한국기계가공학회지 (Journal of the Korean Society of Manufacturing Process Engineers)

  • 제21권8호
  • /
  • Pages.25-31
  • /
  • 2022
  • /
  • 1598-6721(pISSN)
  • /
  • 2288-0771(eISSN)
한국기계가공학회 (The Korean Society of Manufacturing Process Engineers)
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Ti-6Al-4V 합금 항공기 부품 가공 시 발생하는 절삭추력 및 소성변형에 대한 해석

Analysis of Cutting Force and Plastic Deformation Occurring During Machining of Ti-6Al-4V Alloy Aircraft Parts

  • 손휘준 (창원대학교 스마트제조융합협동과정) ;
  • 김석 (창원대학교 스마트제조융합협동과정) ;
  • 박기범 (창원대학교 스마트제조기술센터) ;
  • 정현철 ((주) 티씨티) ;
  • 조영태 (창원대학교 스마트제조융합협동과정)
  • Son, Hwi Jun (Department of Smart Manufacturing Engineering, Changwon National University) ;
  • Kim, Seok (Department of Smart Manufacturing Engineering, Changwon National University) ;
  • Park, Ki-Beom (Smart Manufacturing Technology Center, Changwon National University) ;
  • Jung, Hyoun Chul (Turbo CAM Technology) ;
  • Cho, Young Tae (Department of Smart Manufacturing Engineering, Changwon National University)
  • 투고 : 2022.06.02
  • 심사 : 2022.06.24
  • 발행 : 2022.08.31
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초록

Recently, investment in the aerospace industry has increased, and titanium alloys have been widely adopted for manufacturing parts in the aerospace industry. The Ti-6Al-4V alloy has high strength in high-temperature and high-pressure environments and is evaluated as a material with excellent heat, corrosion, and abrasion. However, titanium alloys are expensive, difficult to cut, and possess a large cutting load during the drilling process. In this study, the cutting force generated in the drilling process of Ti-6Al-4V alloy was verified via finite element analysis (FEM) and cutting force measurement experiments. A structural analysis was performed based on the cutting analysis data to verify the plastic deformation occurring during the drilling process of cylindrical Ti-6Al-4V alloy aircraft parts. Methods were proposed to predict the amount of deformation that occur during the manufacturing process of titanium-alloy aircraft parts and control the external environment, to minimize the amount of deformation.

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과제정보

이 논문은 2020년 정부(산업통상자원부)의 재원으로 한국산업기술진흥원의 지원을 받아 수행된 연구임. (P0015893, 항공기 엔진용 고압압축기 케이스의 성능개선) 이 논문은 정부(과학기술정보통신부)의 재원으로 한국연구재단의 지원을 받아 수행된 연구임. (No. NRF-2019R1A5A8083201)

참고문헌

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