Bolting configuration for joining ceramic combustor liner to metal mounting attachments
    2.
    发明申请
    Bolting configuration for joining ceramic combustor liner to metal mounting attachments 有权
    将陶瓷燃烧器衬套连接到金属安装附件的螺栓结构

    公开(公告)号:US20070240423A1

    公开(公告)日:2007-10-18

    申请号:US11247129

    申请日:2005-10-12

    IPC分类号: F02C1/00

    CPC分类号: F23R3/60 F23R3/007

    摘要: A gas turbine combustor includes a substantially cylindrical combustor liner located substantially concentrically within a flow sleeve, the combustor liner composed through a ceramic matrix composite material, a forward end of the combustor liner provided with a plurality of circumferentially arranged bolt holes. An inner metal ring is located about an outside surface of the forward end of the combustor liner, the inner metal ring provided with a second plurality of circumferentially spaced bolt holes, with a plurality of bolts extending through the first and second pluralities of bolt holes and secured by self-locking nuts. An outer metal ring is spaced radially outwardly of the inner metal ring, with a plurality of circumferentially spaced struts extending between the inner and outer rings.

    摘要翻译: 燃气轮机燃烧器包括基本上圆柱形的燃烧器衬套,其基本上同心地位于流动套管内,燃烧器衬套通过陶瓷基体复合材料构成,燃烧器衬套的前端设有多个周向布置的螺栓孔。 内金属环位于燃烧器衬套的前端的外表面周围,内金属环设置有第二多个周向间隔开的螺栓孔,多个螺栓延伸穿过第一和第二多个螺栓孔, 由自锁螺母固定。 外金属环与内金属环径向向外间隔开,多个周向隔开的支柱在内环和外环之间延伸。

    Turbine engine shroud segment
    3.
    发明申请
    Turbine engine shroud segment 审中-公开
    涡轮发动机护罩段

    公开(公告)号:US20060078429A1

    公开(公告)日:2006-04-13

    申请号:US10962310

    申请日:2004-10-08

    IPC分类号: F01D9/00

    CPC分类号: F01D25/246 F01D9/04

    摘要: A turbine engine shroud segment comprises a body including an outer surface away from which an integral attachment system projects. The attachment system comprises a plurality of at least two axially spaced apart circumferentially extending rows of discrete projection hook segments to interrupt a potential hoop stress path through the attachment system. Each projection hook segment includes a segment support surface aligned circumferentially and radially with other segment support surfaces in a row.

    摘要翻译: 涡轮发动机护罩段包括主体,该主体包括远离该整体附接系统突出的外表面。 附接系统包括多个至少两个轴向间隔开的周向延伸的一排离散的突出钩段,以中断通过附接系统的潜在的环向应力路径。 每个突出钩段包括沿圆周和径向对准的一段支撑表面,其中一行中的其他段支撑表面。