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公开(公告)号：US09435259B2
公开(公告)日：2016-09-06
申请号：US13405527
申请日：2012-02-27
Applicant: Gabriel L. Suciu , Ioannis Alvanos
Inventor： Gabriel L. Suciu , Ioannis Alvanos
Abstract: A gas turbine engine includes a heat exchanger, a diffuser case, a passageway and a nozzle assembly. The heat exchanger exchanges heat with a bleed airflow to provide a conditioned airflow. The diffuser case includes a plenum that receives the conditioned airflow. The passageway is fluidly connected between the heat exchanger and the diffuser case, and the conditioned airflow is communicated through the passageway and into the plenum. The nozzle assembly is in fluid communication with the plenum of the diffuser case to receive the conditioned airflow from the plenum.
Abstract translation: 燃气涡轮发动机包括热交换器，扩散器壳体，通道和喷嘴组件。 热交换器与放气气流交换热量以提供调节气流。 扩散器壳体包括容纳调节气流的增压室。 通道流体地连接在热交换器和扩散器壳体之间，并且经调节的气流通过通道连通并进入通风室。 喷嘴组件与扩散器壳体的气室流体连通以接收来自气室的经调节的气流。
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公开(公告)号：US20160215638A1
公开(公告)日：2016-07-28
申请号：US14603033
申请日：2015-01-22
Applicant: United Technologies Corporation
Inventor： Steven D. Porter , Seth A. Max
CPC classification number: F01D11/005 , F01D11/003 , F01D25/12 , F01D25/16 , F02C7/08 , F02C7/28 , F05D2240/58 , F05D2240/581 , F05D2250/75 , F16J15/0887 , Y02T50/675
Abstract: A sealing arrangement has a turbine static structure with contact surfaces, a bearing compartment with contact surfaces, and a cavity between the turbine static structure and the bearing compartment. There are also two seals, wherein each seal is configured to contact the turbine static structure and the bearing compartment.
Abstract translation: 密封装置具有带有接触表面的涡轮机静态结构，具有接触表面的轴承室以及涡轮机静态结构和轴承室之间的空腔。 还有两个密封件，其中每个密封件构造成接触涡轮机静态结构和轴承室。
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公开(公告)号：US09395122B2
公开(公告)日：2016-07-19
申请号：US13036428
申请日：2011-02-28
Applicant: Andreas Eleftheriou , David Menheere , Daniel Alecu , Darius Jehangir Karanjia
Inventor： Andreas Eleftheriou , David Menheere , Daniel Alecu , Darius Jehangir Karanjia
CPC classification number: F02C7/10 , F02C7/08 , F02C7/14 , F05D2220/32 , F05D2260/213 , F05D2260/96 , F28D9/0018 , F28D21/0003 , F28D2021/0026 , F28F13/08
Abstract: A gas turbine engine recuperator including exhaust passages providing fluid flow communication between an exhaust inlet and an exhaust outlet, the exhaust inlet being oriented to receive exhaust flow from a turbine of the engine and the exhaust outlet being oriented to deliver the exhaust flow to atmosphere, the exhaust inlet having a smaller cross-sectional area than that of the exhaust outlet, and a cross sectional area of each exhaust passage progressively increasing from the exhaust inlet to the exhaust outlet such as to diffuse the exhaust flow. Air passages are in heat exchange relationship with the exhaust passages and provide fluid flow communication between an air inlet and an air outlet designed to sealingly engage respective plenums of the gas turbine engine.
Abstract translation: 一种燃气涡轮发动机换热器，包括排气通道，其提供排气入口和排气出口之间的流体流动连通，所述排气入口被定向为接收来自所述发动机的涡轮机的排气流，所述排气出口被定向成将排气流输送到大气， 排气入口具有比排气出口小的横截面面积，并且每个排气通道的横截面面积从排气入口逐渐增加到排气出口，从而扩散排气流。 空气通道与排气通道处于热交换关系，并且在空气入口和设计成密封地接合燃气涡轮发动机的各个通风室的空气出口之间提供流体流动连通。
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公开(公告)号：US20160201557A1
公开(公告)日：2016-07-14
申请号：US15076787
申请日：2016-03-22
Applicant: UNITED TECHNOLOGIES CORPORATION
Inventor： Federico PAPA , Thomas G. PHILLIPS , Kathleen R. PHILLIPS , Ethan K. STEARNS , Justin W. HEISS
CPC classification number: F02C7/12 , F01D25/12 , F02C3/08 , F02C7/06 , F02C7/08 , F02C7/14 , F02C7/224 , F02C7/232 , F02C9/00 , F02C9/48 , F05D2220/32 , F05D2260/213 , G05B15/02 , G05D7/06 , Y02T50/675
Abstract: A thermal management system for a gas turbine engine according to an exemplary aspect of the present disclosure includes, among other things, a heat exchanger and a valve that controls an amount of a first fluid that is communicated through the heat exchanger. A first sensor senses a first characteristic of a second fluid that is communicated through the heat exchanger to exchange heat with the first fluid and a second sensor senses a second characteristic of the second fluid. A positioning of the valve is based on at least one of the first characteristic and the second characteristic.
Abstract translation: 根据本公开的示例性方面的用于燃气涡轮发动机的热管理系统尤其包括热交换器和阀，其控制通过热交换器连通的第一流体的量。 第一传感器感测通过热交换器连通的第二流体的第一特征，以与第一流体交换热量，第二传感器感测第二流体的第二特性。 阀的定位基于第一特征和第二特性中的至少一个。
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25.发明授权Aero boost—gas turbine energy supplementing systems and efficient inlet cooling and heating, and methods of making and using the same 有权航空增压燃气轮机能量补充系统和高效入口冷却和加热，以及制造和使用它们的方法公开(公告)号：US09388737B2
公开(公告)日：2016-07-12
申请号：US14419853
申请日：2013-10-03
Applicant: PowerPHASE LLC
Inventor： Robert J. Kraft
Abstract: The invention relates generally to electrical power systems, including generating capacity of a gas turbine, and more specifically to pressurized air injection that is useful for providing additional electrical power during periods of peak electrical power demand from a gas turbine system power plant, as well as to inlet heating to allow increased engine turn down during periods of reduced electrical demand.
Abstract translation: 本发明一般涉及电力系统，包括燃气轮机的发电容量，更具体地说，涉及在从燃气轮机系统发电厂的峰值电力需求期间提供附加电力的加压空气喷射，以及 进气加热以允许在减少的电力需求期间增加发动机的转向。
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Patent Agency Ranking
公开(公告)号：US20160169105A1
公开(公告)日：2016-06-16
申请号：US14623939
申请日：2015-02-17
Applicant: PowerPHASE LLC
Inventor： ROBERT J. KRAFT
Abstract: The invention relates generally to electrical power systems, including generating capacity of a gas turbine, and more specifically to pressurized air injection that is useful for providing additional electrical power during periods of peak electrical power demand from a gas turbine system power plant, as well as to inlet heating to allow increased engine turn down during periods of reduced electrical demand.
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公开(公告)号：US20160160755A1
公开(公告)日：2016-06-09
申请号：US14910062
申请日：2014-07-25
Applicant: ICE INDUSTRIAL PROPERTIES B.V.
Inventor： George Johannes KRUIJER , Johannes Arjen HOOGLAND , Karl MAY
CPC classification number: F02C1/05 , F02C1/08 , F02C3/02 , F02C7/08 , F02C7/105 , F16K11/074 , F28D17/04 , F28D21/001
Abstract: The invention is directed to a fluid distributing apparatus comprising a fixed part and a rotating part. The fixed part is provided with at least one inlet channel and at least one outlet channel and wherein each inlet and outlet channel has a facing opening facing the rotating part. The rotating part is rotatably positioned relative to the fixed part such that the rotating part can have multiple rotational positions relative to the fixed part, wherein the rotating part is provided with at least a connecting channel having an inlet and outlet opening in the rotating part. The inlet and outlet opening of at least one connecting channel in the rotating part aligns with the facing openings of at least one inlet and outlet channel in the fixed part in at least one rotational position and not align in another position.
Abstract translation: 本发明涉及一种包括固定部分和旋转部分的流体分配装置。 固定部分设置有至少一个入口通道和至少一个出口通道，并且其中每个入口和出口通道具有面向旋转部分的面对开口。 旋转部分相对于固定部分可旋转地定位，使得旋转部分可以相对于固定部分具有多个旋转位置，其中旋转部分设置有至少一个在旋转部分中具有入口和出口的连接通道。 旋转部件中的至少一个连接通道的入口和出口开口与至少一个入口和出口通道在至少一个旋转位置中的至少一个入口通道和出口通道对准，而不在另一位置对准。
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公开(公告)号：US09347375B2
公开(公告)日：2016-05-24
申请号：US13531262
申请日：2012-06-22
Applicant: Michael John Hughes
Inventor： Michael John Hughes
CPC classification number: F02C7/08 , F02C3/14 , F02C3/34 , F23C9/00 , F23C9/006 , F23C2202/30 , F23C2202/50 , F23C2900/09001 , F23R3/005 , F23R3/04 , F23R3/06 , F23R3/286 , Y02T50/675
Abstract: In one embodiment, a system includes a turbine combustor of a turbine system with the turbine combustor at least partially enclosed within a compressor discharge casing. The turbine system also includes an exhaust gas recovery system that includes an exhaust gas recirculation duct. The exhaust gas recirculation duct is configured to recirculate exhaust gas from a downstream end of the turbine combustor to an upstream end of the turbine combustor. This exhaust gas recirculation duct is entirely enclosed within the compressor discharge casing.
Abstract translation: 在一个实施例中，系统包括涡轮机系统的涡轮机燃烧器，涡轮机燃烧器至少部分地封闭在压缩机排放壳体内。 涡轮机系统还包括排气回收系统，其包括废气再循环管道。 排气再循环管道被配置为使来自涡轮机燃烧器的下游端的废气再循环到涡轮机燃烧器的上游端。 该废气再循环管道完全封闭在压缩机排放壳体内。
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29.发明申请公开(公告)号：US20160131031A1
公开(公告)日：2016-05-12
申请号：US14534598
申请日：2014-11-06
Applicant: PowerPhase LLC
Inventor： ROBERT J. KRAFT , SCOTT AUERBACH , PETER PERRI
CPC classification number: F02C6/16 , F02C3/34 , F02C6/08 , F02C6/14 , F02C7/08 , F02C7/10 , F02C7/143 , Y02E60/15
Abstract: The present invention discloses a novel apparatus and methods for augmenting the power of a gas turbine engine, improving gas turbine engine operation, and reducing the response time necessary to meet changing demands of an electrical grid. Improvements in power augmentation and engine operation include systems and methods for providing rapid response given a change in electrical grid.
Abstract translation: 本发明公开了一种用于增加燃气轮机发动机功率，改进燃气轮机发动机运行以及减少满足电网不断变化的需求所需的响应时间的新型装置和方法。 功率增加和发动机运行的改进包括由于电网变化而提供快速响应的系统和方法。
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公开(公告)号：US09249728B2
公开(公告)日：2016-02-02
申请号：US13468218
申请日：2012-05-10
Applicant: Chan-Sun Lim , Myeong-Hyo Kim , Jong-Sub Shin , Young-Chang Shon , Jeong-Hun Lee
Inventor： Chan-Sun Lim , Myeong-Hyo Kim , Jong-Sub Shin , Young-Chang Shon , Jeong-Hun Lee
Abstract: A power generation system includes a compression unit which compresses a gas, a storage which stores the compressed gas output from the compression unit, a first expansion unit which generates first power and outputs a first exhaust gas, a heating unit which heats at least the stored gas output from the storage, a second expansion unit which generates second power and outputs a second exhaust gas, a first regenerator which performs a first heat exchange between the second exhaust gas and the stored gas output from the storage, to generate a first heat exchange gas used to generate the first power and a first regenerator gas, and a second regenerator which performs a second heat exchange between the first exhaust gas and the first regenerator gas to generate a second heat exchange gas used to generate the second power after heated at the heating unit.
Abstract translation: 发电系统包括压缩气体的压缩单元，存储从压缩单元输出的压缩气体的存储器，产生第一功率并输出第一排气的第一膨胀单元，至少加热存储的加热单元 从存储器输出的气体，产生第二功率并输出第二废气的第二膨胀单元，在第二排气和从储存器输出的储存气体之间进行第一热交换的第一再生器，以产生第一热交换 用于产生第一功率的气体和第一再生器气体;以及第二再生器，其在第一废气和第一再生器气体之间进行第二热交换，以产生用于在第二再生器加热后产生第二功率的第二热交换气体 加热单元
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