이크 디스크(CFRC)의 피로특성연구

A Study on Fatigue Characteristics of Aircraft Brake Disk Material (CFRC)

  • 김혜성 (부산대학교 나노과학기술대학 나노정보소재공학과) ;
  • 김현수 (부산대학교 나노과학기술대학 나노시스템공정학과) ;
  • 감문갑 (국방품질기술원) ;
  • 김태규 (부산대학교 나노과학기술대학 나노시스템공정학과)
  • Kim, Hye Sung (Dept. of Nanomaterials Engineering, Pusan National University) ;
  • Kim, Hyun Soo (Dept. of Nanosystem Engineering, Pusan National University) ;
  • Kam, Moon Gap (Defence Agency for Technology & Quality) ;
  • Kim, Tae Gyu (Dept. of Nanosystem Engineering, Pusan National University)
  • 투고 : 2008.03.19
  • 심사 : 2008.04.11
  • 발행 : 2008.05.31

초록

The fatigue characteristics of the carbon fiber reinforced carbon composites (CFRC) material are necessary for the advanced industries requiring the thermal resistance. The research and development of CFRC have been in progress in the field of aerospace and defense industry. In this paper, we investigated the fatigue characteristics of CFRC by using an aircraft brake disk system. As the results of a series of tensile tests, the tensile strengths of CFRC were appeared 102.8 MPa ($0^{\circ}$), 98.6 MPa ($60^{\circ}$), and 95.5 MPa ($90^{\circ}$), respectively. It was showed that CFRC had better tensile property than the usual composite materials. As the results of fatigue tests, the fatigue limit was ~ 77 MPa, which is under the 75% of the maximum tensile load. CFRC is recommended as a strong potential composite materials because the carbon fibers are closely packed and strongly bonded between the carbon fibers.

키워드

참고문헌

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