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1. 发明授权

US08387397B2 Flow conditioner for use in gas turbine component in which combustion occurs 失效
标题翻译：用于燃烧发生的燃气轮机部件的流量调节器
公开(公告)号：US08387397B2
公开(公告)日：2013-03-05
申请号：US12360490
申请日：2009-01-27
申请人： Wei Chen , Ronald James Chila , Eric William King
发明人： Wei Chen , Ronald James Chila , Eric William King
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/06 , F23R2900/03045
摘要： A gas turbine component in which combustion occurs. The gas turbine component includes a liner, including a first surface facing a first space and a second surface facing a second space, the liner being interposed between the first and second spaces and having a through-hole defined therein extending from the first to the second surface by which incoming flows proceed from the first space and to the second space. At least the first surface is formed to flow condition the incoming flows to resist separating from sidewalls of the through-hole.
摘要翻译：燃烧发生的燃气轮机部件。所述燃气涡轮机部件包括衬套，所述衬套包括面对第一空间的第一表面和面向第二空间的第二表面，所述衬垫插入在所述第一和第二空间之间，并且具有限定在其中的通孔，所述通孔从所述第一空间延伸到第二空间输入流从第一空间和第二空间进入的表面。至少第一表面形成为使进入的流动流动以抵抗与通孔的侧壁分离。

2. 发明申请

US20100186416A1 FLOW CONDITIONER FOR USE IN GAS TURBINE COMPONENT IN WHICH COMBUSTION OCCURS 失效
标题翻译：用于燃气燃烧的燃气涡轮机组件中的流量调节器
公开(公告)号：US20100186416A1
公开(公告)日：2010-07-29
申请号：US12360490
申请日：2009-01-27
申请人： Wei Chen , Ronald James Chila , Eric William King
发明人： Wei Chen , Ronald James Chila , Eric William King
IPC分类号： F23R3/42
CPC分类号： F23R3/06 , F23R2900/03045
摘要： A gas turbine component in which combustion occurs. The gas turbine component includes a liner, including a first surface facing a first space and a second surface facing a second space, the liner being interposed between the first and second spaces and having a through-hole defined therein extending from the first to the second surface by which incoming flows proceed from the first space and to the second space. At least the first surface is formed to flow condition the incoming flows to resist separating from sidewalls of the through-hole.
摘要翻译：燃烧发生的燃气轮机部件。所述燃气涡轮机部件包括衬套，所述衬套包括面对第一空间的第一表面和面向第二空间的第二表面，所述衬垫插入在所述第一和第二空间之间，并且具有限定在其中的通孔，所述通孔从所述第一空间延伸到第二空间输入流从第一空间和第二空间进入的表面。至少第一表面形成为使进入的流动流动以抵抗与通孔的侧壁分离。

3. 发明申请

US20100005804A1 COMBUSTOR STRUCTURE 审中-公开
标题翻译： COMBUSTOR结构
公开(公告)号：US20100005804A1
公开(公告)日：2010-01-14
申请号：US12171386
申请日：2008-07-11
申请人： Wei Chen , David Martin Johnson , Ronald James Chila , Joseph Citeno
发明人： Wei Chen , David Martin Johnson , Ronald James Chila , Joseph Citeno
IPC分类号： F02C1/00
CPC分类号： F23R3/16 , F01D9/023 , F23R3/002 , F23R2900/00014 , F23R2900/03044
摘要： A combustor includes at least one combustor liner defining a combustion chamber capable of directing combustion products toward a turbine. At least one combustor sleeve is located outside of the combustion chamber and is capable of reducing a magnitude of acoustic waves in the combustion chamber. The at least one combustor liner and the at least one combustor sleeve define at least one flow channel therebetween. Further, a combustor includes at least one combustor liner defining a combustion chamber capable of directing combustion products toward turbomachinery. At least one combustor sleeve disposed outside of the combustion chamber and is capable of controlling distribution of fluid flow in the combustor to modify a uniformity of the fluid flow to the combustion chamber.
摘要翻译：燃烧器包括限定燃烧室的至少一个燃烧器衬套，其能够将燃烧产物引向涡轮。至少一个燃烧器套筒位于燃烧室的外部，并且能够减小燃烧室中的声波的大小。所述至少一个燃烧器衬套和所述至少一个燃烧器套筒在其间限定至少一个流动通道。此外，燃烧器包括限定能够将燃烧产物引导到涡轮机械的燃烧室的至少一个燃烧器衬套。至少一个燃烧器套筒设置在燃烧室的外部，并且能够控制燃烧器中的流体流动的分布，以改变流向燃烧室的流体的均匀性。

4. 发明授权

US08887508B2 Impingement sleeve and methods for designing and forming impingement sleeve 有权
标题翻译：冲击套筒和冲击套管的设计和成型方法
公开(公告)号：US08887508B2
公开(公告)日：2014-11-18
申请号：US13048394
申请日：2011-03-15
申请人： Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar , Matthew Paul Berkebile , Wei Chen , John Drake Vanselow
发明人： Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar , Matthew Paul Berkebile , Wei Chen , John Drake Vanselow
IPC分类号： F23R3/06 , F01D9/02
CPC分类号： F01D9/023 , F05D2260/201 , F23R2900/03044 , Y10T29/49229
摘要： An impingement sleeve and methods for designing and forming an impingement sleeve are disclosed. In one embodiment, a method for designing an impingement sleeve is disclosed. The method includes determining a desired operational value for a transition piece, inputting a combustor characteristic into a processor, and utilizing the combustor characteristic in the processor to determine a cooling hole pattern for the impingement sleeve, the cooling hole pattern comprising a plurality of cooling holes, at least a portion of the plurality of cooling holes being generally longitudinally asymmetric, the cooling hole pattern providing the desired operational value.
摘要翻译：公开了一种冲击套筒和用于设计和形成冲击套筒的方法。在一个实施例中，公开了一种用于设计冲击套筒的方法。该方法包括确定过渡件的期望操作值，将燃烧器特性输入到处理器中，以及利用处理器中的燃烧器特性来确定冲击套筒的冷却孔图案，冷却孔图案包括多个冷却孔所述多个冷却孔的至少一部分大致纵向不对称，所述冷却孔图案提供期望的操作值。

5. 发明申请

US20120304659A1 IMPINGEMENT SLEEVE AND METHODS FOR DESIGNING AND FORMING IMPINGEMENT SLEEVE 有权
标题翻译： IMPINGEMENT SLEEVE AND METHODS FOR DESIGN AND FORMING IMPINGEMENT SLEEVE
公开(公告)号：US20120304659A1
公开(公告)日：2012-12-06
申请号：US13589375
申请日：2012-08-20
申请人： Matthew Paul Berkebile , Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar , Wei Chen , John Drake Vanselow
发明人： Matthew Paul Berkebile , Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar , Wei Chen , John Drake Vanselow
IPC分类号： F23R3/02 , G06F17/50 , F02C7/12
CPC分类号： F01D9/023 , F05D2260/201 , F23R3/06 , F23R2900/03044
摘要： An impingement sleeve and methods for designing and forming an impingement sleeve are disclosed. In one embodiment, the impingement sleeve includes a body configured to at least partially surround a transition piece of the combustor. The impingement sleeve further includes a plurality of cooling holes defined in the body, the plurality of cooling holes having a cooling hole pattern configured to provide a desired operational value for the transition piece. At least one of the plurality of cooling holes has a chamfer extending at least partially between an inlet and an outlet of the at least one of the plurality of cooling holes. At least a portion of the plurality of cooling holes are generally longitudinally asymmetric.
摘要翻译：公开了一种冲击套筒和用于设计和形成冲击套筒的方法。在一个实施例中，冲击套筒包括构造成至少部分地围绕燃烧器的过渡件的主体。所述冲击套筒还包括限定在所述主体中的多个冷却孔，所述多个冷却孔具有冷却孔图案，所述冷却孔图案被配置为为所述过渡件提供期望的操作值。多个冷却孔中的至少一个具有至少部分地在所述多个冷却孔中的至少一个冷却孔的入口和出口之间延伸的倒角。多个冷却孔的至少一部分大体上是纵向不对称的。

6. 发明授权

US09249679B2 Impingement sleeve and methods for designing and forming impingement sleeve 有权
标题翻译：冲击套筒和冲击套管的设计和成型方法
公开(公告)号：US09249679B2
公开(公告)日：2016-02-02
申请号：US13589375
申请日：2012-08-20
申请人： Matthew Paul Berkebile , Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar , Wei Chen , John Drake Vanselow
发明人： Matthew Paul Berkebile , Jerome David Brown , Ronald James Chila , Patrick Benedict Melton , Russell DeForest , David William Cihlar , Wei Chen , John Drake Vanselow
IPC分类号： F23R3/06 , F01D9/02
CPC分类号： F01D9/023 , F05D2260/201 , F23R3/06 , F23R2900/03044
摘要： An impingement sleeve and methods for designing and forming an impingement sleeve are disclosed. In one embodiment, the impingement sleeve includes a body configured to at least partially surround a transition piece of the combustor. The impingement sleeve further includes a plurality of cooling holes defined in the body, the plurality of cooling holes having a cooling hole pattern configured to provide a desired operational value for the transition piece. At least one of the plurality of cooling holes has a chamfer extending at least partially between an inlet and an outlet of the at least one of the plurality of cooling holes. At least a portion of the plurality of cooling holes are generally longitudinally asymmetric.
摘要翻译：公开了一种冲击套筒和用于设计和形成冲击套筒的方法。在一个实施例中，冲击套筒包括构造成至少部分地围绕燃烧器的过渡件的主体。所述冲击套筒还包括限定在所述主体中的多个冷却孔，所述多个冷却孔具有冷却孔图案，所述冷却孔图案被配置为为所述过渡件提供期望的操作值。多个冷却孔中的至少一个具有至少部分地在所述多个冷却孔中的至少一个冷却孔的入口和出口之间延伸的倒角。多个冷却孔的至少一部分大体上是纵向不对称的。

7. 发明申请

US20130236301A1 Apparatus And System For Directing Hot Gas 审中-公开
标题翻译：用于引导热气的设备和系统
公开(公告)号：US20130236301A1
公开(公告)日：2013-09-12
申请号：US13416559
申请日：2012-03-09
申请人： Wei Chen , Stacy Ann Holzman , Keith Cletus Belsom , Ronald James Chila , Richard Martin DiCintio
发明人： Wei Chen , Stacy Ann Holzman , Keith Cletus Belsom , Ronald James Chila , Richard Martin DiCintio
IPC分类号： F01D1/04 , F02C7/12 , F04D29/54
CPC分类号： F01D9/023 , F23R3/46
摘要： Disclosed herein are apparatuses and systems for directing the flow of hot gas exiting a transition piece. In an embodiment, an aft frame an aft frame has an exit face that has an airfoil shape. In an embodiment, a transition piece aft exit has an airfoil shape.
摘要翻译：这里公开了用于引导离开过渡件的热气流的装置和系统。在一个实施例中，后框架具有具有翼型形状的出口面。在一个实施例中，过渡件后出口具有翼型形状。

8. 发明授权

US08646276B2 Combustor assembly for a turbine engine with enhanced cooling 有权
标题翻译：用于具有增强冷却的涡轮发动机的燃烧器组件
公开(公告)号：US08646276B2
公开(公告)日：2014-02-11
申请号：US12616304
申请日：2009-11-11
申请人： Lewis Berkley Davis, Jr. , Ronald James Chila
发明人： Lewis Berkley Davis, Jr. , Ronald James Chila
IPC分类号： F02C1/00
CPC分类号： F23R3/005 , F23R3/06 , F23R3/54 , F23R2900/03043 , F23R2900/03044
摘要： A combustor assembly for a turbine engine includes a combustor liner and a flow sleeve which surrounds the combustor liner. Compressed air flows through an annular space located between an outer surface of the combustor liner and an inner surface of the flow sleeve. A plurality of cooling holes are formed through the flow sleeve to allow compressed air to flow from a position outside the flow sleeve, through the cooling holes, and into the annular space. The height of the annular space may vary along the length of the combustor assembly. Thus, the flow sleeve may have reduced diameter portions which result in the height of the annular space being smaller in certain locations than at other locations along the length of the combustor assembly.
摘要翻译：用于涡轮发动机的燃烧器组件包括燃烧器衬套和围绕燃烧器衬套的流动套管。压缩空气流过位于燃烧器衬套的外表面和流动套管的内表面之间的环形空间。通过流动套筒形成多个冷却孔，以允许压缩空气从流动套筒外部的位置流过冷却孔并进入环形空间。环形空间的高度可以沿着燃烧器组件的长度而变化。因此，流动套管可以具有减小的直径部分，这导致环形空间的高度在某些位置比沿着燃烧器组件的长度的其它位置更小。

9. 发明申请

US20130086915A1 FILM COOLED COMBUSTION LINER ASSEMBLY 审中-公开
标题翻译：薄膜冷却燃料内衬组件
公开(公告)号：US20130086915A1
公开(公告)日：2013-04-11
申请号：US13267994
申请日：2011-10-07
申请人： David William Cihlar , Ronald James Chila , Patrick Benedict Melton , William David York
发明人： David William Cihlar , Ronald James Chila , Patrick Benedict Melton , William David York
IPC分类号： F02C7/18
CPC分类号： F23R3/002 , F01D9/023 , F05D2240/55 , F23R3/06 , F23R3/46 , F23R2900/00012 , F23R2900/03042 , F23R2900/03044
摘要： A combustion liner assembly is provided and includes a combustion liner and a transition piece. A portion of the transition piece is circumferentially disposed around a portion of the combustion liner. A seal is attached to the transition piece, and the seal is configured to apply a compressive force to an aft end of the combustion liner.
摘要翻译：提供燃烧衬套组件并且包括燃烧衬套和过渡件。过渡件的一部分周向地布置在燃烧衬套的一部分周围。密封件附接到过渡件，并且密封件构造成对燃烧衬套的后端施加压缩力。

10. 发明授权

US08359867B2 Combustor having a flow sleeve 有权
标题翻译：具有流动套筒的燃烧器
公开(公告)号：US08359867B2
公开(公告)日：2013-01-29
申请号：US12756329
申请日：2010-04-08
申请人： Ronald James Chila , Martin Ronald Watts , Sheng-Yi Wu
发明人： Ronald James Chila , Martin Ronald Watts , Sheng-Yi Wu
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/02 , F23R3/44 , F23R2900/03043
摘要： A combustor is provided and includes a liner through which fluid fed from at least two injection points flows from a head end to an interior of a transition piece, a first one of the at least two injection points being axially proximate to a fluid impenetrable coupling between the liner and the transition piece and defining apertures disposed in fluid communication with a first passage leading to the head end, and a second one of the at least two injection points being disposed axially between the apertures and the head end and upstream from the apertures relative to a direction of fluid flow through the first passage, the second one of the at least two injection points being formed of openings disposed in fluid communication with a second passage leading to the head end.
摘要翻译：提供燃烧器并且包括衬套，通过所述衬套从至少两个注射点供给的流体从头端流动到过渡件的内部，所述至少两个注射点中的第一个轴向靠近液体不可穿透的联接所述衬套和所述过渡件并且限定出孔设置成与通向所述头端的第一通道流体连通，并且所述至少两个注射点中的第二个注射点轴向地设置在所述孔和所述头部端部之间以及所述孔的相对上游流体流过第一通道的方向，所述至少两个注射点中的第二个注射点由与通向头端的第二通道流体连通的开口形成。

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