The Case Study of High Strength Bolt Cadmium Embrittlement Failure

고강도 볼트 카드늄 취성파괴 사례연구

  • 윤용인 (공군사관학교 항공우주공학과) ;
  • 박찬욱 (공군 항공기술연구소 시험분석실) ;
  • 손경숙 (공군 항공기술연구소 시험분석실)
  • Published : 2008.11.05

Abstract

It happened a failure on special bolt which supported main landing gear actuator up-lock rod of 00 aircraft. Fracture was occurred at end of center drilled hole and thread machined on bolt. Metallographic, fractographic, and other characteristics of embrittlement analysis and experiments carried out on the failed bolt to find out the reason. Bolt surface was cadmium electroplated(EP) to give lubrication and provide excellent corrosion resistance. Resultly, Bolt was failed due to cadmium embrittlement occurred during baking treatment as well as center drilled hole. for the failure that are relevant to failure analysis and prevention. For their successful functional application, cadmium EP bolts require proper and adequate baking treatment after electroplating, and is complete with no center drilled hole

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