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公开(公告)号：US20160169519A1
公开(公告)日：2016-06-16
申请号：US14567768
申请日：2014-12-11
Applicant: General Electric Company
Inventor： Lewis Berkley Davis, JR. , Gregory Thomas Foster , Kaitlin Marie Graham , Krishnakumar Venkataraman , Stanley Kevin Widener
CPC classification number: F23R3/34 , F02C9/28 , F23N1/00 , F23N5/003 , F23N2023/04 , F23N2023/08 , F23N2041/20 , F23R2900/03341
Abstract: Aspects of the present disclosure provide an apparatus including: an injector in fluid communication with an aft section of a reheat combustor in a power generation system, the aft section being positioned downstream of a combustion reaction zone in the reheat combustor, and positioned upstream of a turbine stage of the power generation system, wherein the turbine stage includes a turbine nozzle and a turbine blade row; and a conduit in fluid communication with the injector, wherein the conduit delivers at least one of a fuel from a fuel supply line and a carrier gas to the injector.
Abstract translation: 本公开的方面提供一种装置，包括：与发电系统中的再热燃烧器的后部流体连通的喷射器，所述后部位于所述再热燃烧器中的燃烧反应区的下游，并且位于所述再热燃烧器的上游 涡轮机级，其中所述涡轮级包括涡轮喷嘴和涡轮叶片排; 以及与所述注射器流体连通的导管，其中所述导管将来自燃料供应管线和载气的燃料中的至少一个输送到所述注射器。
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公开(公告)号：US20160169518A1
公开(公告)日：2016-06-16
申请号：US14567761
申请日：2014-12-11
Applicant: General Electric Company
Inventor： Lewis Berkley Davis, JR. , Gregory Thomas Foster , Kaitlin Marie Graham , Krishnakumar Venkataraman , Stanley Kevin Widener
IPC: F23R3/20
CPC classification number: F23R3/34 , F02C9/28 , F23N1/00 , F23N5/003 , F23N2023/04 , F23N2023/08 , F23N2041/20 , F23R2900/03341
Abstract: Embodiments of the present disclosure provide an apparatus comprising: a reaction chamber positioned between a first turbine stage of a power generation system and a turbine stage of the power generation system, wherein the turbine stage comprises a turbine nozzle and a turbine blade row; a plurality of injectors positioned on a wall of the reaction chamber; and a conduit in fluid communication with the plurality of injectors, wherein the conduit delivers at least one of fuel from a fuel supply line to the reaction chamber through the plurality of injectors.
Abstract translation: 本公开的实施例提供了一种装置，包括：位于发电系统的第一涡轮机级和发电系统的涡轮级之间的反应室，其中所述涡轮级包括涡轮喷嘴和涡轮叶片排; 位于所述反应室的壁上的多个喷射器; 以及与所述多个喷射器流体连通的导管，其中所述导管通过所述多个喷射器将来自燃料供应管线的燃料中的至少一个输送到所述反应室。
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公开(公告)号：US20150218962A1
公开(公告)日：2015-08-06
申请号：US14173949
申请日：2014-02-06
Applicant: General Electric Company
Inventor： David Wayne Weber , Gregory Thomas Foster , Benjamin Paul Lacy , Aaron Ezekiel Smith , Dustin Michael Earnhardt
CPC classification number: B22C7/02 , B22C9/04 , B22C9/10 , B22C9/103 , B22C9/108 , B22C9/24 , F01D5/186 , F05D2230/211 , F05D2240/81 , F05D2260/204
Abstract: A core for forming micro channels within a turbine component is provided. The core includes a base comprising a first side and a second side; and a core assembly coupled to the second side. The core assembly further includes a plurality of channel members, wherein each channel member has a first end, a second end, and a channel body coupled to and extending between said first end and said second end. The channel body includes a channel shape configured to form the micro channels within the turbine component.
Abstract translation: 提供了一种用于在涡轮机部件内形成微通道的芯。 芯部包括一个包括第一面和第二面的基底; 以及耦合到第二侧的芯组件。 芯组件还包括多个通道构件，其中每个通道构件具有第一端，第二端和与所述第一端和所述第二端连接并在其之间延伸的通道体。 通道体包括被配置为在涡轮部件内形成微通道的通道形状。
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公开(公告)号：US20150037165A1
公开(公告)日：2015-02-05
申请号：US13955679
申请日：2013-07-31
Applicant: General Electric Company
Inventor： Mark Andrew Jones , Bradley Taylor Boyer , Robert Alan Brittingham , Gregory Thomas Foster , Christopher William Kester
CPC classification number: F01D5/16 , B22C9/10 , B22C9/24 , B23P15/04 , F01D5/147 , F01D5/18 , F01D5/186 , F01D5/187 , F05D2240/304 , F05D2240/305 , F05D2240/306 , F05D2260/2212 , F05D2260/2214 , F05D2260/22141 , F05D2260/961 , Y10T29/49337
Abstract: A turbine blade is provided and includes pressure and suction surfaces connected to define an interior through which coolant is passable and first and second pedestal arrays, each of the first and second pedestal arrays including pedestals respectively coupled to radially outboard portions of respective interior faces of one of the pressure and suction surfaces. The pedestals of the first pedestal array are separated from pedestals of the second pedestal array by gaps respectively defined therebetween.
Abstract translation: 涡轮叶片被设置并且包括连接以限定冷却剂可通过的内部的压力和吸力表面，以及第一和第二基座阵列，第一和第二基座阵列中的每一个包括基座，分别联接到一个的相应内部面的径向外侧部分 的压力和吸力表面。 第一基座阵列的基座通过分别限定在其间的间隙与第二基座阵列的基座分离。
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