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公开(公告)号：US20140352316A1
公开(公告)日：2014-12-04
申请号：US13908050
申请日：2013-06-03
Applicant: General Electric Company
Inventor： Elizabeth Angelyn Fadde , Lucas John Stoia , Christopher Paul Willis
IPC: F23R3/00
CPC classification number: F23R3/002 , F02C7/264 , F02C7/266 , F23R3/60 , F23R2900/00012
Abstract: The present application provides a combustor with a radial penetration. The combustor may include a combustion chamber, a liner surrounding the combustion chamber, a flow sleeve surrounding the liner, a penetration tube extending through the liner and the flow sleeve with the radial penetration positioned within the penetration tube, a flange extending from the penetration tube about the flow sleeve, and a ferrule positioned about the flange and the radial penetration so as to limit leakage about the radial penetration.
Abstract translation: 本申请提供了具有径向穿透的燃烧器。 燃烧器可以包括燃烧室，围绕燃烧室的衬套，围绕衬套的流动套筒，穿过衬套延伸的穿透管和流体套筒，其中径向穿透位于穿透管内，从穿透管延伸的凸缘 围绕流动套筒和围绕凸缘定位的套圈和径向穿透以限制径向穿透的泄漏。
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公开(公告)号：US20140216363A1
公开(公告)日：2014-08-07
申请号：US13759985
申请日：2013-02-05
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Diego Fernando Rancruel , Drake Joseph Viscome , Elizabeth Angelyn Fadde , Ashlee Nicole Atwell , Kyle Joseph Conger
CPC classification number: F22G3/00 , F01K23/067 , F01K23/10 , F22B29/06 , F22B33/02 , F22G5/00 , Y02E20/16 , Y02E20/18 , Y10T137/0324
Abstract: A system includes a heat recovery steam generator (HRSG) having a plurality of evaporator sections. At least one evaporator section includes a forced circulation evaporator configured to generate a saturated steam, a once-through evaporator configured to generate a first superheated steam, and a first superheater configured to receive the saturated steam and the first superheated steam.
Abstract translation: 一种系统包括具有多个蒸发器部分的热回收蒸汽发生器（HRSG）。 至少一个蒸发器部分包括配置成产生饱和蒸汽的强制循环蒸发器，配置成产生第一过热蒸汽的直流蒸发器和被配置为接收饱和蒸汽和第一过热蒸汽的第一过热器。
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公开(公告)号：US20140182303A1
公开(公告)日：2014-07-03
申请号：US14067726
申请日：2013-10-30
CPC classification number: F23R3/26 , F02C3/34 , F23C9/00 , F23C9/006 , F23C2202/30 , F23R3/10 , F23R3/286 , F23R3/46 , Y02E20/16 , Y02T50/675
Abstract: A system includes a turbine combustor that includes a head end portion having a head end chamber, a combustion portion having a combustion chamber disposed downstream from the head end chamber, a cap disposed between the head end chamber and the combustion chamber, and a flow distributor configured to distribute an exhaust flow circumferentially around the head end chamber. The flow distributor includes at least one exhaust gas flow path.
Abstract translation: 一种系统包括涡轮机燃烧器，其包括具有头端室的头端部分，具有设置在头端腔室下游的燃烧室的燃烧部分，设置在头端室和燃烧室之间的盖，以及流量分配器 被配置成围绕头端室周向地分布排气流。 流量分配器包括至少一个废气流动路径。
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Patent Agency Ranking
公开(公告)号：US09989254B2
公开(公告)日：2018-06-05
申请号：US13908050
申请日：2013-06-03
Applicant: General Electric Company
Inventor： Elizabeth Angelyn Fadde , Lucas John Stoia , Christopher Paul Willis
CPC classification number: F23R3/002 , F02C7/264 , F02C7/266 , F23R3/60 , F23R2900/00012
Abstract: The present application provides a combustor with a radial penetration. The combustor may include a combustion chamber, a liner surrounding the combustion chamber, a flow sleeve surrounding the liner, a penetration tube extending through the liner and the flow sleeve with the radial penetration positioned within the penetration tube, a flange extending from the penetration tube about the flow sleeve, and a ferrule positioned about the flange and the radial penetration so as to limit leakage about the radial penetration.
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15.发明授权Internally cooled transition duct aft frame with serpentine cooling passage and conduit 有权内部冷却过渡管道后部框架与蛇形冷却通道和导管公开(公告)号：US09574498B2
公开(公告)日：2017-02-21
申请号：US14036101
申请日：2013-09-25
Applicant: General Electric Company
Inventor： Elizabeth Angelyn Fadde , Patrick Benedict Melton , David William Cihlar , Richard Martin DiCintio
CPC classification number: F02C7/141 , F01D9/023 , F01D25/12 , F05D2260/2214 , F23R3/002 , F23R3/04 , F23R3/60 , F23R2900/03043 , F23R2900/03044
Abstract: An aft frame for a transition duct of a gas turbine combustor includes a main body having an outer rail, an inner rail, a first side rail circumferentially separated from an opposing second side rail, a forward portion, an aft portion and an outer surface. An inlet port extends through the outer surface and an exhaust port extends through the forward portion. A serpentine cooling passage is defined within the main body beneath the outer surface. The serpentine cooling passage is in fluid communication with the inlet port and the exhaust port. A conduit may be connected to the exhaust port for routing a compressed working fluid away from aft frame.
Abstract translation: 用于燃气轮机燃烧器的过渡管道的后框架包括主体，其具有外轨，内轨，与相对的第二侧轨周向隔开的第一侧轨，前部，后部和外表面。 入口端口延伸穿过外表面，并且排气口延伸穿过前部。 蛇形冷却通道限定在主体下面的外表面下方。 蛇形冷却通道与入口端口和排气口流体连通。 导管可以连接到排气口，用于使压缩的工作流体远离后框架。
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公开(公告)号：US20140182304A1
公开(公告)日：2014-07-03
申请号：US14067731
申请日：2013-10-30
CPC classification number: F23R3/26 , F23C9/00 , F23C2202/30 , F23R3/04 , F23R3/10 , F23R3/286 , F23R3/46 , Y02E20/16 , Y02T50/675
Abstract: A system includes a turbine combustor that includes a head end portion having a head end chamber, a combustion portion having a combustion chamber disposed downstream from the head end chamber, a cap disposed between the head end chamber and the combustion chamber, and a flow distributor configured to distribute an oxidant flow circumferentially around the head end chamber. The flow distributor includes at least one oxidant flow path.
Abstract translation: 一种系统包括涡轮机燃烧器，其包括具有头端室的头端部分，具有设置在头端腔室下游的燃烧室的燃烧部分，设置在头端室和燃烧室之间的盖，以及流量分配器 被配置为围绕头端室周向地分布氧化剂流。 流量分配器包括至少一个氧化剂流动路径。
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公开(公告)号：US20140182302A1
公开(公告)日：2014-07-03
申请号：US14067714
申请日：2013-10-30
CPC classification number: F23R3/26 , F23C9/00 , F23C2202/30 , F23R3/10 , F23R3/286 , F23R3/46 , Y02E20/16 , Y02T50/675
Abstract: A system includes a turbine combustor that includes a head end portion having a head end chamber, a combustion portion having a combustion chamber disposed downstream from the head end chamber, a cap disposed between the head end chamber and the combustion chamber, and a flow distributor configured to distribute at least one of an exhaust flow, an oxidant flow, an oxidant-exhaust mixture, or any combination thereof circumferentially around the head end chamber.
Abstract translation: 一种系统包括涡轮机燃烧器，其包括具有头端室的头端部分，具有设置在头端腔室下游的燃烧室的燃烧部分，设置在头端室和燃烧室之间的盖，以及流量分配器 被配置为分布在头端室周围的排气流，氧化剂流，氧化剂 - 排气混合物或其任何组合中的至少一种。
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公开(公告)号：US20140182301A1
公开(公告)日：2014-07-03
申请号：US14067679
申请日：2013-10-30
CPC classification number: F02C3/34 , F23C9/00 , F23C2202/30 , F23J2215/50 , F23J2900/15061 , F23L7/007 , F23L2900/07001 , F23R3/26 , F23R3/286 , Y02E20/16 , Y02E20/322 , Y02E20/344
Abstract: A system includes a turbine combustor that includes a head end portion having a head end chamber, a combustion portion having a combustion chamber disposed downstream from the head end chamber, a cap disposed between the head end chamber and the combustion chamber, and a flow separator configured to separate a first exhaust flow from an oxidant flow. The flow separator is configured to direct the first exhaust flow into the head end chamber. The turbine combustor also includes a mixing region configured to mix the first exhaust flow with the oxidant flow to provide an oxidant-exhaust mixture.
Abstract translation: 一种系统包括涡轮机燃烧器，其包括具有头端室的头端部分，具有设置在头端室下游的燃烧室的燃烧部分，设置在头端室和燃烧室之间的盖子以及流动分离器 被配置为将第一废气流与氧化剂流分离。 流动分离器构造成将第一排气流引导到头端室中。 涡轮机燃烧器还包括混合区域，其被配置为将第一排气流与氧化剂流混合以提供氧化剂 - 排气混合物。
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