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公开(公告)号:SG128549A1
公开(公告)日:2007-01-30
申请号:SG200602657
申请日:2006-04-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MULDOON MARC J , HARRIS MEGGAN H , BROOKS ROBERT T , SHERWOOD TOR W
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.
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公开(公告)号:SG128547A1
公开(公告)日:2007-01-30
申请号:SG200602545
申请日:2006-04-18
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MULDOON MARC J , SHERWOOD TOR W , HARRIS MEGGAN H , BROOKS ROBERT T
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.
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公开(公告)号:CA2545113A1
公开(公告)日:2006-12-30
申请号:CA2545113
申请日:2006-04-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MULDOON MARC J , HARRIS MEGGAN H , SHERWOOD TOR W , BROOKS ROBERT T
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 augmentor fuel conduit extends through a first of the vanes t o deliver fuel to the centerbody. An electrographitic carbon bushing guides and supports the augmentor fuel conduit.
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公开(公告)号:AU2006201270A1
公开(公告)日:2007-01-18
申请号:AU2006201270
申请日:2006-03-28
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MULDOON MARC J , BROOKS ROBERT T , HARRIS MEGGAN H , SHERWOOD TOR W
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公开(公告)号:CA2476471A1
公开(公告)日:2005-02-28
申请号:CA2476471
申请日:2004-08-04
Applicant: UNITED TECHNOLOGIES CORP
Inventor: RADER MATTHEW R , BROOKS ROBERT T
Abstract: An apparatus for separating two flanges, comprising a first prying grip havi ng at least one flange contact member, a second prying grip having at least one flange contact member; and means for separating the flange contact members.
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公开(公告)号:DE602004029535D1
公开(公告)日:2010-11-25
申请号:DE602004029535
申请日:2004-08-12
Applicant: UNITED TECHNOLOGIES CORP
Inventor: BROOKS ROBERT T , RADER MATTHEW R
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公开(公告)号:SG128548A1
公开(公告)日:2007-01-30
申请号:SG200602655
申请日:2006-04-20
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MULDOON MARC J , SHERWOOD TOR W , HARRIS MEGGAN H , BROOKS ROBERT T
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.
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公开(公告)号:AU2006201269A1
公开(公告)日:2007-01-18
申请号:AU2006201269
申请日:2006-03-28
Applicant: UNITED TECHNOLOGIES CORP
Inventor: MULDOON MARC J , BROOKS ROBERT T , HARRIS MEGGAN H , SHERWOOD TOR W
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.
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公开(公告)号:AU2006201268A1
公开(公告)日:2007-01-18
申请号:AU2006201268
申请日:2006-03-28
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SHERWOOD TOR W , MULDOON MARC J , BROOKS ROBERT T , HARRIS MEGGAN H
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公开(公告)号:CA2545149A1
公开(公告)日:2006-12-30
申请号:CA2545149
申请日:2006-04-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: SHERWOOD TOR W , HARRIS MEGGAN H , MULDOON MARC J , BROOKS ROBERT T
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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