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TBC attachment construction for a cooled turbine airfoil and method of forming a TBC covered airfoil

机译:用于冷却的涡轮机翼型的TBC附接构造和形成TBC覆盖的翼型的方法

摘要

A TBC covered substrate, such as an airfoil used in a gas turbine engine, the substrate has a plurality of open cells formed thereon with the cell walls being formed by ribs arranged to form substantially rectangular shaped cells. The walls or ribs or the cells have cross-over holes formed at about the mid-point of the cell wall and a wire band is passed through the cross-over holes and extends through the cells. A TBC is sprayed into the cells to fill the cell and cover the wire band such that the wire band functions to reinforce the TBC. The cell floors include at least one cooling air feed hole and the TBC is a porous material such that cooling air passing through the feed holes will also pass through the TBC. During the process of forming the airfoil with the TBC covered, air is passed through the feed holes while the TBC is being applied to prevent the feed holes from being blocked by the TBC.
机译:TBC覆盖的基底,例如在燃气涡轮发动机中使用的翼型,该基底具有在其上形成的多个开孔,该孔壁由布置为形成基本矩形孔的肋形成。壁或肋或单元具有在单元壁的大约中点处形成的交叉孔,并且线带穿过交叉孔并延伸穿过单元。将TBC喷涂到小室中以填充小室并覆盖导线带,以使导线带起到增强TBC的作用。隔室底板包括至少一个冷却空气供给孔,并且TBC是多孔材料,使得通过供给孔的冷却空气也将通过TBC。在形成覆盖有TBC的翼型的过程中,在施加TBC的同时使空气通过进料孔,以防止进料孔被TBC阻塞。

著录项

  • 公开/公告号US7704049B1

    专利类型

  • 公开/公告日2010-04-27

    原文格式PDF

  • 申请/专利权人 GEORGE LIANG;

    申请/专利号US20060636237

  • 发明设计人 GEORGE LIANG;

    申请日2006-12-08

  • 分类号B64C11/24;F01D5/18;

  • 国家 US

  • 入库时间 2022-08-21 18:49:10

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