• Title/Summary/Keyword: Jet flap

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Reliability Evaluation of Aircraft Brake Disk using the Non-contact Air-coupled Ultrasonic Transducer Method (비접촉 초음파 탐상 기법을 이용한 항공기 브레이크 디스크의 신뢰성 평가)

  • Kwak, Nam-Su;Kim, Jae-Yeol;Gao, Jia-Chen;Park, Dae-Kwang
    • Journal of the Korean Society of Manufacturing Process Engineers
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    • v.15 no.3
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    • pp.36-43
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    • 2016
  • Carbon fiber-reinforced silicon carbide (Cf-SiC) and SiC / SiC composites have high thermal conductivity, and excellent corrosion and wear resistance, a low coefficient for thermal expansion and are lightweight. This is why they are commonly used in parts of the aerospace industry to develop an aircraft thrust deflector, jet vane, combustion chamber, elevens, body flap, and a shingle. So, understanding how this state-of-the-art Cf-SiC affects both internal and external crack detection and determining issues during the manufacturing process of composite materials, should be evaluated according to valuation techniques in the external environment. In this paper, we apply a non-contact air ultrasonic technique of non-destructive testing techniques to perform a study on internal defect detection identification and assessment of carbon-fiber reinforced silicon carbide composites to perform basic research and applied research.