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公开(公告)号：US09394828B2
公开(公告)日：2016-07-19
申请号：US13036407
申请日：2011-02-28
CPC分类号： F02C7/08 , F05D2220/323 , F05D2230/60 , F05D2230/642 , F28D9/0018 , F28D21/001 , F28F9/0236 , F28F9/26 , F28F21/087 , F28F2230/00 , F28F2265/26 , Y10T29/49716
摘要： A gas turbine engine recuperator including a plurality of independent arcuate segments, each segment having an inlet connection member designed to sealingly engage a plenum in fluid flow communication with the compressor discharge, and an outlet connection member designed to sealingly engage a plenum containing the combustor. One of the inlet and outlet connection members is a rigid member forming a rigid connection to the respective plenum, and the other of the inlet and outlet connection members includes a flexible member and forms a floating connection to the respective plenum, the floating connection allowing relative movement between the segment and a remainder of the gas turbine engine.
摘要翻译： 一种燃气涡轮发动机换热器，包括多个独立的弧形段，每个段具有入口连接构件，其设计成密封地接合与压缩机排放流体流动连通的气室;以及出口连接构件，设计成密封地接合包含燃烧器的气室。 入口和出口连接构件中的一个是刚性构件，其形成与相应的气室的刚性连接，并且入口和出口连接构件中的另一个包括柔性构件并且形成到相应气室的浮动连接，所述浮动连接允许相对 该段与燃气涡轮发动机的其余部分之间的运动。
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公开(公告)号：US09068506B2
公开(公告)日：2015-06-30
申请号：US13435051
申请日：2012-03-30
CPC分类号： F02C7/08 , F01D25/30 , F05D2270/17
摘要： A gas turbine engine recuperator system includes a heat recuperator positioned in a gas turbine exhaust gas duct for recovering heat from turbine exhaust gases to preheat a compressor flow being supplied to the combustor. A continuous bleed flow of the turbine exhaust gases is provided to bypass the heat recuperator. The continuous bleed flow of the turbine exhaust gases is adjustable to reduce turbine exhaust gas pressure loss at a high engine operation level and to provide efficient heat recovery at low and/or medium engine operation levels.
摘要翻译： 燃气涡轮发动机换热器系统包括定位在燃气轮机废气管道中的热回收器，用于从涡轮废气回收热量以预热供应到燃烧器的压缩机流。 提供涡轮废气的连续排出流以绕过热交换器。 涡轮废气的连续排放流量是可调节的，以在高发动机操作水平下降低涡轮机废气压力损失并且在低和/或中等发动机运行水平下提供有效的热回收。
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公开(公告)号：US20120216506A1
公开(公告)日：2012-08-30
申请号：US13036407
申请日：2011-02-28
CPC分类号： F02C7/08 , F05D2220/323 , F05D2230/60 , F05D2230/642 , F28D9/0018 , F28D21/001 , F28F9/0236 , F28F9/26 , F28F21/087 , F28F2230/00 , F28F2265/26 , Y10T29/49716
摘要： A gas turbine engine recuperator including a plurality of independent arcuate segments, each segment having an inlet connection member designed to sealingly engage a plenum in fluid flow communication with the compressor discharge, and an outlet connection member designed to sealingly engage a plenum containing the combustor. One of the inlet and outlet connection members is a rigid member forming a rigid connection to the respective plenum, and the other of the inlet and outlet connection members includes a flexible member and forms a floating connection to the respective plenum, the floating connection allowing relative movement between the segment and a remainder of the gas turbine engine.
摘要翻译： 一种燃气涡轮发动机换热器，包括多个独立的弧形段，每个段具有入口连接构件，其设计成密封地接合与压缩机排放流体流动连通的气室;以及出口连接构件，设计成密封地接合包含燃烧器的气室。 入口和出口连接构件中的一个是刚性构件，其形成与相应气室的刚性连接，并且入口和出口连接构件中的另一个包括柔性构件并形成到相应气室的浮动连接，浮动连接允许相对 该段与燃气涡轮发动机的其余部分之间的运动。
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公开(公告)号：US09766019B2
公开(公告)日：2017-09-19
申请号：US13036463
申请日：2011-02-28
申请人： Andreas Eleftheriou , David Menheere , Daniel Alecu , Darius Jehangir Karanjia , Daniel Van Den Ende
发明人： Andreas Eleftheriou , David Menheere , Daniel Alecu , Darius Jehangir Karanjia , Daniel Van Den Ende
CPC分类号： F28D21/0003 , F02C7/08 , F02C7/10 , F02C7/143 , F28D9/0018 , F28F2250/102 , F28F2265/26 , F28F2265/30 , Y02T50/675
摘要： A gas turbine engine recuperator 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 passages having an arcuate profile in a plane perpendicular to a central axis of the recuperator to reduce a swirl of the exhaust flow. Air passages are in heat exchange relationship with the exhaust passages and providing fluid flow communication between an air inlet and an air outlet, design to sealingly respective plenum of the gas turbine engine.
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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
CPC分类号： F02C7/10 , F02C7/08 , F02C7/14 , F05D2220/32 , F05D2260/213 , F05D2260/96 , F28D9/0018 , F28D21/0003 , F28D2021/0026 , F28F13/08
摘要： 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.
摘要翻译： 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：US09169780B2
公开(公告)日：2015-10-27
申请号：US13183848
申请日：2011-07-15
申请人： Barry Barnett , Daniel Alecu , Andreas Eleftheriou
发明人： Barry Barnett , Daniel Alecu , Andreas Eleftheriou
CPC分类号： F02C7/06 , F02C7/32 , F02C7/36 , F05D2260/202
摘要： A gas turbine engine having an electric generator includes a transmission shaft extending along a longitudinal axis of the engine and drivingly interconnecting a turbine shaft of the engine and a rotor shaft of the electric generator. The transmission shaft is engaged by splined mating connections with the turbine shaft and the rotor shaft. The transmission shaft has a shear neck defining a reduced radial wall thickness with respect to a remainder of the transmission shaft such as to provide a weakened region of the transmission shaft. An annular support structure, concentric with and surrounding the transmission shaft, is axially located between the shear neck and a forward end of the transmission shaft engaged to the turbine shaft, and includes a bearing operable to rotationally support the transmission shaft.
摘要翻译： 具有发电机的燃气涡轮发动机包括：沿着发动机的纵轴延伸的传动轴，并将发动机的涡轮轴与发电机的转子轴驱动连接。 传动轴通过与涡轮轴和转子轴的花键配合连接接合。 传动轴具有剪切颈部，其相对于传动轴的其余部分限定径向壁厚度减小，以便提供传动轴的弱化区域。 与传动轴同心并且围绕传动轴的环形支撑结构轴向地位于剪切颈部和接合到涡轮轴的传动轴的前端之间，并且包括可操作以可旋转地支撑传动轴的轴承。
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公开(公告)号：US09316111B2
公开(公告)日：2016-04-19
申请号：US13326434
申请日：2011-12-15
申请人： Andreas Eleftheriou , Daniel Alecu
发明人： Andreas Eleftheriou , Daniel Alecu
摘要： An active tip clearance control (ATCC) system of a gas turbine engine includes an ejector to selectively drive an air flow passing through the ATCC system. A high pressure air flow as a motive flow of the ejector is controlled by a valve according to engine operation requirements.
摘要翻译： 燃气涡轮发动机的主动顶尖间隙控制（ATCC）系统包括用于选择性地驱动通过ATCC系统的空气流的喷射器。 作为喷射器的动力流动的高压空气流由根据发动机操作要求的阀门控制。
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公开(公告)号：US09951639B2
公开(公告)日：2018-04-24
申请号：US13358889
申请日：2012-02-10
CPC分类号： F01D11/005 , F01D9/042 , F05D2240/55 , Y10T29/49245
摘要： Vane assemblies for gas turbine engines and methods for assembling vane assemblies are disclosed. The vane assemblies may include at least one shroud having at least one vane-receiving portion, at least one vane having at least one end portion received in the vane-receiving portion, and at least one sealing member having an uncompressed cross-section that is substantially circular. The sealing member(s) are disposed between and in contact with the end portion of the vane and the vane-receiving portion of the shroud.
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公开(公告)号：US20130014513A1
公开(公告)日：2013-01-17
申请号：US13183848
申请日：2011-07-15
申请人： Barry Barnett , Daniel Alecu , Andreas Eleftheriou
发明人： Barry Barnett , Daniel Alecu , Andreas Eleftheriou
IPC分类号： F02C6/00
CPC分类号： F02C7/06 , F02C7/32 , F02C7/36 , F05D2260/202
摘要： A gas turbine engine having an electric generator includes a transmission shaft extending along a longitudinal axis of the engine and drivingly interconnecting a turbine shaft of the engine and a rotor shaft of the electric generator. The transmission shaft is engaged by splined mating connections with the turbine shaft and the rotor shaft. The transmission shaft has a shear neck defining a reduced radial wall thickness with respect to a remainder of the transmission shaft such as to provide a weakened region of the transmission shaft. An annular support structure, concentric with and surrounding the transmission shaft, is axially located between the shear neck and a forward end of the transmission shaft engaged to the turbine shaft, and includes a bearing operable to rotationally support the transmission shaft.
摘要翻译： 具有发电机的燃气涡轮发动机包括：沿着发动机的纵轴延伸的传动轴，并将发动机的涡轮轴与发电机的转子轴驱动连接。 传动轴通过与涡轮轴和转子轴的花键配合连接接合。 传动轴具有剪切颈部，其相对于传动轴的其余部分限定径向壁厚度减小，以便提供传动轴的弱化区域。 与传动轴同心并且围绕传动轴的环形支撑结构轴向地位于剪切颈部和接合到涡轮轴的传动轴的前端之间，并且包括可操作以可旋转地支撑传动轴的轴承。
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公开(公告)号：US08632299B2
公开(公告)日：2014-01-21
申请号：US12956405
申请日：2010-11-30
IPC分类号： F01D25/26
CPC分类号： F01D25/002 , F01D25/24
摘要： A gas turbine engine includes a structure defining a circumferential passage in fluid communication with an internal passage in at least one strut radially extending into the engine, circumferential passage also in fluid communication with a plurality or nozzles or jets to provide a wash manifold integrated with the engine casing structure. One or more nozzles are provided in the manifold for directing a washing fluid injected into the duct.
摘要翻译： 燃气涡轮发动机包括限定在径向延伸到发动机中的至少一个支柱中的内部通道流体连通的圆周通道的结构，圆周通道也与多个喷嘴或喷嘴流体连通，以提供与 发动机套管结构。 在歧管中设置一个或多个喷嘴，用于引导注入到管道中的洗涤流体。
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