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System for applying a continuous surface layer on porous substructures of turbine airfoils

机译:用于在涡轮机翼的多孔子结构上施加连续表面层的系统

摘要

A system for forming a surface coating on an outer surface of a foam for use with cooling system of turbine engines. The system may include removing filler from the outer surface of the foam to expose a porous structure of the foam, whereby portions of the porous structure extend outwardly from a newly formed outer surface of the filler. A surface layer may be applied to the outer surface of the filler and exposed portions of the porous structure, whereby the surface layer is attached to the porous structure at least in part due to mechanical interaction with the portions of the porous structure extending outwardly from the newly formed outer surface of the filler. The filler material may then be removed from the porous structure.
机译:一种用于在泡沫的外表面上形成表面涂层的系统,用于涡轮发动机的冷却系统。该系统可以包括从泡沫的外表面去除填料以暴露出泡沫的多孔结构,由此多孔结构的部分从填料的新形成的外表面向外延伸。可以将表面层施加到填料的外表面和多孔结构的暴露部分上,由此该表面层至少部分地由于与从多孔结构向外延伸的多孔结构部分的机械相互作用而附着于多孔结构。新形成的填料外表面。然后可以从多孔结构中去除填充材料。

著录项

  • 公开/公告号US7968144B2

    专利类型

  • 公开/公告日2011-06-28

    原文格式PDF

  • 申请/专利权人 ALLISTER W. JAMES;DOUGLAS J. ARRELL;

    申请/专利号US20070784982

  • 发明设计人 ALLISTER W. JAMES;DOUGLAS J. ARRELL;

    申请日2007-04-10

  • 分类号B05D3/00;B05D3/10;B05D1/02;B23P15/02;B32B5/18;

  • 国家 US

  • 入库时间 2022-08-21 18:09:19

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