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1.发明授权Apparatus and methods for minimizing and/or eliminating dilution air leakage in a combustion liner assembly 有权用于最小化和/或消除燃烧衬套组件中的稀释空气泄漏的装置和方法公开(公告)号：US06951109B2
公开(公告)日：2005-10-04
申请号：US10751541
申请日：2004-01-06
CPC分类号： F23R3/42 , F23R3/002 , Y10T29/49346
摘要： Variations in dilution air leakage paths in a gas turbine combustion liner assembly are minimized or eliminated to reduce emissions and variations in emissions from combustor to combustor. Leakage paths between the liner sleeve and venturi outer liner are minimized by using additional rivets at that joint. The leakage paths between the outer and inner sleeves of the venturi are eliminated by applying a peripheral weld to the end edges of the flanges of the outer and inner sleeves. The leakage paths between the venturi and outer liner are minimized while simultaneously maintaining accurate venturi throat area relative to the cap centerbody by match drilling holes through the liner sleeve and the overlapped flanges of the venturi and followed by riveting the parts together.
摘要翻译： 在燃气轮机燃烧衬套组件中的稀释空气泄漏路径的变化被最小化或消除，以减少从燃烧器到燃烧器的排放和排放变化。 通过在该接头处使用额外的铆钉，使衬套和文氏管外衬套之间的泄漏路径最小化。 通过向外套筒和内套管的凸缘的端部边缘施加周边焊缝来消除文丘里管的外套筒和内套筒之间的泄漏路径。 文丘里管和外衬套之间的泄漏路径最小化，同时通过匹配钻孔穿过衬套套管和文丘里管的重叠凸缘，同时将零件铆接在一起，同时保持精确的文氏管喉部区域相对于盖中心体。
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公开(公告)号：US20120088201A1
公开(公告)日：2012-04-12
申请号：US12898887
申请日：2010-10-06
IPC分类号： F23D14/46
CPC分类号： F23R3/28 , F23R3/14 , F23R2900/00016
摘要： A combustor nozzle includes a nozzle body that defines a cavity. An orifice in the nozzle body provides fluid communication from the cavity through the nozzle body. A movable barrier proximate to the orifice has a first position in which the movable barrier at least partially obstructs the orifice. A method for supplying fuel to a combustor includes flowing fuel through an orifice in a nozzle, determining a reactivity of the fuel, and adjusting an effective cross sectional area of the orifice based on the reactivity of the fuel.
摘要翻译： 燃烧器喷嘴包括限定空腔的喷嘴体。 喷嘴主体中的孔口提供从腔体到喷嘴体的流体连通。 靠近孔口的可动挡板具有第一位置，在该第一位置中，可动挡板至少部分地阻塞孔口。 用于向燃烧器供应燃料的方法包括使燃料通过喷嘴中的孔流动，确定燃料的反应性，并且基于燃料的反应性调节孔口的有效横截面面积。
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3.发明授权Hula seal with preferential cooling having spring fingers and/or adjacent slots with different widths 有权具有弹簧指和/或具有不同宽度的相邻槽的优先冷却的呼啦密封公开(公告)号：US08695351B2
公开(公告)日：2014-04-15
申请号：US13101641
申请日：2011-05-05
CPC分类号： F01D9/023 , F16J15/0887
摘要： An annular seal for use between coupled combustor components includes a segmented annular solid edge portion and a plurality of alternating spring fingers and slots extending from the solid edge portion and arranged about a circumference of the solid edge portion, wherein one or more of the plurality of spring fingers or one or more of the plurality of straight and angled slots have non-uniform width dimensions.
摘要翻译： 在连接的燃烧器部件之间使用的环形密封件包括分段的环形实心边缘部分和多个交替的弹簧指状物和从实心边缘部分延伸并围绕实心边缘部分的圆周布置的槽，其中多个 弹簧手指或多个直的和倾斜的狭槽中的一个或多个具有不均匀的宽度尺寸。
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4.发明授权Apparatus and systems relating to fuel injectors and fuel passages in gas turbine engines 有权与燃气涡轮发动机中的燃料喷射器和燃料通道相关的装置和系统公开(公告)号：US08919125B2
公开(公告)日：2014-12-30
申请号：US13176784
申请日：2011-07-06
摘要： A combustor casing fuel injector in a combustor of a combustion turbine engine, the combustor including a combustor casing that encloses internal structure of the combustor, wherein the combustor casing fuel injector includes a fuel manifold adjacent to an outer surface of the combustor casing. In certain embodiments, the combustor casing fuel injector includes a fuel injector; wherein the fuel injector extends through the combustor casing from a position within the fuel manifold to a predetermined fuel injection location; and wherein the fuel injector includes a protruding injector inlet within the fuel manifold.
摘要翻译： 在燃烧涡轮发动机的燃烧器中的燃烧器壳体燃料喷射器，所述燃烧器包括包围燃烧器的内部结构的燃烧器壳体，其中燃烧器壳体燃料喷射器包括邻近燃烧器壳体的外表面的燃料歧管。 在某些实施例中，燃烧器壳体燃料喷射器包括燃料喷射器; 其中所述燃料喷射器通过所述燃烧器壳体从所述燃料歧管内的位置延伸到预定的燃料喷射位置; 并且其中所述燃料喷射器包括在所述燃料歧管内的突出的喷射器入口。
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5.发明授权Gas turbine combustor endcover assembly with integrated flow restrictor and manifold seal 有权具有集成流量限制器和歧管密封件的燃气轮机燃烧器整流器组件公开(公告)号：US08820086B2
公开(公告)日：2014-09-02
申请号：US13008399
申请日：2011-01-18
IPC分类号： F02C1/00
CPC分类号： F23R3/283 , F23K5/14 , F23K2900/05142 , F23R2900/00005 , F23R2900/00012
摘要： An endcover assembly for a turbine combustor adapted to support one or more combustor nozzles includes a substantially flat plate having one side which in use, faces a combustion chamber and an opposite side which, in use, faces away from the combustion chamber. At least one fuel passage extends through the substantially flat plate. A fuel manifold porting block is secured to the opposite side of the flat plate with at least one port aligned with the at least one passage. A fuel restrictor insert formed with multiple flow orifices is located between the flat plate and the fuel manifold porting block in alignment with the at least one fuel passage and the at least one port.
摘要翻译： 适于支撑一个或多个燃烧器喷嘴的用于涡轮机燃烧器的封盖组件包括基本平坦的板，其具有一个侧面，其在使用中面向燃烧室，在使用中相对侧面远离燃烧室。 至少一个燃料通道延伸穿过基本平坦的板。 燃料歧管移动块被固定到平板的相对侧，其中至少一个端口与至少一个通道对准。 形成有多个流动孔的燃料限制器插件位于平板和燃料歧管移动块之间，与至少一个燃料通道和至少一个端口对准。
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6.发明授权公开(公告)号：US08646277B2
公开(公告)日：2014-02-11
申请号：US12708736
申请日：2010-02-19
CPC分类号： F23R3/002 , F02K1/82 , F02K9/346 , F23R3/06 , F23R2900/03043 , F23R2900/03045
摘要： A combustor liner for a combustor of a turbine engine includes a single-walled generally cylindrical liner that extends from a head end to an aft end. A venturi is formed on the combustor liner at a location between the head and aft ends. The venturi is formed by first and second straight portions of the combustor liner that angle inward to form a reduced diameter portion. The combustor liner may also include an air deflector to deflect air down onto the exterior of the reduced diameter portion of the single-walled combustor liner. The combustor liner may also include dilution holes, and turbulator rings.
摘要翻译： 用于涡轮发动机的燃烧器的燃烧器衬套包括从头端延伸到后端的单壁大体圆柱形衬套。 在头部和后端之间的位置处，在燃烧器衬套上形成文丘里管。 文丘里管由燃烧器衬套的第一和第二直线部分形成，向内倾斜以形成直径减小的部分。 燃烧器衬套还可以包括空气导流板，以将空气向下偏转到单壁燃烧器衬套的直径减小的部分的外部。 燃烧器衬套也可以包括稀释孔和湍流环。
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公开(公告)号：US20130227964A1
公开(公告)日：2013-09-05
申请号：US13410417
申请日：2012-03-02
申请人： Christopher Paul Willis , William Lawrence Byrne , David William Cihlar , Donald Timothy Lemon , Patrick Benedict Melton
发明人： Christopher Paul Willis , William Lawrence Byrne , David William Cihlar , Donald Timothy Lemon , Patrick Benedict Melton
CPC分类号： F01D9/023
摘要： A transition piece aft frame assembly is provided, and includes a transition piece aft frame and a heat shield. The transition piece aft frame has an aft face. At least a portion of the aft face is exposed to an exhaust gas stream. The heat shield is connected to the transition piece aft frame. The heat shield is oriented to generally deflect the exhaust gas stream away from the aft face of the transition piece aft frame.
摘要翻译： 提供过渡件后框架组件，并且包括过渡件后框架和隔热罩。 过渡件后框架有一个后面。 后表面的至少一部分暴露于排气流。 隔热罩与过渡件后框架连接。 隔热罩被定向成使废气流大致偏离过渡件后框架的后表面。
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公开(公告)号：US09010127B2
公开(公告)日：2015-04-21
申请号：US13410417
申请日：2012-03-02
申请人： Christopher Paul Willis , William Lawrence Byrne , David William Cihlar , Donald Timothy Lemon , Patrick Benedict Melton
发明人： Christopher Paul Willis , William Lawrence Byrne , David William Cihlar , Donald Timothy Lemon , Patrick Benedict Melton
CPC分类号： F01D9/023
摘要： A transition piece aft frame assembly is provided, and includes a transition piece aft frame and a heat shield. The transition piece aft frame has an aft face. At least a portion of the aft face is exposed to an exhaust gas stream. The heat shield is connected to the transition piece aft frame. The heat shield is oriented to generally deflect the exhaust gas stream away from the aft face of the transition piece aft frame.
摘要翻译： 提供过渡件后框架组件，并且包括过渡件后框架和隔热罩。 过渡件后框架有一个后面。 后表面的至少一部分暴露于排气流。 隔热罩与过渡件后框架连接。 隔热罩被定向成使废气流大致偏离过渡件后框架的后表面。
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9.发明申请APPARATUS AND SYSTEMS RELATING TO FUEL INJECTORS AND FUEL PASSAGES IN GAS TURBINE ENGINES 有权与燃油喷射器相关的装置和系统以及燃油涡轮发动机中的燃油通道公开(公告)号：US20130008169A1
公开(公告)日：2013-01-10
申请号：US13176784
申请日：2011-07-06
IPC分类号： F02C7/22
摘要： A combustor casing fuel injector in a combustor of a combustion turbine engine, the combustor including a combustor casing that encloses internal structure of the combustor, wherein the combustor casing fuel injector includes a fuel manifold adjacent to an outer surface of the combustor casing. In certain embodiments, the combustor casing fuel injector includes a fuel injector; wherein the fuel injector extends through the combustor casing from a position within the fuel manifold to a predetermined fuel injection location; and wherein the fuel injector includes a protruding injector inlet within the fuel manifold.
摘要翻译： 在燃烧涡轮发动机的燃烧器中的燃烧器壳体燃料喷射器，所述燃烧器包括包围燃烧器的内部结构的燃烧器壳体，其中燃烧器壳体燃料喷射器包括邻近燃烧器壳体的外表面的燃料歧管。 在某些实施例中，燃烧器壳体燃料喷射器包括燃料喷射器; 其中所述燃料喷射器通过所述燃烧器壳体从所述燃料歧管内的位置延伸到预定的燃料喷射位置; 并且其中所述燃料喷射器包括在所述燃料歧管内的突出的喷射器入口。
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公开(公告)号：US07134287B2
公开(公告)日：2006-11-14
申请号：US10615776
申请日：2003-07-10
申请人： Keith Cletus Belsom , Larry Lou Thomas , Donald Timothy Lemon , Bradley Donald Crawley , Matthew Eugene Roberts , David Kevin Spikings
发明人： Keith Cletus Belsom , Larry Lou Thomas , Donald Timothy Lemon , Bradley Donald Crawley , Matthew Eugene Roberts , David Kevin Spikings
IPC分类号： F02C7/20
CPC分类号： F23R3/60
摘要： The endcover assembly for a combustor includes an endcover having an aperture, an insert disposed in the stepped bore opening through an internal face of the endcover, a fuel cartridge extending through the insert and aperture and a seal cover on the external face of the endcover. Seal cover/endcover annular seals are disposed in registering axial cavities to seal against fluid leakage externally of the endcover assembly. Generally C-shaped and W-shaped seals are disposed in the cavities between the stepped shoulders of the insert and aperture to seal against leakage through the internal face of the endcover. The seals maintain sealing engagement during assembly and thermal distortion during turbine usage.
摘要翻译： 用于燃烧器的封盖组件包括具有开口的端盖，通过端盖的内表面设置在阶梯式孔开口中的插入件，延伸穿过插入件和孔的燃料盒以及在封盖的外表面上的密封盖。 密封盖/端盖环形密封件设置成对准轴向空腔以密封外罩组件的流体泄漏。 通常，C形和W形密封件设置在插入件的阶梯状肩部和孔之间的空腔中，以防止通过内罩的内表面泄漏。 涡轮机使用期间，密封件在组装和热变形期间保持密封接合。
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