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Turbine airfoil with floating wall mechanism and multi-metering diffusion technique

机译:带有浮动壁机构和多计量扩散技术的涡轮机翼型

摘要

A turbine airfoil usable in a turbine engine and having at least one cooling system. The turbine airfoil may include an interlayer coupled to an outer surface of the outer wall of the airfoil, wherein the interlayer may be formed from a porous material that allows cooling fluids to pass through the interlayer. The floating wall may be coupled to an outer surface of the interlayer, wherein the floating wall may be formed from a plurality of floating wall segments positioned in close proximity to each other but with a film cooling slot positioned between the adjacent wall segments to enable cooling fluids to be exhausted from the elongated hollow airfoil. The cooling system may include an outer wall diffusion chamber positioned in the outer wall and an interlayer diffusion chamber. One or more metering holes may be in communication with the outer wall and interlayer diffusion chambers.
机译:一种可用于涡轮发动机并具有至少一个冷却系统的涡轮机翼。涡轮机翼型件可以包括联接至翼型件的外壁的外表面的中间层,其中,中间层可以由允许冷却流体通过中间层的多孔材料形成。所述浮壁可以联接至所述中间层的外表面,其中,所述浮壁可以由彼此紧邻设置的多个浮壁段形成,但是在相邻的壁段之间设置有薄膜冷却槽以实现冷却。从细长的中空翼型中排出的流体。冷却系统可包括位于外壁中的外壁扩散室和层间扩散室。一个或多个计量孔可以与外壁和层间扩散室连通。

著录项

  • 公开/公告号US2007280832A1

    专利类型

  • 公开/公告日2007-12-06

    原文格式PDF

  • 申请/专利权人 GEORGE LIANG;

    申请/专利号US20060447730

  • 发明设计人 GEORGE LIANG;

    申请日2006-06-06

  • 分类号F01D5/18;

  • 国家 US

  • 入库时间 2022-08-21 20:11:13

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