An Experimental Study on Selecting the Diameter of Probe Stylus of a Coordinate Measuring Machine in Measuring the Edge Profile of High Pressure Compressor

압축기 블레이드의 Edge 형상 측정시 3차원 측정기의 탐침 볼 직경 선정을 위한 실험적 연구

  • Joung, Soo-Ho (Department of Industrial and Systems Engineering and Research Center for Aircraft Parts Technology) ;
  • Byun, Jai-Hyun (Department of Industrial and Systems Engineering and Research Center for Aircraft Parts Technology)
  • 정수호 (경상대학교 산업시스템공학부.항공기부품기술연구센터) ;
  • 변재현 (경상대학교 산업시스템공학부.항공기부품기술연구센터)
  • Received : 20020300
  • Accepted : 20020800
  • Published : 2002.12.31

Abstract

When the trailing edge and leading edge of an airfoil contour of high pressure compressor blades are measured, there exists a measurement error due to the size of the probe stylus ball diameter. In the paper an experimental study is provided to determine the optimum diameter of the probe stylus in inspecting the airfoil of the high pressure compressor blade. The measurement and analysis procedure suggested in this paper will be helpful to those who are involved in measuring and inspecting various types of blades.

Keywords

References

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