부분분사 축류형 마이크로터빈에서의 성능예측 및 성능특성에 관한 연구

Performance Characteristics and Prediction on a Partially Admitted Single-Stage Axial-Type Micro Turbine

  • 조종현 (경상대학교 대학원) ;
  • 조수용 (경상대학교 항공기부품기술연구센터(기계항공공학부)) ;
  • 최상규 (한국기계연구원 장비개발실)
  • 발행 : 2005.12.01

초록

For axial-type turbines which operate at partial admission, a performance prediction model is developed. In this study, losses generated within the turbine are classified to windage loss, expansion loss and mixing loss. The developed loss model is compared with experimental results. Particularly, if a turbine operates at a very low partial admission rate, a circular-type nozzle is more efficient than a rectangular-type nozzle. For this case, a performance prediction model is developed and an experiment is conducted with the circular-type nozzle. The predicted result is compared with the measured performance, and the developed model quite well agrees with the experimental results. So the developed model could be applied to predict the performance of axial-type turbines which operate at various partial admission rates or with different nozzle shape.

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