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公开(公告)号：US20180085869A1
公开(公告)日：2018-03-29
申请号：US15278058
申请日：2016-09-28
CPC分类号： F23R3/48 , F01D9/023 , F01D25/285 , F05D2230/64 , F05D2230/70 , F05D2230/72 , F23R2900/00017 , F23R2900/00019
摘要： A tool kit for decoupling a telescoping tube from a first liner of a gas turbine engine is disclosed. The tool kit includes a base plate coupled to a combustor casing. A post extends outward from the base plate into a combustion chamber defined by the liner. A plunger slidably mounts to the post and is slidable between an extended position and a retracted position. A lever arm pivotably couples to the post and the plunger. Pivoting the lever arm in a first direction slides the plunger to the extended position to decouple the telescoping tube from the liner. A retaining clip couples to the combustor casing and extends into an annular plenum at least partially defined between the liner and the combustor casing. The retaining clip defines a notch that receives the telescoping tube after the plunger assembly decouples the telescoping tube from the liner.
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公开(公告)号：US20170059161A1
公开(公告)日：2017-03-02
申请号：US14836117
申请日：2015-08-26
CPC分类号： F23R3/16 , F02C6/06 , F02C6/08 , F02C7/12 , F02C7/18 , F02C9/18 , F05D2220/32 , F05D2240/35 , F05D2260/20 , F23C9/08 , F23C2900/09001 , F23R3/002 , F23R3/02 , F23R3/04 , F23R3/42 , F23R3/425 , F23R3/44 , F23R3/46 , F23R3/48 , F23R3/50 , F23R3/52 , F23R3/54 , F23R3/56 , F23R3/58
摘要： An air extraction port at a combustor of a gas turbine engine includes a port inlet at a combustor case of the combustor having an inlet area, a port outlet having a final area, and a fluid passage extending from the port inlet to the port outlet to convey an airflow, the port inlet sized and configured to extract the airflow from the combustor case at the same nominal upstream Mach number with a tolerance of +/−0.05.
摘要翻译： 燃气涡轮发动机的燃烧器处的空气抽出口包括在燃烧器壳体处的具有入口区域的端口入口，具有最终区域的端口出口和从端口入口延伸到端口出口的流体通道 传送气流，端口入口的尺寸和构造可以在相同标称上游马赫数处从燃烧器壳体提取气流，其公差为+/- 0.05。
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3.发明申请SERVICE-FRIENDLY CROSS FLAME TUBE WITH TWIST LOCK ATTACHMENT FOR CAN-ANNULAR GAS TURBINES 审中-公开服务友好的交叉火焰管，带有两个用于CAN-ANNULAR气体涡轮机的锁定连接公开(公告)号：US20160298853A1
公开(公告)日：2016-10-13
申请号：US14682294
申请日：2015-04-09
申请人： Siemens Energy, Inc.
发明人： Dustin C. Boudin , Leonel R. Leon
CPC分类号： F23R3/48 , F02C3/14 , F16L37/252 , F23R3/60
摘要： A twist lock attachment mechanism for attaching a cross flame tube to a cross flame tube port that is part of a combustor basket in a combustion section of a gas turbine engine, where the cross flame tube includes opposing flange sections coupled to an end of the cross flame tube and being spaced apart from each other. The attachment mechanism includes an annular collar mounted to the cross flame tube port and first and second spaced apart flange extensions mounted to the annular collar, where each flange extension includes a slot open at one end and blocked at an opposite end. The flange sections of the cross flame tube are positioned between the flange extensions so that the flange sections align with the slots, and the cross flame tube is rotated in a manner that causes the flange sections to slide into the slots.
摘要翻译： 一种用于将十字火焰管连接到十字火焰管口的扭转锁附接机构，所述交叉火焰管口是燃气轮机的燃烧部分中的燃烧器筐的一部分，其中所述十字火焰管包括联接到所述十字架的一端的相对的凸缘部分 火焰管并彼此间隔开。 附接机构包括安装到十字火焰管端口的环形轴环和安装到环形套环的第一和第二间隔开的凸缘延伸部，其中每个凸缘延伸部包括在一端开放并在相对端被阻挡的狭槽。 十字火焰管的凸缘部分位于凸缘延伸部之间，使得凸缘部分与狭槽对准，并且十字火焰管以使凸缘部分滑入槽中的方式旋转。
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公开(公告)号：US09400111B2
公开(公告)日：2016-07-26
申请号：US14158032
申请日：2014-01-17
CPC分类号： F23R3/06 , F23R3/005 , F23R3/48 , F23R2900/00014 , F23R2900/00017 , F23R2900/00018 , F23R2900/03043
摘要： A gas turbine combustor is disposed in a casing interior space of a gas turbine. A combustor basket of the combustor is formed into a cylindrical shape by abutting ends of a curved panel member and welding the ends together along a welding line 16. A communication tube is provided for communication between an interior space of the combustor basket and an interior space of a combustor basket of an adjacent combustor. The position of the welding line of the combustor basket coincides with a connection position for connecting the communication tube to the combustor basket. A cooling air hole is disposed in the communication tube or in the combustor basket in the vicinity of the communication tube to introduce cooling air from the casing interior space 9 to the interior of the combustor basket.
摘要翻译： 燃气轮机燃烧器设置在燃气轮机的壳体内部空间中。 燃烧器的燃烧器篮通过邻接曲面板构件的端部并沿着焊接线16将端部焊接在一起而形成为圆柱形的形状。连通管设置成用于在燃烧器筐的内部空间与内部空间 的相邻燃烧器的燃烧器筐。 燃烧器筐的焊接线的位置与用于将连通管连接到燃烧器筐的连接位置重合。 冷凝空气孔设置在连通管或连通管附近的燃烧器筐中，以将冷却空气从壳体内部空间9引入燃烧器筐的内部。
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公开(公告)号：US20160010868A1
公开(公告)日：2016-01-14
申请号：US14681410
申请日：2015-04-08
发明人： Donald E. Pinnick , Kevin M. Sauer , Russell N. Bennett , Bradley A. Lemke , Caleb Camara , Catherine Hidlebaugh , Katherine A. Dimon
摘要： Crossover tubes for use with cans of a turbine engine. The crossover tubes include an outer member, an inner member that is adapted to move collinearly with the outer member. The crossover tubes also include a pair of flanges and a biasing member positioned between the flanges.
摘要翻译： 用于涡轮发动机罐的交叉管。 交叉管包括外部构件，适于与外部构件共线地移动的内部构件。 交叉管还包括一对凸缘和位于凸缘之间的偏置构件。
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公开(公告)号：US20150260404A1
公开(公告)日：2015-09-17
申请号：US14432433
申请日：2013-09-30
发明人： Dennis J. Sullivan
CPC分类号： F23R3/005 , F23R3/002 , F23R3/007 , F23R3/10 , F23R3/48 , F23R3/50 , F23R2900/00012 , F23R2900/03042 , F23R2900/03044 , Y02T50/675
摘要： A combustor for a gas turbine engine includes an interface shield between a first heat shield and a second heat shield.
摘要翻译： 用于燃气涡轮发动机的燃烧器包括在第一隔热罩和第二隔热罩之间的接口屏蔽。
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公开(公告)号：US20150052910A1
公开(公告)日：2015-02-26
申请号：US13975109
申请日：2013-08-23
IPC分类号： F23R3/60
CPC分类号： F01D25/00 , B23P2700/13 , F01D5/288 , F01D9/023 , F01D19/00 , F01D21/003 , F05D2230/70 , F05D2230/72 , F23R3/48 , F23R2900/00019 , Y10T29/49229
摘要： The present disclosure relates to an apparatus having an elongated body configured to be inserted into a tubular structure extending between a first combustor and a second combustor of a gas turbine engine. A movable arm may be positioned proximate to a first end of the elongated body, and the movable arm may be configured to engage a surface of the first combustor when the elongated body is placed within the tubular structure. A drive member may be accessible near a second end of the elongated body, and the drive member may be configured to rotate within the elongated body and to drive the movable arm along a longitudinal axis of the elongated body toward the second end to separate the tubular structure from the second combustor.
摘要翻译： 本公开涉及一种具有细长主体的装置，其被配置为插入到在燃气涡轮发动机的第一燃烧器和第二燃烧器之间延伸的管状结构中。 可移动臂可以定位成靠近细长主体的第一端，并且当细长主体放置在管状结构内时，可动臂可以构造成与第一燃烧器的表面接合。 驱动构件可以在细长主体的第二端附近接近，并且驱动构件可构造成在细长主体内旋转并且沿着细长主体的纵向轴线朝向第二端驱动可动臂以分离管状 结构从第二燃烧器。
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公开(公告)号：US08955327B2
公开(公告)日：2015-02-17
申请号：US13210478
申请日：2011-08-16
CPC分类号： F23R3/286 , F23R3/48 , F23R2900/00002
摘要： A combustor includes a combustor wall defining a combustion zone and a fuel nozzle. The fuel nozzle includes a forward face, an aft face downstream from the forward face and adjacent to the combustion zone, a plurality of mixing tubes extending between the forward face and the aft face, an outer sleeve positioned radially outward of the plurality of mixing tubes, a heat shield positioned radially inward of the outer sleeve, and a baffle plate between the forward face and the aft face. At least one of the plurality of mixing tubes includes a sidewall that includes an injection opening defined therethrough. The baffle plate is oriented to channel fuel between the plurality of mixing tubes and between the baffle plate and the aft face prior to the fuel being channeled through the injection opening.
摘要翻译： 燃烧器包括限定燃烧区和燃料喷嘴的燃烧器壁。 燃料喷嘴包括前表面，从前表面下游并邻近燃烧区的后表面，在前表面和后表面之间延伸的多个混合管，位于多个混合管径向外侧的外套筒 ，位于外套筒径向内侧的隔热罩，以及在前表面和后表面之间的挡板。 所述多个混合管中的至少一个包括侧壁，所述侧壁包括通过其限定的注射开口。 在燃料被引导通过注射开口之前，挡板被定向成在多个混合管之间和挡板与后面之间引导燃料。
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公开(公告)号：US20140144122A1
公开(公告)日：2014-05-29
申请号：US13688625
申请日：2012-11-29
发明人： Brandon Taylor Overby , Keith Cletus Belsom , Jonathan Kay Allen , Kyle Eric Benson , Patrick Benedict Melton , Richard Martin DiCintio , Lucas John Stoia , Ronnie Ray Pentecost
IPC分类号： F23R3/48
CPC分类号： F23R3/48
摘要： A crossfire tube assembly between adjacent combustors includes a first sleeve adapted to provide fluid communication from a first combustor and a second sleeve adapted to connect to provide fluid communication from a second combustor. The second sleeve extends at least partially inside the first sleeve. A bias is between the first and second sleeves.
摘要翻译： 相邻燃烧器之间的交火管组件包括适于提供来自第一燃烧器和适于连接以提供来自第二燃烧器的流体连通的第一燃烧器和第二套管的流体连通的第一套筒。 第二套筒至少部分地在第一套筒内部延伸。 偏置在第一和第二袖之间。
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公开(公告)号：US08109099B2
公开(公告)日：2012-02-07
申请号：US12169994
申请日：2008-07-09
申请人： John S. Tu , Jaisukhlal V. Chokshi , Christopher R. Brdar , Randal G. McKinney , Shakira A. Ramos
发明人： John S. Tu , Jaisukhlal V. Chokshi , Christopher R. Brdar , Randal G. McKinney , Shakira A. Ramos
IPC分类号： F02C1/00
CPC分类号： F23R3/48 , F23R3/002 , F23R3/06 , F23R2900/03044
摘要： A combustion duct for a gas turbine engine has a combustion liner to receive products of combustion, and deliver the products of combustion downstream toward a turbine rotor. An outer housing is positioned radially outwardly of the combustion liner. A flow sleeve is positioned radially intermediate the outer housing and the combustion liner. A chamber radially outwardly of the flow sleeve receives cooling air. A plurality of holes through the flow sleeve deliver cooling air from the chamber against an outer periphery of the combustion liner. A plurality of tabs are associated with at least some of the holes in the flow sleeve. The tabs are positioned to extend radially inwardly on a downstream side of the holes.
摘要翻译： 用于燃气涡轮发动机的燃烧管具有燃烧衬套以接收燃烧产物，并将燃烧产物向下流向涡轮转子传送。 外壳体位于燃烧衬套的径向外侧。 流动套筒径向位于外壳体和燃烧衬套之间。 流动套管径向向外的腔容纳冷却空气。 穿过流动套管的多个孔将来自腔室的冷却空气传递到燃烧衬套的外周。 多个翼片与流动套筒中的至少一些孔相关联。 突片被定位成在孔的下游侧径向向内延伸。
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