Augmentor fuel conduit bushing
    1.
    发明专利

    公开(公告)号:SG128549A1

    公开(公告)日:2007-01-30

    申请号:SG200602657

    申请日:2006-04-20

    Abstract: A gas turbine engine augmentor has a centerbody within a gas flowpath from upstream to downstream. A plurality of vanes are positioned in the gas flowpath outboard of the centerbody. An aumentor fuel conduit extends through a first of the vanes to deliver fuel to the centerbody. An electrographitic carbon bushing guides and supports the augmentor fuel conduit.

    Augmentor spray bar mounting
    2.
    发明专利

    公开(公告)号:SG128547A1

    公开(公告)日:2007-01-30

    申请号:SG200602545

    申请日:2006-04-18

    Abstract: A gas turbine engine augmentor has a centerbody within a gas flowpath from upstream to downstream. The augmentor has upstream and downstream shell sections, a downstream rim of the upstream shell section meeting an upstream rim of the downstream shell section shell section. A plurality of vanes are positioned in the gas flowpath outboard of the centerbody. An augmentor spray bar fuel conduit extends through the centerbody and a first of the vanes to deliver fuel to the centerbody. A seal is mounted to the spray bar and positioned in a recess extending from at least one of the downstream rim of the upstream shell section and upstream rim of the downstream shell section shell section. The seal has a first portion and a second portion engaging the first portion in a backlocked interfitting.

    Augmentor spray bars
    7.
    发明专利

    公开(公告)号:SG128548A1

    公开(公告)日:2007-01-30

    申请号:SG200602655

    申请日:2006-04-20

    Abstract: A gas turbine engine fueling system includes a number of spray bars having conduits extending through associated vanes. A number of fuel injector nozzles are along each conduit. Each of the nozzles are positioned to discharge an associated fuel stream from one of the sides of the associated vane. A number of wear members are each mounted relative to the associated one of the nozzles for a range of motion relative thereto. The wear members movably cooperate with the associated vane to accommodate operating deflection and/or tolerances of the spray bars and vanes.

    Augmentor spray bar mounting
    8.
    发明专利

    公开(公告)号:AU2006201269A1

    公开(公告)日:2007-01-18

    申请号:AU2006201269

    申请日:2006-03-28

    Abstract: A gas turbine engine augmentor (18) has a centerbody (30) within a gas flowpath (20) from upstream to downstream. The augmentor (18) has upstream and downstream shell sections (32, 34), a downstream rim (108) of the upstream shell section (32) meeting an upstream rim (110) of the downstream shell section (34). A plurality of vanes (36) are positioned in the gas flowpath (20) outboard of the centerbody (30). An augmentor spray bar fuel conduit (66, 68) extends through the centerbody (30) and a first of the vanes (36) to deliver fuel to the centerbody (30). A seal (100) is mounted to the spray bar (64) and positioned in a recess (106) extending from at least one of the downstream rim (108) of the upstream shell section (32) and upstream rim (110) of the downstream shell section (34). The seal (100) has a first portion (150) and a second portion (152) engaging the first portion (150) in a backlocked interfitting.

    AUGMENTOR SPRAY BAR MOUNTING
    10.
    发明专利

    公开(公告)号:CA2545149A1

    公开(公告)日:2006-12-30

    申请号:CA2545149

    申请日:2006-04-25

    Abstract: A gas turbine engine augmentor has a centerbody within a gas flowpath fr om upstream to downstream. The augmentor has upstream and downstream shell sections, a downstream rim of the upstream shell section meeting an upstream rim of the downstream shell section shell section. A plurality of vanes are positioned in the gas flowpath outboard of the centerbody. An augmentor spray bar fuel conduit extends through the centerbody and a first of the vanes to deliver fuel to the centerbody. A seal is mounted to t he spray bar and positioned in a recess extending from at least one of the downstream rim of the upstream shell section and upstream rim of the downstream shell section shell section. The seal has a first portion and a second portion engaging the first portion in a backlocked interfitting.

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