首页> 外国专利> TURBINE BLADE HAVING HEAT SINKS THAT HAVE THE SHAPE OF AN AEROFOIL PROFILE

TURBINE BLADE HAVING HEAT SINKS THAT HAVE THE SHAPE OF AN AEROFOIL PROFILE

机译:涡轮叶片具有热变形,具有翼型外形

摘要

A turbine blade has a pressure side, a suction side, and a cooling air channel, which is arranged between the pressure side and the suction side and which is bounded by inner surfaces of the pressure side and of the suction side. A cylindrical heat sink having a base surface, which has the shape of an aerofoil profile and has a profile top side and a profile bottom side, is arranged in the cooling air channel, which heat sink extends from the pressure side to the suction side. Turbulators are arranged on the inner surface of the pressure side and/or of the suction side in a region adjacent to the heat sink. The turbulators are arranged in such a way that lower air turbulence is produced in a region adjacent to the profile top side than in a region adjacent to the profile bottom side.
机译:涡轮叶片具有压力侧,吸入侧和冷却空气通道,该冷却空气通道布置在压力侧和吸入侧之间并且由压力侧和吸入侧的内表面界定。在冷却空气通道中布置有圆柱形的散热器,该圆柱形的散热器具有底面,该底面具有翼型轮廓的形状并且具有轮廓的顶侧和轮廓的底侧,该散热器从压力侧延伸到吸力侧。涡流器布置在压力侧和/或吸力侧的内表面上与散热器相邻的区域中。湍流器被布置成使得在与型材顶侧相邻的区域中产生比在与型材底侧相邻的区域中更低的空气湍流。

著录项

  • 公开/公告号US2016177739A1

    专利类型

  • 公开/公告日2016-06-23

    原文格式PDF

  • 申请/专利权人 SIEMENS AKTIENGESELLSCHAFT;

    申请/专利号US201414906322

  • 发明设计人 FATHI AHMAD;

    申请日2014-07-04

  • 分类号F01D5/18;

  • 国家 US

  • 入库时间 2022-08-21 14:36:31

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