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Process Design of Isothermal Forging for Three-Dimensional Ti-6Al-4V Wing-Shape

Ti-6Al-4V 합금 3D 날개형상의 항온단조 공정설계

  • 염종택 (한국기계연구원 공정연구부) ;
  • 박노광 (한국기계연구원 공정연구부) ;
  • 이유환 (포항공과대학교 신소재공학과) ;
  • 신태진 (포항공과대학교 기계공학과) ;
  • 홍성석 (국방과학연구소 기술연구본부) ;
  • 심인옥 (국방과학연구소 기술연구본부) ;
  • 황상무 (포항공과대학교 기계공학과) ;
  • 이종수 (포항공과대학교 신소재공학과)
  • Published : 2005.04.01

Abstract

The isothermal forging design of a Ti-6Al-4V wing shape was performed by 3D FE simulation. The design focuses on near-net shape forming by the single stage. The process variables such as the die design, pre-form shape and size, ram speed and forging temperature were investigated. The main design priorities were to minimize forging loads and to distribute strain uniformly in a given forging condition. The FE simulation results for the final process design were compared with the isothermal forging tests. The instability of deformation was evaluated using a processing map based on the dynamic materials model(DMM), including flow stability criteria. Finally, a modified process design for producing a uniform Ti-6Al-4V wing product without forming defects was suggested.

Keywords

References

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