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Shape Optimization for Enhancing the Performance of an Inducer for the Main Hydraulic Pump in a Rotary Wing Aircraft

회전익 항공기 주유압펌프용 인듀서 성능 향상을 위한 형상최적설계

  • Kim, Hyogyeum (Defence Systems Division, Research and Development 1 Team, Doosan Corporation) ;
  • Heo, Hyeungseok (Defence Systems Division, Research and Development 1 Team, Doosan Corporation) ;
  • Park, Youngil (Defence Systems Division, Research and Development 1 Team, Doosan Corporation) ;
  • Lee, Changdon (Defence Systems Division, Research and Development 1 Team, Doosan Corporation)
  • Received : 2017.03.15
  • Accepted : 2017.05.31
  • Published : 2017.06.01

Abstract

In this study, in order to prevent cavitation in a variable swash-plate type hydraulic pump, a basic model impeller has been applied to a new pump, and the impeller shape has been optimized through flow analysis. Based on the analysis results, we could propose an impeller shape with high efficiency and low possibility of cavitation in comparison with the basic model. The simplification of the basic shape of the impeller of the hydraulic pump was performed in three parts in the order of hub shape, wing, and curvature, and eight design parameters were defined to satisfy the design requirement. Compared with the initial model of the impeller, when the differential pressure of the optimum model increased, the efficiency was improved. It achieved the goal of design improvement because cavitation did not occur under the rated operating conditions.

Keywords

References

  1. Herbert H. Kouns, Inlet inducer-impeller for piston pump, US4281971, Aug. 4. 1981.
  2. 조재홍 외, 항공기용 가변 용량형 피스톤 펌프의 특성에 관한 연구, pp. 387-389, 한국정밀공학회 2008년도 추계학술대회논문집, 2008.
  3. Michael W. Volk., Pump characteristics and application, Marcel Dekker, 1996.
  4. David Japikse, William D. Marscher, Raymond B. Furst, Centrifugal Pump Design and Performance, Concepts ETI, Inc. pp.1-1-1-11, 1997.
  5. "Technical Report, Development Test Report", Eaton Aerospace, 2008.