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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
Applicant: Richard Ivakitch , Andreas Eleftheriou , David Denis , David Menheere
Inventor： Richard Ivakitch , Andreas Eleftheriou , David Denis , David Menheere
CPC classification number: F01D11/005 , F01D9/042 , F05D2240/55 , Y10T29/49245
Abstract: 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：US09766019B2
公开(公告)日：2017-09-19
申请号：US13036463
申请日：2011-02-28
Applicant: Andreas Eleftheriou , David Menheere , Daniel Alecu , Darius Jehangir Karanjia , Daniel Van Den Ende
Inventor： Andreas Eleftheriou , David Menheere , Daniel Alecu , Darius Jehangir Karanjia , Daniel Van Den Ende
CPC classification number: F28D21/0003 , F02C7/08 , F02C7/10 , F02C7/143 , F28D9/0018 , F28F2250/102 , F28F2265/26 , F28F2265/30 , Y02T50/675
Abstract: 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：US08956108B2
公开(公告)日：2015-02-17
申请号：US13469712
申请日：2012-05-11
Applicant: Andreas Eleftheriou , David Menheere
Inventor： Andreas Eleftheriou , David Menheere
IPC: F01D15/12
CPC classification number: F02K3/06 , F02C3/06 , F02C3/107 , F02C7/36 , F05D2260/40311 , Y10T29/49231
Abstract: An assembly for a gas turbine engine, with a gearbox including a first portion having a first input gear coupled to a rotatable turbine shaft, a first output gear, and defining a first transmission path between the first input and output gears, and a second portion having a second input gear coupled to the turbine shaft, a second output gear, and defining a second transmission path between the second input and output gears different from the first transmission path. A fan rotor is coupled to the first output gear and a booster rotor is coupled to the second output gear on a same side of the gearbox than the coupling between the fan rotor and the first output gear. A method of assembling a drive for a fan rotor and a booster rotor in a gas turbine engine is also disclosed.
Abstract translation: 一种用于燃气涡轮发动机的组件，其具有包括第一部分的齿轮箱，第一部分具有联接到可旋转的涡轮轴的第一输入齿轮，第一输出齿轮，并且限定第一输入和输出齿轮之间的第一传动路径，以及第二部分 具有联接到涡轮机轴的第二输入齿轮，第二输出齿轮，并且在不同于第一传动路径的第二输入齿轮和输出齿轮之间限定第二传动路径。 风扇转子联接到第一输出齿轮，并且增强转子与齿轮箱的与风扇转子和第一输出齿轮之间的联接相同的一侧耦合到第二输出齿轮。 还公开了一种在燃气轮机中组装用于风扇转子和升压转子的驱动装置的方法。
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公开(公告)号：US20130058778A1
公开(公告)日：2013-03-07
申请号：US13224379
申请日：2011-09-02
Applicant: Andreas ELEFTHERIOU , David MENHEERE , Quantai LIU
Inventor： Andreas ELEFTHERIOU , David MENHEERE , Quantai LIU
IPC: F02C7/20
CPC classification number: F02C7/20 , F05D2230/232
Abstract: A fabricated engine case has a plurality of circumferentially spaced struts radially extending between an outer case and an inner case. A mount apparatus is affixed to the outer case of the engine case. The mount apparatus is a mount base radially spaced apart from a circumferential skin of the outer case and a load bearing member extending radially inwardly to connect the mount base to an outer end of one of the struts.
Abstract translation: 制造的发动机壳体具有在外壳和内壳之间径向延伸的多个周向间隔的支柱。 发动机壳体的外壳附着有安装装置。 安装装置是与外壳的圆周表皮径向间隔开的安装基座和径向向内延伸的承载构件，以将安装基座连接到一个支柱的外端。
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公开(公告)号：US20120216544A1
公开(公告)日：2012-08-30
申请号：US13036463
申请日：2011-02-28
Applicant: Andreas ELEFTHERIOU , David Menheere , Daniel Alecu , Darius Jehangir Karanjia , Daniel Van Den Ende
Inventor： Andreas ELEFTHERIOU , David Menheere , Daniel Alecu , Darius Jehangir Karanjia , Daniel Van Den Ende
CPC classification number: F28D21/0003 , F02C7/08 , F02C7/10 , F02C7/143 , F28D9/0018 , F28F2250/102 , F28F2265/26 , F28F2265/30 , Y02T50/675
Abstract: 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.
Abstract translation: 一种燃气涡轮发动机换热器换热器，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成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 排气通道在垂直于换热器的中心轴的平面中具有弧形轮廓，以减少排气流的漩涡。 空气通道与排气通道处于热交换关系，并且在空气入口和空气出口之间提供流体流动连通，设计为燃气涡轮发动机的密封相应的气室。
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Patent Agency Ranking
公开(公告)号：US20120216506A1
公开(公告)日：2012-08-30
申请号：US13036407
申请日：2011-02-28
Applicant: Andreas Eleftheriou , David Menheere , Daniel Alecu
Inventor： Andreas Eleftheriou , David Menheere , Daniel Alecu
CPC classification number: F02C7/08 , F05D2220/323 , F05D2230/60 , F05D2230/642 , F28D9/0018 , F28D21/001 , F28F9/0236 , F28F9/26 , F28F21/087 , F28F2230/00 , F28F2265/26 , Y10T29/49716
Abstract: 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.
Abstract translation: 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：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：US08979484B2
公开(公告)日：2015-03-17
申请号：US13344057
申请日：2012-01-05
Applicant: Andreas Eleftheriou , David Menheere , David Denis
Inventor： Andreas Eleftheriou , David Menheere , David Denis
CPC classification number: F01D9/065 , F01D25/162 , F01D25/24 , F05D2230/232 , F05D2230/237
Abstract: A casing for an aircraft turbofan bypass engine includes an outer ring, an inner hub and a plurality of struts radially extending therebetween. An annular portion of an engine core casing having an outer wall and an inner wall, is disposed between the outer ring and inner hub, forming an annular splitter supporting an upstream splitter tip structure. The annular splitter further includes an intermediate wall disposed in the annular splitter fixed to the outer wall and the struts, to distribute loads from the annular splitter box to the struts.
Abstract translation: 用于飞行器涡扇风扇旁路发动机的壳体包括外环，内毂和在它们之间径向延伸的多个支柱。 具有外壁和内壁的发动机芯壳的环形部分设置在外环和内毂之间，形成支撑上游分流器顶端结构的环形分流器。 环形分离器还包括设置在固定到外壁和支柱的环形分配器中的中间壁，以将负载从环形分配箱分配到支柱。
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公开(公告)号：US08801376B2
公开(公告)日：2014-08-12
申请号：US13224379
申请日：2011-09-02
Applicant: Andreas Eleftheriou , David Menheere , Quantai Liu
Inventor： Andreas Eleftheriou , David Menheere , Quantai Liu
IPC: F01D25/14
CPC classification number: F02C7/20 , F05D2230/232
Abstract: A fabricated engine case has a plurality of circumferentially spaced struts radially extending between an outer case and an inner case. A mount apparatus is affixed to the outer case of the engine case. The mount apparatus is a mount base radially spaced apart from a circumferential skin of the outer case and a load bearing member extending radially inwardly to connect the mount base to an outer end of one of the struts.
Abstract translation: 制造的发动机壳体具有在外壳和内壳之间径向延伸的多个周向间隔的支柱。 发动机壳体的外壳附着有安装装置。 安装装置是与外壳的圆周表皮径向间隔开的安装基座和径向向内延伸的承载构件，以将安装基座连接到一个支柱的外端。
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公开(公告)号：US20130298522A1
公开(公告)日：2013-11-14
申请号：US13469712
申请日：2012-05-11
Applicant: Andreas Eleftheriou , David Menheere
Inventor： Andreas Eleftheriou , David Menheere
CPC classification number: F02K3/06 , F02C3/06 , F02C3/107 , F02C7/36 , F05D2260/40311 , Y10T29/49231
Abstract: An assembly for a gas turbine engine, with a gearbox including a first portion having a first input gear coupled to a rotatable turbine shaft, a first output gear, and defining a first transmission path between the first input and output gears, and a second portion having a second input gear coupled to the turbine shaft, a second output gear, and defining a second transmission path between the second input and output gears different from the first transmission path. A fan rotor is coupled to the first output gear and a booster rotor is coupled to the second output gear on a same side of the gearbox than the coupling between the fan rotor and the first output gear. A method of assembling a drive for a fan rotor and a booster rotor in a gas turbine engine is also disclosed.
Abstract translation: 一种用于燃气涡轮发动机的组件，其具有包括第一部分的齿轮箱，第一部分具有联接到可旋转的涡轮轴的第一输入齿轮，第一输出齿轮，并且限定第一输入和输出齿轮之间的第一传动路径，以及第二部分 具有联接到涡轮机轴的第二输入齿轮，第二输出齿轮，并且在不同于第一传动路径的第二输入齿轮和输出齿轮之间限定第二传动路径。 风扇转子联接到第一输出齿轮，并且增强转子与齿轮箱的与风扇转子和第一输出齿轮之间的联接相同的一侧耦合到第二输出齿轮。 还公开了一种在燃气轮机中组装用于风扇转子和升压转子的驱动装置的方法。
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