Study of Design Technology of a Turbo-impeller

터보 임펠러 설계기술에 관한 고찰

  • 박영하 (경상대학교 대학원 항공우주시스템공학과) ;
  • 최형준 (경상대학교 대학원 항공우주시스템공학과) ;
  • 김재실 (창원대학교 메카트로닉스공학부 기계공학전공) ;
  • 조수용 (경상대학교 항공기부품기술연구센터)
  • Received : 2011.03.03
  • Accepted : 2011.04.22
  • Published : 2011.04.30

Abstract

A Turbo-impeller is widely used in industries as well as in aero engines. Its design technology has been developed since the early 20th century. However, the final configuration of the impeller depends on the designers. In this study, a whole design process was introduced and an optimization method to design an impeller was studied in order to design a better impeller without influence by designers. In particular, as the Artificial Neural Network was applied to the optimization, the computational time for the optimization was equivalent to the time consumed by the gradient method and its result was guaranteed as the optimum in the whole design domain. Using this method, any impeller can be improved by selecting design variables after measuring profiles of the impeller.

Keywords

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