동력기계공학회지 (Journal of Power System Engineering)

  • 제21권1호
  • /
  • Pages.70-79
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  • 2017
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  • 2713-8429(pISSN)
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  • 2713-8437(eISSN)
한국동력기계공학회 (The Korean Society for Power System Engineering)
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터빈익렬의 이동에 따른 손실 및 유동장에 관한 실험적 연구

Losses and Flow Structure for the Movement of Turbine Blade Row

  • 조수용 (경상대학교 공과대학 항공기부품 기술연구센터) ;
  • 정양범 (BIP 기술연구소)
  • 투고 : 2016.12.09
  • 심사 : 2017.02.01
  • 발행 : 2017.02.28
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초록

The output power of turbine is greatly affected by the losses generated within the passage. In order to develop a better turbine or loss models, an experimental study was conducted using a linear cascade experimental apparatus. The total pressure loss and flow structures were measured at two cross-sectional planes located downstream of blade row. Measurement was conducted in a steady state for the several different locations of the blade row along the rotational direction. The blade row moved by 20 % of the pitch, and tip clearance was varied from 2% to 8%. Axial-type blades were used and its blade chord was 200mm. A square nozzle was applied and its size was $200mm{\times}200mm$. The experiment was conducted at a Reynolds number of $3{\times}10^5$ based on the chord. Nozzle flow angle sets to $65^{\circ}$ based on the axial direction and the solidity of blade row was 1.38. From the experimental results, the total pressure loss was greatly varied in the receding region than in the entering region. The flow properties within the blade passage were strongly changed according to the location of blade row.

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참고문헌

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