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96 条记录 (耗时 0.016 秒)

    Stand-off device for double-skin combustor liner
    1.
    发明授权
    Stand-off device for double-skin combustor liner 有权

    公开(公告)号：US11435078B2

    公开(公告)日：2022-09-06

    申请号：US16448584

    申请日：2019-06-21

    申请人： PRATT & WHITNEY CANADA CORP.

    发明人： Tin-Cheung John Hu ,  Oleg Morenko

    IPC分类号： F23R3/00 ,  F23R3/60 ,  F23R3/48 ,  F02C3/14 ,  F02K1/80

    摘要： A combustor for a gas turbine engine comprises a combustor chamber defined at least partially by an outer combustor skin and an inner combustor skin. A plurality of stand-off devices have a body including a first end and a second end, the second end of the body retained in an opening in the outer combustor skin, the first end spaced apart from the second end and abutting the inner combustor skin to space the inner combustor skin apart from the outer combustor skin.

    CROSS IGNITION FLAME DUCT
    5.
    发明申请
    CROSS IGNITION FLAME DUCT 审中-公开

    公开(公告)号：US20170227228A1

    公开(公告)日：2017-08-10

    申请号：US15502638

    申请日：2014-09-05

    申请人： SIEMENS AKTIENGESELLSCHAFT

    发明人： Daniel W. Garan ,  Richard L. Thackway ,  David P. Holzapfel ,  Stephen A. Ramier ,  Charalambos Polyzopoulos ,  Kevin J. Spence ,  Joseph Scott Markovitz

    IPC分类号： F23R3/48 ,  F23R3/46

    摘要： A cross-flame duct (100) for connecting adjacent combustors (1, 2) together in a gas turbine to guard against flameout conditions within the combustors (1, 2), whereby the cross-flame duct (100) may include first and second ducts (102, 106) forming a slip joint to prevent stress from developing within the cross-flame duct (100) is disclosed. The cross-flame duct (100) remains flexible during turbine operation due to the slip joint, thereby preventing damaging thermal and mechanical stresses from developing within the cross-flame duct (100) and enhancing the useful life of the cross-flame duct (100) and associated components. The first and second ducts (102, 106) may also include cooling chambers (138, 156, 174) positioned between outer sleeves (122, 140) and inner housings (128, 146) and maintained with one or more standoffs (134, 152, 170) to reduce thermal stress and gradients or prevent material loss due to overheating or burning. The cooling chambers (138, 156, 174) may be supplied with cooling fluids via one or more fluid ports (176) extending through the outer sleeves (122, 140) enabling air to flow through the cooling chambers (1138, 156, 174) and into the combustors (1, 2).

    CMC CROSS-OVER TUBE
    6.
    发明申请
    CMC CROSS-OVER TUBE 审中-公开

    公开(公告)号：US20170059165A1

    公开(公告)日：2017-03-02

    申请号：US14839260

    申请日：2015-08-28

    申请人： Rolls-Royce High Temperature Composites Inc.

    发明人： Sujit Nanda

    IPC分类号： F23R3/48 ,  F16L23/12

    CPC分类号： F23R3/48 ,  F16L49/04

    摘要： A fluid conduit may be provided comprising a ceramic matrix composite (CMC) cross-over tube and a flange. The CMC cross-over tube may comprise a first end configured to extend into a first combustor liner of a gas turbine engine, and a second end configured to extend into a second combustor liner of a gas turbine engine. The interior of the CMC cross-over tube may define a passageway. The flange may extend outwardly from an outer surface of the CMC cross-over tube. The flange may be configured to engage at least one of the first combustor liner and the second combustor liner.

    摘要翻译： 可以提供流体导管，其包括陶瓷基复合（CMC）交叉管和凸缘。 CMC交叉管可以包括构造成延伸到燃气涡轮发动机的第一燃烧器衬套中的第一端和构造成延伸到燃气涡轮发动机的第二燃烧器衬套中的第二端。 CMC交叉管的内部可以限定通道。 凸缘可以从CMC交叉管的外表面向外延伸。 凸缘可以被构造成接合第一燃烧器衬套和第二燃烧器衬套中的至少一个。

    Gas turbine combustor and operating method for gas turbine combustor
    8.
    发明授权
    Gas turbine combustor and operating method for gas turbine combustor 有权
    燃气轮机燃烧器和燃气轮机燃烧器的操作方法

    公开(公告)号：US09464809B2

    公开(公告)日：2016-10-11

    申请号：US13933227

    申请日：2013-07-02

    申请人： Mitsubishi Hitachi Power Systems, Ltd.

    发明人： Kazuki Abe ,  Tomomi Koganezawa ,  Takeo Saito ,  Keisuke Miura

    IPC分类号： F23R3/28 ,  F02C7/22 ,  F02C7/26 ,  F23R3/12 ,  F23R3/16 ,  F23R3/48 ,  F23R3/34 ,  F23D14/24

    CPC分类号： F23R3/286 ,  F02C7/22 ,  F02C7/26 ,  F23D14/24 ,  F23N2027/02 ,  F23R3/12 ,  F23R3/16 ,  F23R3/28 ,  F23R3/346 ,  F23R3/48

    摘要： Disclosed is a gas turbine combustor equipped with a burner constructed to fire a plurality of combustors at the same time at a fuel/air ratio suitable for gas turbine ignition. A plurality of supports mounted for fixing an air injection hole plate to the combustor are provided at substantially the same phase position as that of cross fire tubes, and combustion air allocations are adjusted. Thus, flame propagation during gas turbine ignition is accelerated and all combustor cans are fired. In addition, porous plates are disposed downstream of the supports and the combustion air allocations are readjusted. Furthermore, air injection holes proximate to the cross fire tubes are particularly reduced in diameter to further adjust the combustion air allocations.

    摘要翻译： 公开了一种装备有燃烧器的燃气轮机燃烧器，该燃烧器构造成以适于燃气轮机点火的燃料/空气比同时燃烧多个燃烧器。 多个安装用于将空气喷射孔板固定到燃烧器的支撑件设置在与防火管基本相同的相位位置，并且调节燃烧空气分配。 因此，燃气轮机点火期间的火焰传播被加速并且所有燃烧器罐都被点燃。 此外，多孔板设置在支撑件的下游，并且重新调节燃烧空气分配。 此外，靠近十字火管的空气喷射孔的直径特别减小，以进一步调节燃烧空气分配。

    SUPER TELESCOPING CROSS-FIRE TUBE AND METHOD OF ASSEMBLING A COMBUSTOR STRUCTURE
    9.
    发明申请
    SUPER TELESCOPING CROSS-FIRE TUBE AND METHOD OF ASSEMBLING A COMBUSTOR STRUCTURE 审中-公开
    超级冲击火管和组装燃烧器结构的方法

    公开(公告)号：US20140137536A1

    公开(公告)日：2014-05-22

    申请号：US13682965

    申请日：2012-11-21

    申请人： GENERAL ELECTRIC COMPANY

    发明人： Joel Russell Cloninger ,  Patrick Benedict Melton ,  Lucas John Stoia ,  James Harold Westmoreland

    IPC分类号： F23R3/48

    CPC分类号： F23R3/48

    摘要： A super-telescoping cross-fire tube includes a cross-fire tube including a first portion and a second portion in mating engagement, the cross-fire tube extending from a first end region to a second end region for fluidly connecting a combustor chamber and an adjacent combustor chamber. Also included is an outer shield spaced radially outwardly and surrounding at least a portion of the cross-fire tube. Further included is a spring extending from proximate the first end region to the second end region and disposed between the cross-fire tube and the outer shield, wherein the cross-fire tube is telescopingly moveable between a first position and a second position.

    摘要翻译： 超伸缩式横火管包括交叉火管，其包括配合接合的第一部分和第二部分，所述交叉火焰管从第一端部区域延伸到第二端部区域，用于流体连接燃烧室和 相邻的燃烧室。 还包括外部屏蔽件，其径向向外隔开并且围绕交叉火管的至少一部分。 还包括从靠近第一端部区域延伸到第二端部区域并且设置在交叉火焰管和外部护罩之间的弹簧，其中交叉火焰管可在第一位置和第二位置之间伸缩移动。

    COMBUSTOR ASSEMBLY
    10.
    发明申请
    COMBUSTOR ASSEMBLY 有权
    燃烧器总成

    公开(公告)号：US20140123619A1

    公开(公告)日：2014-05-08

    申请号：US13672248

    申请日：2012-11-08

    申请人： GENERAL ELECTRIC COMPANY

    发明人： Richard Martin DiCintio

    IPC分类号： F23R3/48 ,  B23P11/00 ,  F23R3/60

    CPC分类号： F23R3/48 ,  F16L37/088 ,  F23C6/02 ,  F23R3/60 ,  Y10T29/49323

    摘要： According to one aspect of the invention, a combustor assembly for a pair of adjacent combustors includes a first passage formed in a liner of a first combustor and a flow sleeve disposed outside the liner of the first combustor, wherein the flow sleeve includes a window and a second passage aligned with the first passage. The assembly also includes a cross-fire tube disposed in the first passage to provide fluid communication between the first combustor and a second combustor and a retention clip disposed through the window to urge the cross-fire tube against an outer surface of the liner to enable the cross-fire tube to receive fluid through the first passage.

    摘要翻译： 根据本发明的一个方面，用于一对相邻的燃烧器的燃烧器组件包括形成在第一燃烧器的衬套中的第一通道和设置在第一燃烧器的衬套外部的流动套筒，其中流动套筒包括窗口和 与第一通道对准的第二通道。 组件还包括布置在第一通道中的交叉火管，以在第一燃烧器和第二燃烧器之间提供流体连通，以及通过窗口设置的保持夹，以将交叉火管推压到衬套的外表面上以使得能够 交叉火焰管通过第一通道接收流体。