대한기계학회논문집B (Transactions of the Korean Society of Mechanical Engineers B)

  • 제30권4호
  • /
  • Pages.328-336
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  • 2006
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  • 1226-4881(pISSN)
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  • 2288-5324(eISSN)
대한기계학회 (The Korean Society of Mechanical Engineers)
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가스터빈 블레이드 끝단 형상에 따른 블레이드 끝단 및 그 주변에서의 열전달 계수 변화

Effect of Blade Tip Geometry on Heat Transfer Coefficients on Gas Turbine Blade Tips and Near Tip Regions

  • 곽재수 (한국항공대학교 항공우주 및 기계공학부)
  • 발행 : 2006.04.01
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초록

Detailed heat transfer coefficient distributions an two. types of gas turbine blade tip, plane tip and squealer tip, were measured using a hue-detection base transient liquid crystals technique.. The heat transfer coefficients an the shroud and near tip regions of the pressure and suction sides af the blade were also. measured. The heat transfer measurements were taken at the three different tip gap clearances af 1.0%, 1.5%, and 2.5% of blade span. Results shaw the overall heat transfer coefficients on the tip and shroud with squealer tip blade were lower than those with plane tip blade. By using squealer tip, however, the reductions af heat transfer coefficients near the tip regions of the pressure and suction sides were nat remarkable.

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참고문헌

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피인용 문헌

  1. Numerical Study of Aerodynamics of Turbine Rotor with Leading Edge Modification Near Hub vol.37, pp.8, 2013, https://doi.org/10.3795/KSME-A.2013.37.8.1007