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105 条记录 (耗时 0.012 秒)

    Flame-passage device for non-annular gas turbine combustion chambers
    11.
    发明授权
    Flame-passage device for non-annular gas turbine combustion chambers 失效

    公开(公告)号：US06834491B2

    公开(公告)日：2004-12-28

    申请号：US10296709

    申请日：2003-03-28

    申请人： Alessandro Coppola

    发明人： Alessandro Coppola

    IPC分类号： F02C300

    CPC分类号： F23R3/60 ,  F23R3/48

    摘要： A flame-passage device (10) for non-annular gas turbine combustion chambers comprises a tubular body (11), which is provided with a plurality of cooling holes (12), for cooling on the swirl-cooling type. The tubular body (11) is inserted in a flanged pipe (27), which connects the cases (31, 32) of two successive combustion chambers (17, 18), and has a first end (13) with a cylindrical shape, and a second end (14) with an oval shape, wherein the second, oval end (14) is provided with three rings (23, 24, 25), for anchorage of the corresponding combustion chamber (17) to the case (31).

    Combustion crossfire tube with integral soft chamber
    12.
    发明授权
    Combustion crossfire tube with integral soft chamber 失效
    具有整体软室的燃烧交叉管

    公开(公告)号：US06334294B1

    公开(公告)日：2002-01-01

    申请号：US09571834

    申请日：2000-05-16

    申请人： Keith Cletus Belsom ,  Marshalla Michelle Wright

    发明人： Keith Cletus Belsom ,  Marshalla Michelle Wright

    IPC分类号： F02C1310

    CPC分类号： F23R3/48

    摘要： A crossfire tube for connecting adjacent combustors in a gas turbine, the crossfire tube includes a hollow tubular body having opposite end portions adapted to be secured to the adjacent combustors; an annular chamber surrounding a mid-section of the hollow tubular member; a first plurality of purge air feed holes in an outer wall of the chamber, and a second plurality of purge air feed holes in an inner wall of the chamber opening into the crossfire tube. A method of supplying purge air to a crossfire tube located between a pair of adjacent combustors in a gas turbine, where the crossfire tube includes a hollow tubular body adapted for connection between the adjacent combustors, includes the steps of establishing a chamber about the tubular body; utilizing compressor discharge air as crossfire tube purge air; feeding the purge air at a first pressure approximately equal to the compressor discharge air pressure into the chamber to thereby reduce the pressure to a second, lower pressure; and subsequently feeding the purge air from the chamber into the tubular body of the crossfire tube at the lower pressure.

    摘要翻译： 用于连接燃气轮机中的相邻燃烧器的交叉火管，交火管包括中空管状体，其具有适于固定到相邻燃烧器的相对端部; 围绕所述中空管状构件的中间部分的环形室; 在室的外壁中的第一组多个吹扫空气供给孔和在通入交火管的室的内壁中的第二多个吹扫空气供给孔。 向位于燃气轮机中的一对相邻燃烧器之间的交火管供应吹扫空气的方法，其中所述交火管包括适于在相邻燃烧器之间连接的中空管状体，所述中空管体包括以下步骤：围绕所述管状体 ; 利用压缩机排放空气作为交火管吹扫空气; 以大致等于压缩机排出空气压力的第一压力将净化空气供给到室中，从而将压力降低到第二较低压力; 随后将来自腔室的净化空气以较低的压力送入交火管的管状体。

    Low leakage, articulating fluid transfer tube
    13.
    发明授权
    Low leakage, articulating fluid transfer tube 失效
    低泄漏，关节流体输送管

    公开(公告)号：US5964250A

    公开(公告)日：1999-10-12

    申请号：US982003

    申请日：1997-12-01

    申请人： Peter W. Mueller

    发明人： Peter W. Mueller

    IPC分类号： F01D25/00 ,  F16L27/04 ,  F23R3/48 ,  F16L9/22

    CPC分类号： F23R3/48

    摘要： A transfer tube system includes a transfer tube, a spring, a pair of opposing seats, and a pair of end assemblies that provide independent axial spring loading of the opposing seats. The spring loading assures continuous sealing contact regardless of dynamic loading, dimensional stack-up, or geometry change resulting from interfaced wear. The transfer tube end assemblies include a spherical or conical seat for mating with the transfer tube. Particularly, the transfer tube has spherical ends for seating in the transfer tube end assembly seats. The conical/spherical seats permit angular motion of interfacing components without lift off and therefore assures minimal leakage.

    摘要翻译： 传送管系统包括传送管，弹簧，一对相对的座，以及提供相对座的独立轴向弹簧加载的一对端组件。 弹簧加载确保连续的密封接触，而不管动态载荷，尺寸叠加或由接口磨损引起的几何变化。 传送管端组件包括用于与传送管配合的球形或锥形座。 特别地，传送管具有用于放置在传送管端组件座中的球形端。 锥形/球形座允许接口部件的角运动，而不会脱落，因此确保最小的泄漏。

    Impingement cooled crossfire tube assembly in multiple-combustor gas turbine engine
    14.
    发明授权
    Impingement cooled crossfire tube assembly in multiple-combustor gas turbine engine 失效
    在多燃烧器燃气涡轮发动机中的冲击冷却交火管组件

    公开(公告)号：US5001896A

    公开(公告)日：1991-03-26

    申请号：US834073

    申请日：1986-02-26

    申请人： Milton B. Hilt ,  Lewis B. Davis, Jr.

    发明人： Milton B. Hilt ,  Lewis B. Davis, Jr.

    IPC分类号： F23R3/48

    CPC分类号： F23R3/48

    摘要： A crossfire tube assembly joining adjacent combustors in a gas turbine engine includes an impingement sleeve within which a crossfire tube is centrally disposed. The impingement sleeve is pierced by an array of impingement cooling holes which form a plurality of small jets of cooling air impinging upon, and cooling, the crossfire tube. The space between the impingement sleeve and the crossfire tube forms a flow channel along which the spent impingement air flows in the axial direction before exiting into the interiors of the combustors. A flow dam at the center of the flow channel forces the impingement air to flow toward the ends. An outward flare in a portions of the crossfire tube extending beyond the extremity of the impingement sleeve directs air exiting the flow channel upon an annular flange which supports the crossflow assembly and thus improves cooling in this area.

    摘要翻译： 连接在燃气涡轮发动机中的相邻燃烧器的交火管组件包括冲击套管，交火管在其中居中设置。 冲击套筒被冲击冷却孔的阵列刺穿，该冲击冷却孔形成多个小的喷射的冷却空气，其冲击并冷却交火管。 冲击套筒和交叉火管之间的空间形成了一个流动通道，消耗的冲击空气沿着该流动通道沿轴向流动，然后离开燃烧器的内部。 在流动通道中心的流动阻力件迫使冲击空气朝向端部流动。 交叉火管中延伸超过冲击套筒末端的部分中的向外的火炬引导离开流动通道的空气在支撑横流组件的环形凸缘上，从而改善该区域中的冷却。

    TOOL AND METHOD FOR DECOUPLING CROSS-FIRE TUBE ASSEMBLIES IN GAS TURBINE ENGINES
    18.
    发明申请
    TOOL AND METHOD FOR DECOUPLING CROSS-FIRE TUBE ASSEMBLIES IN GAS TURBINE ENGINES 审中-公开

    公开(公告)号：US20180100654A1

    公开(公告)日：2018-04-12

    申请号：US15289412

    申请日：2016-10-10

    申请人： General Electric Company

    发明人： Todd James Gattermeyer ,  James Robert Rodgers ,  Stuart Craig Hanson

    IPC分类号： F23R3/60

    CPC分类号： F23R3/60 ,  B25B27/023 ,  F23R3/48 ,  F23R2900/00017 ,  F23R2900/00019

    摘要： A tool for decoupling a telescoping tube from a first liner of a gas turbine engine is disclosed. The tool includes a rod partially positioned in a telescoping tube passage. The rod includes a first portion having a non-circular cross-section and a threaded second portion positioned in a second combustion chamber. A plug couples to the rod and engages a first side surface of the telescoping tube. A base defining a base passage extending therethrough is positioned in a second combustion chamber. The base passage includes a first portion having a non-circular cross-section. The first portion of the rod is at least partially positioned in the first portion of the base passage. A handle threadingly couples to the rod. Rotating the handle in a first direction moves the handle along the rod toward the first combustor to decouple the telescoping tube from the first liner.