Method and apparatus for assembling gas turbine engine combustors
    1.
    发明申请
    Method and apparatus for assembling gas turbine engine combustors 有权
    用于组装燃气涡轮发动机燃烧器的方法和装置

    公开(公告)号:US20060130485A1

    公开(公告)日:2006-06-22

    申请号:US11015175

    申请日:2004-12-17

    IPC分类号: F23R3/42

    摘要: A method enables a combustor for a gas turbine engine to be assembled. The method includes coupling an inner liner to an outer liner such that a combustion chamber is defined therebetween, wherein the outer liner is fabricated from a plurality of panels coupled together, and coupling an outer support radially outward from the outer liner such that an outer passageway is defined between the outer liner and the outer support, wherein the outer support is configured to channel cooling air from the outer passageway towards at least a portion of the outer liner.

    摘要翻译: 一种方法使得能够组装用于燃气涡轮发动机的燃烧器。 该方法包括将内衬套连接到外衬套,使得在其间限定燃烧室,其中外衬套由联接在一起的多个面板制成,并且将外支撑件从外衬里径向向外联接,使得外套管 限定在外衬套和外支撑件之间,其中外支撑件构造成将冷却空气从外通道向至外部衬套的至少一部分引导。