Numerical Analysis of Forming for KEP engine Sheet matal part

KFP 엔진 박팍 부품 드로잉 성형해석

  • 오성국 (삼성 항공(주) 엔진 사업본부) ;
  • 정완진 (삼성 종합기술원 CAE연구실) ;
  • 안홍 (삼성 항공(주) 엔진 사업본부) ;
  • 이영호 (삼성 항공(주) 엔진 사업본부)
  • Published : 1994.06.01

Abstract

The Aerospace and automobile industries have need to avoid sheet-metal forming problem such as incorrect springback after forming and trimming process, excessive thinning/tearing, wrinking/perkering. It is common practice to use costly trial-and-error experimental methods to develop tooling and manufacturing process parameters. Experimentation should be complemented with computer simulation to reduce cost and leadtime in manufacturing and to influence the design of components. In this study, firstly we solved the springback problem after drawing and trimming process of KFP(F100-229) engine airsealing bearing support part(53H00) forming and studied on the effect of several process parameters on the gap between the formed blank and punch shape using the implicit F.E.M code(ABAQUS). Secondly by the three dimensional dynamic analysis using the explicit. F. E. M code (LS-DYNA3D), we studied on the effect of several process parameters which can be used for avoid tearing and wrinking during the drawing process.

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