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38 条记录 (耗时 0.02 秒)

    Combustor liner v-band design
    1.
    发明申请
    Combustor liner v-band design 有权
    燃烧器衬管v带设计

    公开(公告)号：US20070234726A1

    公开(公告)日：2007-10-11

    申请号：US11226442

    申请日：2005-09-15

    申请人： Bhawan Patel ,  Parthasarathy Sampath ,  Jason Fish

    发明人： Bhawan Patel ,  Parthasarathy Sampath ,  Jason Fish

    IPC分类号： F23R3/00

    CPC分类号： F23R3/54 ,  F23R3/06 ,  F23R3/60 ,  F23R2900/03042

    摘要： A combustor wall louver for ducting a flow of compressed air through an inlet opening in the combustor wall from a source of compressed air outside the combustor where the louver is a circumferentially extending member, mounted to an interior surface of the combustor wall and covering the inlet opening with outlet openings fed by a channel in flow communication between each outlet opening and the inlet opening. Preferably, the circumferential member is made of arcuate segments of cast metal removably mounted to the interior surface of the combustor wall with threaded studs.

    摘要翻译： 一种燃烧器壁板百叶窗，用于将压缩空气流通过燃烧器壁中的入口开口从燃烧器外部的压缩空气源引导，其中百叶窗是周向延伸的构件，安装到燃烧器壁的内表面并覆盖入口 开口具有通过每个出口与入口之间流动连通的通道供给的出口。 优选地，周向构件由可拆卸地安装到具有螺柱的燃烧器壁的内表面的铸造金属的弓形段制成。

    Gas turbine engine combustor with improved cooling
    3.
    发明申请
    Gas turbine engine combustor with improved cooling 有权
    燃气轮机发动机燃烧器具有改进的冷却

    公开(公告)号：US20070006588A1

    公开(公告)日：2007-01-11

    申请号：US11175046

    申请日：2005-07-06

    申请人： Bhawan Patel ,  Parthasarathy Sampath ,  Russell Parker

    发明人： Bhawan Patel ,  Parthasarathy Sampath ,  Russell Parker

    IPC分类号： F23R3/42

    CPC分类号： F23R3/42 ,  F23R3/10

    摘要： A gas turbine engine combustor liner having a plurality of holes defined therein for directing air into the combustion chamber. The plurality of holes provide improved cooling efficiency in regions of the combustor dome corresponding to predetermined hotspots.

    摘要翻译： 一种燃气涡轮发动机燃烧器衬套，其具有限定在其中的多个孔，用于将空气引导到燃烧室中。 多个孔在对应于预定热点的燃烧室顶部的区域中提供改善的冷却效率。

    Gas turbine internal manifold mounting arrangement
    7.
    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：US07721546B2

    公开(公告)日：2010-05-25

    申请号：US11488801

    申请日：2006-07-19

    申请人： Jason Fish ,  Bhawan Patel

    发明人： Jason Fish ,  Bhawan Patel

    IPC分类号： F02C1/00 ,  F02G3/00

    CPC分类号： F02C7/222 ,  F23R3/283

    摘要： A mounting system for an annular internal fuel manifold of a gas turbine engine includes three supports equally spaced apart about the annular fuel manifold, the three supports having at least two pin supports disposed between the fuel manifold and a surrounding gas generator casing. Each pin support includes a radially extending pin co-operating with an aligned ring slidingly disposed around the pin for relative sliding displacement therebetween. The pin supports providing axial constraint while permitting the fuel manifold to radially displace relative to the surrounding gas generator casing due to thermal size change.

    摘要翻译： 用于燃气涡轮发动机的环形内部燃料歧管的安装系统包括围绕环形燃料歧管等间隔开的三个支撑件，三个支撑件具有设置在燃料歧管和周围的气体发生器壳体之间的至少两个销支撑件。 每个销支撑件包括径向延伸的销，其与滑动地布置在销周围的对准的环配合，以在它们之间进行相对的滑动位移。 销支撑提供轴向约束，同时由于热尺寸变化允许燃料歧管相对于周围的气体发生器壳体径向移位。

    Gas turbine internal manifold mounting arrangement
    8.
    发明申请
    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：US20080016869A1

    公开(公告)日：2008-01-24

    申请号：US11488801

    申请日：2006-07-19

    申请人： Jason Fish ,  Bhawan Patel

    发明人： Jason Fish ,  Bhawan Patel

    IPC分类号： F02C1/00

    CPC分类号： F02C7/222 ,  F23R3/283

    摘要： A mounting system for an annular internal fuel manifold of a gas turbine engine includes three supports equally spaced apart about the annular fuel manifold, the three supports having at least two pin supports disposed between the fuel manifold and a surrounding gas generator casing. Each pin support includes a radially extending pin co-operating with an aligned ring slidingly disposed around the pin for relative sliding displacement therebetween. The pin supports providing axial constraint while permitting the fuel manifold to radially displace relative to the surrounding gas generator casing due to thermal size change.

    摘要翻译： 用于燃气涡轮发动机的环形内部燃料歧管的安装系统包括围绕环形燃料歧管等间隔开的三个支撑件，三个支撑件具有设置在燃料歧管和周围的气体发生器壳体之间的至少两个销支撑件。 每个销支撑件包括径向延伸的销，其与滑动地布置在销周围的对准的环配合，以在它们之间进行相对的滑动位移。 销支撑提供轴向约束，同时由于热尺寸变化允许燃料歧管相对于周围的气体发生器壳体径向移位。

    FUEL MANIFOLD INLET TUBE
    9.
    发明申请
    FUEL MANIFOLD INLET TUBE 有权
    燃油管道入口管

    公开(公告)号：US20070163265A1

    公开(公告)日：2007-07-19

    申请号：US11669493

    申请日：2007-01-31

    申请人： Jason FISH ,  Bhawan Patel

    发明人： Jason FISH ,  Bhawan Patel

    IPC分类号： F02C7/26

    CPC分类号： F02C7/222

    摘要： An inlet tube supplies fuel to a manifold of a combustor in a gas turbine engine, the manifold defining a manifold plane. The inlet tube comprises a tube body having a channel providing fluid flow communication between first and second ends of the tube body. At least a portion of the channel defines a tube body plane which is spaced apart from the manifold plane.

    摘要翻译： 入口管将燃料供应到燃气涡轮发动机中的燃烧器的歧管，歧管限定歧管平面。 入口管包括管体，其具有提供管体的第一和第二端之间的流体流动连通的通道。 通道的至少一部分限定了与歧管平面间隔开的管体平面。