MULTI-PREMIXER FUEL NOZZLE SUPPORT SYSTEM
    91.
    发明申请
    MULTI-PREMIXER FUEL NOZZLE SUPPORT SYSTEM 有权
    多重燃料燃料喷嘴支持系统

    公开(公告)号:US20100293955A1

    公开(公告)日:2010-11-25

    申请号:US12469507

    申请日:2009-05-20

    CPC classification number: F23R3/10 F23R3/286

    Abstract: A system comprising a fuel nozzle. The fuel nozzle includes a mounting base and an inlet flow conditioner extending directly from the mounting base in a downstream direction. Moreover, the inlet flow conditioner structurally supports the fuel nozzle without a central support member extending directly from the mounting base inside the inlet flow conditioner.

    Abstract translation: 一种包括燃料喷嘴的系统。 燃料喷嘴包括安装基座和沿着下游方向从安装基座直接延伸的入口流动调节器。 此外,入口流动调节器结构地支撑燃料喷嘴,而没有直接从入口流动调节器内的安装基座延伸的中心支撑构件。

    Interlocking Retention Strip
    92.
    发明申请
    Interlocking Retention Strip 有权
    联锁固定带

    公开(公告)号:US20100199628A1

    公开(公告)日:2010-08-12

    申请号:US12366913

    申请日:2009-02-06

    Abstract: An impingement shield assembly for a turbine includes a first impingement shield portion and a second impingement shield joined to the first impingement shield portion. The assembly also includes a first connection portion formed on the first impingement shield portion, a second connection portion formed on the first impingement shield portion and first and second wedge weld portions that mate with and hold the first and a second connection portions in a fixed relationship to one another.

    Abstract translation: 用于涡轮机的冲击屏蔽组件包括第一冲击屏蔽部分和与第一冲击屏蔽部分接合的第二冲击屏蔽。 组件还包括形成在第一冲击屏蔽部分上的第一连接部分,形成在第一冲击屏蔽部分上的第二连接部分和第一和第二楔形焊接部分,第一和第二楔形焊接部分以固定关系与第一和第二连接部分配合 彼此。

    DILUENT SHROUD FOR COMBUSTOR
    95.
    发明申请
    DILUENT SHROUD FOR COMBUSTOR 有权
    公司的DILUENT SHROUD

    公开(公告)号:US20100101204A1

    公开(公告)日:2010-04-29

    申请号:US12260545

    申请日:2008-10-29

    CPC classification number: F23R3/10 F23R3/28

    Abstract: Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one through baffle hole. At least one diluent shroud is affixed to the at least one baffle plate and is configured to guide a diluent flow toward a mixing chamber of the at least one fuel nozzle. Further disclosed is a method for introducing a diluent flow into a mixing chamber of a fuel nozzle including urging the diluent flow from a plenum through a baffle plate gap between a baffle plate and an outer surface of the fuel nozzle. The diluent flow is directed via at least one diluent shroud extending from the baffle plate toward a plurality of air swirler holes extending through a fuel nozzle tip. The diluent flow is flowed through the plurality of air swirler holes into the mixing chamber.

    Abstract translation: 公开了一种燃烧器,其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个通过挡板孔的燃料喷嘴。 至少一个稀释剂护罩固定在所述至少一个挡板上,并被构造成将稀释剂流引向所述至少一个燃料喷嘴的混合室。 进一步公开的是一种将稀释剂流引入燃料喷嘴的混合室中的方法,包括将稀释剂流从气室推压通过挡板和燃料喷嘴的外表面之间的挡板间隙。 稀释剂流经由从挡板延伸的至少一个稀释剂护罩朝向延伸穿过燃料喷嘴尖端的多个空气旋流器引导。 稀释剂流通过多个空气旋流器孔流入混合室。

    METERING OF DILUENT FLOW IN COMBUSTOR
    96.
    发明申请
    METERING OF DILUENT FLOW IN COMBUSTOR 审中-公开
    二氧化碳计量流量

    公开(公告)号:US20100089020A1

    公开(公告)日:2010-04-15

    申请号:US12250933

    申请日:2008-10-14

    CPC classification number: F23R3/04 F23R3/002 F23R3/10 F23R3/283 F23R3/286

    Abstract: Disclosed is a combustor including a baffle plate having at least one through baffle hole and at least one fuel nozzle extending through the at least one baffle hole. A circumferentially adjustable collar is located at the at least one baffle hole between the baffle plate and the at least one fuel nozzle. A plurality of openings at the collar are configured to meter a flow of diluent between the baffle hole and the at least one fuel nozzle. Further disclosed is a method for providing diluent to a combustor including providing a plurality of openings disposed at a circumferentially adjustable collar between a baffle plate and at least one fuel nozzle extending through a through hole in the baffle plate. The diluent is flowed through the plurality of openings toward at least one airflow hole in the at least one fuel nozzle.

    Abstract translation: 公开了一种燃烧器,其包括具有至少一个通过挡板孔的挡板和至少一个延伸穿过至少一个挡板孔的燃料喷嘴。 一个可周向调节的套环位于挡板和至少一个燃料喷嘴之间的至少一个挡板孔处。 在轴环处的多个开口被配置成测量在挡板孔和至少一个燃料喷嘴之间的稀释剂流。 还公开了一种用于向燃烧器提供稀释剂的方法,包括提供设置在挡板和至少一个延伸穿过挡板中的通孔的燃料喷嘴之间的周向可调环圈处的多个开口。 稀释剂通过多个开口朝向至少一个燃料喷嘴中的至少一个气流孔流动。

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