Nested channel ducts for nozzle construction and the like
    1.
    发明授权
    Nested channel ducts for nozzle construction and the like 有权
    用于喷嘴结构的嵌套通道导管等

    公开(公告)号:US08074452B2

    公开(公告)日:2011-12-13

    申请号:US12124593

    申请日:2008-05-21

    IPC分类号: F02C7/22 F23R3/00

    CPC分类号: F23K5/06 F02C7/222 F23R3/283

    摘要: A multiple conduit system for a gas turbine engine, the multiple conduit system extending between a plurality of conduit inlet and outlets. A channel, adapted for conveying fuel flow, is formed in a surface of a gas turbine engine component. The channel includes at least a first discrete conduit and a second discrete conduit. The first and second discrete conduits are each adapted to direct an independent fluid flow from respective inlets to respective outlets.

    摘要翻译: 一种用于燃气涡轮发动机的多管道系统,多管道系统在多个管道入口和出口之间延伸。 在燃气涡轮发动机部件的表面形成有用于输送燃料流的通道。 通道包括至少第一离散导管和第二离散导管。 第一和第二离散导管各自适于将独立的流体流从相应的入口引导到相应的出口。

    NESTED CHANNEL DUCTS FOR NOZZLE CONSTRUCTION AND THE LIKE
    2.
    发明申请
    NESTED CHANNEL DUCTS FOR NOZZLE CONSTRUCTION AND THE LIKE 有权
    用于喷嘴结构和类似的通道通道

    公开(公告)号:US20090320479A1

    公开(公告)日:2009-12-31

    申请号:US12124593

    申请日:2008-05-21

    IPC分类号: F02C7/24 F02C7/22

    CPC分类号: F23K5/06 F02C7/222 F23R3/283

    摘要: A multiple conduit system for a gas turbine engine, the multiple conduit system extending between a plurality of conduit inlet and outlets. A channel, adapted for conveying fuel flow, is formed in a surface of a gas turbine engine component. The channel includes at least a first discrete conduit and a second discrete conduit. The first and second discrete conduits are each adapted to direct an independent fluid flow from respective inlets to respective outlets.

    摘要翻译: 一种用于燃气涡轮发动机的多管道系统,多管道系统在多个管道入口和出口之间延伸。 在燃气涡轮发动机部件的表面形成有用于输送燃料流的通道。 通道包括至少第一离散导管和第二离散导管。 第一和第二离散导管各自适于将独立的流体流从相应的入口引导到相应的出口。

    Nested channel ducts for nozzle construction and the like
    3.
    发明授权
    Nested channel ducts for nozzle construction and the like 有权
    用于喷嘴结构的嵌套通道导管等

    公开(公告)号:US07028484B2

    公开(公告)日:2006-04-18

    申请号:US10231334

    申请日:2002-08-30

    IPC分类号: F02C7/22 F23R3/00

    CPC分类号: F23K5/06 F02C7/222 F23R3/283

    摘要: A multiple conduit system for a gas turbine engine, the multiple conduit system extending between a plurality of conduit inlet and outlets. A channel is formed in a surface of a gas turbine engine component, and the channel is adapted for conveying a fluid flow from an inlet to an outlet. At least a first sealing member is disposed within the channel and divides the channel into at least a first discrete conduit and a second discrete conduit. A second sealing member encloses the channel to define the second discrete conduit. The first and second discrete conduits are each adapted to direct an independent fluid flow from respective inlets to respective outlets.

    摘要翻译: 一种用于燃气涡轮发动机的多管道系统,多管道系统在多个管道入口和出口之间延伸。 在燃气涡轮发动机部件的表面上形成通道,并且该通道适于将流体流从输入口输出到出口。 至少第一密封构件设置在通道内,并将通道分成至少第一离散导管和第二离散导管。 第二密封构件封闭通道以限定第二离散导管。 第一和第二离散导管各自适于将独立的流体流从相应的入口引导到相应的出口。

    Nested channel ducts for nozzle construction and the like
    4.
    发明申请
    Nested channel ducts for nozzle construction and the like 审中-公开
    用于喷嘴结构的嵌套通道导管等

    公开(公告)号:US20060260317A1

    公开(公告)日:2006-11-23

    申请号:US11338827

    申请日:2006-01-25

    IPC分类号: F02C7/22

    CPC分类号: F23K5/06 F02C7/222 F23R3/283

    摘要: A multiple conduit system for a gas turbine engine, the multiple conduit system extending between a plurality of conduit inlet and outlets. A channel, adapted for conveying fuel flow, is formed in a surface of a gas turbine engine component. The channel includes at least a first discrete conduit and a second discrete conduit. The first and second discrete conduits are each adapted to direct an independent fluid flow from respective inlets to respective outlets.

    摘要翻译: 一种用于燃气涡轮发动机的多管道系统,多管道系统在多个管道入口和出口之间延伸。 在燃气涡轮发动机部件的表面形成有用于输送燃料流的通道。 通道包括至少第一离散导管和第二离散导管。 第一和第二离散导管各自适于将独立的流体流从相应的入口引导到相应的出口。