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Cast gas turbine blade through which coolant flows, together with appliance and method for manufacturing a distribution space of the gas turbine blade

机译:冷却剂流过的铸造燃气轮机叶片,以及用于制造燃气轮机叶片的分配空间的器具和方法

摘要

A cast gas turbine blade through which coolant flows, includes a blade root inserted into a disk of the gas turbine; a plurality of supply ducts; and a distribution space. Coolant is fed to the supply ducts through. a feed duct of the disk, the feed duct communicating with the supply duct via the distribution space. Flow and manufacture are optimized by a cast distribution space being present which has rounded or beveled inlet openings for the supply ducts and which is manufactured by means of a one-piece casting core.
机译:冷却剂流过的铸造燃气轮机叶片,包括插入到燃气轮机盘中的叶片根部;多个供应管道;和分配空间。冷却液通过管道输送到供应管道。盘的供给管,该供给管经由分配空间与供给管连通。通过铸件分配空间优化流动和制造,该铸件分配空间具有用于供应管道的圆形或斜角的入口,并通过一件式铸芯制造。

著录项

  • 公开/公告号US6565318B1

    专利类型

  • 公开/公告日2003-05-20

    原文格式PDF

  • 申请/专利权人 SIEMENS AKTIENGESELLSCHAFT;

    申请/专利号US20010937829

  • 发明设计人 PETER TIEMANN;

    申请日2001-09-28

  • 分类号B64C110/00;F01D51/80;

  • 国家 US

  • 入库时间 2022-08-22 00:07:34

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