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    GAS TURBINE INTERNAL MANIFOLD MOUNTING ARRANGEMENT
    1.
    发明申请
    GAS TURBINE INTERNAL MANIFOLD MOUNTING ARRANGEMENT 有权
    气体涡轮内部安装安装

    公开(公告)号：US20120186257A1

    公开(公告)日：2012-07-26

    申请号：US13440528

    申请日：2012-04-05

    申请人： Jason FISH ,  Bryan Olver

    发明人： Jason FISH ,  Bryan Olver

    IPC分类号： F02C7/22 ,  B23P11/00

    CPC分类号： F02C7/222 ,  Y10T29/4932

    摘要： A mounting method and system for supporting and positioning an internal fuel manifold relative to a combustor in a fuel injection system for a gas turbine engine. The method includes positioning the fuel manifold within a gas generator casing, applying a heat shield around a radially extending fuel inlet connected to the fuel manifold, and using the heat shield to at least partially support the fuel manifold within the gas generator casing.

    摘要翻译： 一种用于在用于燃气涡轮发动机的燃料喷射系统中相对于燃烧器支撑和定位内部燃料歧管的安装方法和系统。 该方法包括将燃料歧管定位在气体发生器壳体内，围绕连接到燃料歧管的径向延伸的燃料入口施加隔热罩，并且使用隔热罩至少部分地支撑燃气发生器壳体内的燃料歧管。

    GAS TURBINE INTERNAL MANIFOLD MOUNTING ARRANGEMENT
    2.
    发明申请
    GAS TURBINE INTERNAL MANIFOLD MOUNTING ARRANGEMENT 有权
    气体涡轮内部安装安装

    公开(公告)号：US20080092545A1

    公开(公告)日：2008-04-24

    申请号：US11552249

    申请日：2006-10-24

    申请人： Jason Fish ,  Bryan Olver

    发明人： Jason Fish ,  Bryan Olver

    IPC分类号： F02C1/00

    CPC分类号： F02C7/222 ,  Y10T29/4932

    摘要： A mounting system supporting and positioning an internal fuel manifold of a gas turbine engine includes at least a heat shield surrounding a fuel inlet of the fuel manifold, the heat shield bearing at least a portion of a load to support the fuel manifold.

    摘要翻译： 支撑和定位燃气涡轮发动机的内部燃料歧管的安装系统包括至少围绕燃料歧管的燃料入口的隔热罩，所述隔热板承载用于支撑燃料歧管的负载的至少一部分。

    Side-fed shielded internal fuel manifold inlet tube
    3.
    发明申请
    Side-fed shielded internal fuel manifold inlet tube 有权
    侧向屏蔽内部燃料歧管入口管

    公开(公告)号：US20050160738A1

    公开(公告)日：2005-07-28

    申请号：US10764578

    申请日：2004-01-27

    申请人： Jason Fish ,  Bryan Olver ,  Vittorio Bruno

    发明人： Jason Fish ,  Bryan Olver ,  Vittorio Bruno

    IPC分类号： F02C7/22 ,  F23R3/28

    CPC分类号： F02C7/222

    摘要： In a gas turbine engine, a fuel inlet tube comprising a body, a channel defined in the body and in fluid communication with a manifold, and a side inlet in fluid communication with the channel, such that fuel entering the side inlet is delivered to the manifold through the channel with a pressure generally directed along a radial axis of the body. Also, a fuel inlet tube comprising a heat shield surrounding at least part of a body, a chamber defined between the heat shield and the body and in fluid communication with fuel leak sources, a drain channel defined in the body in fluid communication with the chamber, and a drain hole defined in the body in fluid communication with the drain channel, such that a leak produces fuel received in the chamber and safely directed through the channel and the hole to allow detection of the leak.

    摘要翻译： 在燃气涡轮发动机中，燃料入口管包括主体，限定在主体中并与歧管流体连通的通道以及与通道流体连通的侧入口，使得进入侧入口的燃料被输送到 通过通道的歧管，其压力通常沿身体的径向轴线引导。 另外，一种燃料入口管，其包括围绕主体的至少一部分的隔热罩，限定在隔热罩和主体之间并与燃料泄漏源流体连通的腔室;限定在主体中的与腔室流体连通的排放通道 ，以及限定在主体中的排水孔，其与排水通道流体连通，使得泄漏产生在室中接收的燃料并且安全地引导通过通道和孔以允许检测泄漏。

    Gas turbine internal manifold mounting arrangement
    4.
    发明授权
    Gas turbine internal manifold mounting arrangement 有权
    燃气轮机内部歧管安装布置

    公开(公告)号：US09068508B2

    公开(公告)日：2015-06-30

    申请号：US13440528

    申请日：2012-04-05

    申请人： Jason Fish ,  Bryan Olver

    发明人： Jason Fish ,  Bryan Olver

    IPC分类号： F02C7/20 ,  F02C7/22

    CPC分类号： F02C7/222 ,  Y10T29/4932

    摘要： A mounting method and system for supporting and positioning an internal fuel manifold relative to a combustor in a fuel injection system for a gas turbine engine. The method includes positioning the fuel manifold within a gas generator casing, applying a heat shield around a radially extending fuel inlet connected to the fuel manifold, and using the heat shield to at least partially support the fuel manifold within the gas generator casing.

    摘要翻译： 一种用于在用于燃气涡轮发动机的燃料喷射系统中相对于燃烧器支撑和定位内部燃料歧管的安装方法和系统。 该方法包括将燃料歧管定位在气体发生器壳体内，围绕连接到燃料歧管的径向延伸的燃料入口施加隔热罩，并且使用隔热罩至少部分地支撑燃气发生器壳体内的燃料歧管。

    Gas turbine internal manifold mounting arrangement
    5.
    发明授权
    Gas turbine internal manifold mounting arrangement 有权
    燃气轮机内部歧管安装布置

    公开(公告)号：US08171738B2

    公开(公告)日：2012-05-08

    申请号：US11552249

    申请日：2006-10-24

    申请人： Jason Fish ,  Bryan Olver

    发明人： Jason Fish ,  Bryan Olver

    IPC分类号： F02C1/00

    CPC分类号： F02C7/222 ,  Y10T29/4932

    摘要： A mounting system supporting and positioning an internal fuel manifold of a gas turbine engine includes at least a heat shield surrounding a fuel inlet of the fuel manifold, the heat shield bearing at least a portion of a load to support the fuel manifold.

    摘要翻译： 支撑和定位燃气涡轮发动机的内部燃料歧管的安装系统包括至少围绕燃料歧管的燃料入口的隔热罩，所述隔热板承载用于支撑燃料歧管的负载的至少一部分。

    Bypass lip seal
    6.
    发明申请
    Bypass lip seal 审中-公开
    旁路唇密封

    公开(公告)号：US20080053060A1

    公开(公告)日：2008-03-06

    申请号：US11511443

    申请日：2006-08-29

    申请人： Bryan Olver

    发明人： Bryan Olver

    IPC分类号： F02K3/02

    CPC分类号： F02K3/04 ,  F01D25/18 ,  F02C7/14 ,  F05D2240/12 ,  Y02T50/675

    摘要： A cooling apparatus for cooling a fluid in a bypass gas turbine engine comprises a heat exchanger disposed within a bypass duct and accommodated by a sub-passage defined by a flow divider affixed to an annular wall of the bypass duct. The sub-passage defines an open upstream end and an open downstream end to direct a portion of the bypass air flow to pass therethrough. A sealing assembly for the bypass duct is also provided.

    摘要翻译： 用于冷却旁路燃气涡轮发动机中的流体的冷却装置包括设置在旁通管道内的热交换器，并且由通过固定到旁通管道的环形壁的分流器限定的子通道容纳。 子通道限定开放的上游端和敞开的下游端，以引导旁路空气流的一部分通过。 还提供了用于旁路管道的密封组件。

    Grommeted bypass duct penetration
    9.
    发明申请
    Grommeted bypass duct penetration 审中-公开
    引导旁路管穿透

    公开(公告)号：US20060288687A1

    公开(公告)日：2006-12-28

    申请号：US11178282

    申请日：2005-12-08

    申请人： Vittorio Bruno ,  Goll Hadi ,  Bryan Olver

    发明人： Vittorio Bruno ,  Goll Hadi ,  Bryan Olver

    IPC分类号： F02K3/04

    CPC分类号： F01D9/065 ,  F01D11/005 ,  F05D2230/642 ,  Y10T16/063

    摘要： A bypass duct sealing grommet, for sealing between an opening in a gas turbine engine bypass duct wall and an external surface of a projection extending through the opening, where the grommet has an annular body with a central aperture having an internal periphery adapted to sealingly engage the external surface of the projection. A first flange and a second flange define an external slot about an exterior periphery of the body adapted to receive and seal the bypass duct wall between the flanges.

    摘要翻译： 旁通管道密封垫圈，用于密封燃气涡轮发动机旁通管壁中的开口和延伸穿过开口的突出部的外表面，其中，索环具有环形体，中心孔具有适于密封接合的内周边 投影的外表面。 第一凸缘和第二凸缘限定围绕本体的外周的外槽，其适于容纳和密封凸缘之间的旁通管壁。

    INTERNAL FUEL MANIFOLD AND FUEL FAIRING INTERFACE
    10.
    发明申请
    INTERNAL FUEL MANIFOLD AND FUEL FAIRING INTERFACE 有权
    内燃燃油和燃油接口

    公开(公告)号：US20080072601A1

    公开(公告)日：2008-03-27

    申请号：US11534246

    申请日：2006-09-22

    申请人： Oleg MORENKO ,  Bryan Olver

    发明人： Oleg MORENKO ,  Bryan Olver

    IPC分类号： F02C1/00

    CPC分类号： F02C7/222 ,  F02C3/145

    摘要： A mounting system for an annular internal fuel manifold disposed within a gas turbine engine includes a fuel inlet assembly having a heat shield extending about at least a portion of an inner fuel inlet tube. The heat shield has a distal end engaged with the fuel manifold and has a radially outwardly projecting shoulder proximate an opposed proximal end thereof. The proximal end of the heat shield is received within a bushing disposed within a corresponding opening of a supporting casing. The shoulder of the heat shield retains the bushing in place.

    摘要翻译： 设置在燃气涡轮发动机内的环形内部燃料歧管的安装系统包括燃料入口组件，其具有围绕内部燃料入口管的至少一部分延伸的隔热罩。 隔热罩具有与燃料歧管接合的远端，并且在其相对的近端处具有径向向外突出的肩部。 隔热罩的近端容纳在设置在支撑壳体的相应开口内的衬套内。 隔热罩的肩部将衬套保持在适当的位置。