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    • 1. 发明申请
    • Combustor flow sleeve attachment system
    • 燃烧器流套管附件系统
    • US20070130958A1
    • 2007-06-14
    • US11298323
    • 2005-12-08
    • Rajeev OhriArthur HarrisElliot GriffinMichael KoenigHerbert ReidPaul Maples
    • Rajeev OhriArthur HarrisElliot GriffinMichael KoenigHerbert ReidPaul Maples
    • F23R3/60
    • F23R3/60
    • Embodiments of the invention relate to a combustor flow sleeve for a turbine engine. According to aspects of the invention, the flow sleeve can be attached to one of the components in the combustor head-end by a plurality of fasteners. In one embodiment, the flow sleeve can be attached directly to the combustor head-end component by a plurality of bolts. The bolted flow sleeve can reduce the time to install or remove the flow sleeve. In certain areas, it may not be possible to directly attach the flow sleeve to the combustor component. A flow sleeve according to aspects of the invention can be adapted to facilitate indirect attachment to the combustor head-end component. The flow sleeve can further be adapted to include thermal relief slots to accommodate any differential thermal expansion or contraction between the flow sleeve and the component to which the flow sleeve is attached.
    • 本发明的实施例涉及一种用于涡轮发动机的燃烧器流动套筒。 根据本发明的方面,流动套管可以通过多个紧固件附接到燃烧器头端中的一个部件。 在一个实施例中,流动套筒可以通过多个螺栓直接附接到燃烧器头端部件。 螺栓流动套筒可以减少安装或拆卸流动套管的时间。 在某些区域中,可能不可能将流动套筒直接附接到燃烧器部件。 根据本发明的方面的流动套筒可以适于促进间接地连接到燃烧器头端部件。 流动套管还可以适于包括热释放槽,以适应流动套筒与流动套筒所附接的部件之间的任何不同的热膨胀或收缩。