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Study on Deformation Analysis of Holes during Drilling of Aircraft Engine Compressor Cases

항공기 엔진 압축기 케이스의 드릴링 시 홀의 변형 해석에 관한 연구

  • Received : 2018.04.24
  • Accepted : 2018.05.01
  • Published : 2018.06.30

Abstract

M152, used for aircraft engine compressor cases, causes many problems in the cutting process due to its high hardness and high toughness. Characterized by a concave cylindrical center, aircraft engine compressor cases are thin but have multiple side holes to connect with internal parts. Thus, deformation occurs despite the jig sustaining the inside. The object of this study was to lessen the deformation arising from drilling by improving the drilling jig for aircraft engine compressor cases. To this end, an aircraft engine compressor case modeled with SolidWorks was analyzed with ANSYS under real conditions. Then, to secure reliability, the analyzed deformation was compared with the actual deformation. Based on the results, the effects of the improved drilling jig for aircraft engine compressor cases were verified.

Keywords

References

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