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1. 发明申请

US20070113557A1 System for coupling flow from a centrifugal compressor to an axial combustor for gas turbines 有权
标题翻译：用于将来自离心压缩机的流动耦合到用于燃气轮机的轴向燃烧器的系统
公开(公告)号：US20070113557A1
公开(公告)日：2007-05-24
申请号：US11286102
申请日：2005-11-22
申请人： Jurgen Schumacher , Frank Zupanc , Paul Yankowich , Rodolphe Dudebout , Michael Barton
发明人： Jurgen Schumacher , Frank Zupanc , Paul Yankowich , Rodolphe Dudebout , Michael Barton
IPC分类号： F02C7/00
CPC分类号： F23R3/04 , F23R3/50
摘要： A system is provided for aerodynamically coupling air flow from a centrifugal compressor to an axial combustor. The system includes a diffuser, a deswirl assembly, combustor inner and outer annular liners, a combustor dome, and a curved annular plate. The diffuser has an inlet that communicates with the centrifugal compressor, an outlet, and a flow path that extends radially outward. The deswirl assembly has an inlet that communicates with the diffuser outlet to receive air flowing in a radially outward direction, an outlet, and a flow path configured to redirect the air in a radially inward and axial direction through the deswirl assembly outlet at an angle toward a longitudinal axis. The curved annular plate is coupled to combustor inner and outer annular liner upstream ends to form a combustor subplenum therebetween and has a first opening and a second opening formed therein, the first opening aligned with the deswirl assembly outlet to receive air discharged therefrom.
摘要翻译：提供了一种用于将来自离心式压缩机的空气动力耦合到轴向燃烧器的系统。该系统包括扩散器，去沫组件，燃烧器内部和外部环形衬垫，燃烧器圆顶和弯曲的环形板。扩散器具有与离心式压缩机，出口和径向向外延伸的流路连通的入口。洗涤组件具有与扩散器出口连通的入口，以接收沿径向向外的方向流动的空气，出口和流路，其配置成沿着径向向内和轴向方向将空气以一定的角度朝向脱水组件出口纵轴。弯曲的环形板联接到燃烧器的内部和外部环形衬套上游端，以在它们之间形成燃烧器子板，并且具有形成在其中的第一开口和第二开口，第一开口与脱水组件出口对准以接收从其排出的空气。

2. 发明申请

US20070169484A1 Segmented effusion cooled gas turbine engine combustor 有权
标题翻译：分段喷射冷却燃气轮机发动机燃烧器
公开(公告)号：US20070169484A1
公开(公告)日：2007-07-26
申请号：US11339439
申请日：2006-01-24
申请人： Jurgen Schumacher , Frank Zupanc , Rodolphe Dudebout
发明人： Jurgen Schumacher , Frank Zupanc , Rodolphe Dudebout
IPC分类号： F23R3/04
CPC分类号： F23R3/002 , F23R3/06 , F23R2900/03041 , Y02T50/675
摘要： A combustor includes two or more sets of effusion cooling holes that extend through the inner and outer liners. Each set of effusion cooling holes includes one or more initial rows of effusion cooling holes, one or more final rows of effusion cooling holes disposed downstream of the one or more initial rows, and a plurality of interposed rows of effusion cooling holes disposed between the initial and final rows. Each effusion cooling hole is disposed at a tangential angle relative to an axial line. The tangential angle of the effusion cooling holes in each set of effusion cooling holes gradually transitions from a substantially transverse tangential angle in each initial row to a substantially axial tangential angle in each final row.
摘要翻译：燃烧器包括两组或多组延伸穿过内衬和外衬的积液冷却孔。每套排出冷却孔包括一排或多排初始排出的冷却孔，设置在一个或多个初始行下游的一排或多排排出的冷却孔，以及设置在初始和最后一行。每个排出冷却孔相对于轴线设置成切线角。每组排出冷却孔中的排出冷却孔的切向角逐渐从每个初始行中的基本上横向的切向角逐渐转变到每个最后一行的基本轴向的切向角。

3. 发明申请

US20060272335A1 Advanced effusion cooling schemes for combustor domes 失效
公开(公告)号：US20060272335A1
公开(公告)日：2006-12-07
申请号：US11146595
申请日：2005-06-07
申请人： Jurgen Schumacher , Frank Zupanc , Rodolphe Dudebout
发明人： Jurgen Schumacher , Frank Zupanc , Rodolphe Dudebout
IPC分类号： F23R3/04
CPC分类号： F23R3/50 , F23R3/12 , Y02T50/675
摘要： A cooling scheme for a dome comprises an effusion array drilled directly through a single walled dome. In one embodiment, the layout of the holes comprises two regions, a region close to the fuel injector where the holes follow a tangential path around the injector, and a second region where the direction of the holes is radially outward from the injector axis. A film of cooling air may be applied on the interior side of the combustor dome via an air swirler, which projects air radially outward from the injector axis. The first series of cooling holes supplement this air supply so that cooling efficacy is extended along the dome surface and is directed in a counter-rotating manner with respect to the main air swirler. The second series of dome cooling holes infuse further cooling flux that reduces the temperature in the corner regions between fuel injectors.

4. 发明申请

US20070245710A1 Optimized configuration of a reverse flow combustion system for a gas turbine engine 审中-公开
标题翻译：用于燃气涡轮发动机的逆流燃烧系统的优化配置
公开(公告)号：US20070245710A1
公开(公告)日：2007-10-25
申请号：US11408662
申请日：2006-04-21
申请人： Jurgen Schumacher , Rodolphe Dudebout , Brad Bazzell
发明人： Jurgen Schumacher , Rodolphe Dudebout , Brad Bazzell
IPC分类号： F02K3/04
CPC分类号： F23R3/54 , F23R3/60
摘要： An apparatus is provided for a gas turbine engine. The gas turbine engine comprises a high pressure compressor, a single-stage high pressure turbine, a multi-stage low pressure turbine, and a reverse flow combustor unit. The reverse flow combustor comprises a combustor liner assembly, a combustor dome, and a plurality of straight-shafted fuel injectors. The combustor liner assembly includes an inner liner and an outer liner. The inner liner surrounds the single-stage high pressure turbine, and the outer liner is disposed radially outwardly of, and at least partially surrounding, the inner liner. The combustor dome assembly is coupled between the inner liner and the outer liner to define a combustion chamber therebetween. The plurality of straight-shafted fuel injectors are coupled to the combustor dome, with each fuel injector having at least an inlet, an outlet, and a linear fuel passageway extending therebetween.
摘要翻译：提供一种用于燃气涡轮发动机的装置。燃气涡轮发动机包括高压压缩机，单级高压涡轮机，多级低压涡轮机和逆流式燃烧器单元。逆流燃烧器包括燃烧器衬套组件，燃烧器穹顶和多个直轴式燃料喷射器。燃烧器衬套组件包括内衬和外衬。内衬层围绕单级高压涡轮机，并且外衬套设置在内衬层的径向外部并且至少部分地围绕内衬套。燃烧器穹顶组件联接在内衬和外衬套之间以在其间限定燃烧室。多个直轴式燃料喷射器联接到燃烧器穹顶，每个燃料喷射器至少具有在其间延伸的入口，出口和线性燃料通道。

5. 发明申请

US20070214791A1 Combustor dome assembly including retaining ring 失效
标题翻译：燃烧器圆顶组件包括固定环
公开(公告)号：US20070214791A1
公开(公告)日：2007-09-20
申请号：US11367282
申请日：2006-03-02
申请人： Jurgen Schumacher , Frank Zupanc , Paul Yankowich , Ronald Pardington
发明人： Jurgen Schumacher , Frank Zupanc , Paul Yankowich , Ronald Pardington
IPC分类号： F02C1/00 , F02C7/20
CPC分类号： F02C7/20
摘要： A retaining ring is provided for use in conjunction with a carburetor assembly having a flow passage therethrough for conducting a fuel-air mixture into a combustion chamber, the carburetor assembly comprising an air flow modifier and a fuel injector receiving element adjacent thereto. The retaining ring comprises a collar configured to engage the fuel injector receiving element so as to maintain its position adjacent the air flow modifier, and a retaining portion coupled to the collar and configured to engage the air flow modifier to secure the airflow modifier to the combustion chamber. The retaining portion cooperates with the collar to form an aperture through the retaining ring for receiving the carburetor assembly.
摘要翻译：提供一个保持环，用于与具有通过其的流动通道的化油器组件一起使用，以将燃料 - 空气混合物传导到燃烧室中，化油器组件包括气流调节器和与其相邻的燃料喷射器接收元件。保持环包括被配置为接合燃料喷射器接收元件以便保持其邻近空气流量调节器的位置的轴环，以及联接到轴环并被配置为接合气流调节器以将气流调节器固定到燃烧的保持部分房间。保持部分与套环协作以形成穿过保持环的孔，用于容纳化油器组件。

6. 发明申请

US20050241316A1 Uniform effusion cooling method for a can combustion chamber 审中-公开
标题翻译：罐式燃烧室均匀喷射冷却方法
公开(公告)号：US20050241316A1
公开(公告)日：2005-11-03
申请号：US10835169
申请日：2004-04-28
申请人： Ly Nguyen , Stony Kujala , David Walhood , Ian Critchley , Gregory Woodcock , Jurgen Schumacher
发明人： Ly Nguyen , Stony Kujala , David Walhood , Ian Critchley , Gregory Woodcock , Jurgen Schumacher
IPC分类号： F02C3/14 , F23R3/10
CPC分类号： F23R3/10 , F23R2900/03041 , Y02T50/675
摘要： A dome for a combustion chamber may have a plurality of effusion holes therein to provide efficient cooling while preventing carbon formation on the dome and chamber walls of the combustion chamber. Conventional dome cooling designs, using dome louvers, for example, may become corroded and/or may allow for ingestion of carbon particles that may build up and eventually separate from the dome. Furthermore, the dome cooling design of the present invention allows for the use of a lower profile dome as compared with conventional domes, thereby maximizing liner volume in the constrained combustion envelope while reducing combustor case weight. Additionally, the dome effusion cooling design of the present invention requires the use of less thermal barrier coating, as compared to conventional designs, in order to minimize thermal variation within the dome and between the dome and the combustor wall. A method for uniformly cooling a dome of a combustion chamber of an engine is also disclosed.
摘要翻译：用于燃烧室的圆顶可以在其中具有多个渗出孔以提供有效的冷却，同时防止燃烧室的圆顶和室壁上的碳形成。例如，使用圆顶百叶窗的常规圆顶冷却设计可能被腐蚀和/或可能允许摄取可能积聚并最终与圆顶分离的碳颗粒。此外，本发明的圆顶冷却设计允许与常规圆顶相比使用下部轮廓圆顶，由此在减小燃烧器壳体重量的同时最大化受限燃烧包层中的衬管体积。此外，与传统设计相比，本发明的圆顶渗出冷却设计需要使用较少的热障涂层，以便最小化圆顶内部和圆顶与燃烧室壁之间的热变化。还公开了一种用于均匀冷却发动机的燃烧室的圆顶的方法。

7. 发明申请

US20050204744A1 Temperature variance reduction using variable penetration dilution jets 有权
标题翻译：使用可变渗透稀释喷嘴进行温度变化减小
公开(公告)号：US20050204744A1
公开(公告)日：2005-09-22
申请号：US10803428
申请日：2004-03-17
申请人： Jurgen Schumacher , Ian Critchley , David Walhood
发明人： Jurgen Schumacher , Ian Critchley , David Walhood
IPC分类号： F23R3/04 , F23R3/06 , F23R3/52
CPC分类号： F23R3/06 , F23R3/52 , Y02T50/675
摘要： A variable penetration dilution jet array for a single can and scroll assembly includes a plurality of differentially sized dilution openings around the circumference of the combustor can. The alternating smaller and larger openings provide for circumferential and radial mixing uniformity with the smaller openings giving shallow penetration and the larger openings enabling deep core penetration. The larger openings provide dilution air to the hot gas flow core without the need for an increase in combustor pressure drop. The smaller openings provide a film cooling flow to the downstream scroll, reducing dedicated scroll cooling requirements.
摘要翻译：用于单个罐和涡旋组件的可变渗透稀释喷射阵列包括围绕燃烧器罐的圆周的多个差异尺寸的稀释开口。交替的较小和较大的开口提供周向和径向混合均匀性，较小的开口提供浅穿透，并且较大的开口使得能够深入岩心穿透。较大的开口为热气流芯提供稀释空气，而不需要增加燃烧室压降。较小的开口提供到下游涡卷的薄膜冷却流，从而减少专用的涡旋冷却要求。

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