公开(公告)号：US09297534B2

公开(公告)日：2016-03-29

申请号：US13193865

申请日：2011-07-29

申请人： Joseph Citeno ,  Dmitry Alexandrovitch Lysenko ,  Sergey Anatolievich Meshkov ,  Valery Alexandrovich Mitrofanov ,  Almaz Valeev

发明人： Joseph Citeno ,  Dmitry Alexandrovitch Lysenko ,  Sergey Anatolievich Meshkov ,  Valery Alexandrovich Mitrofanov ,  Almaz Valeev

IPC分类号： F23R3/34 ,  F23R3/28

CPC分类号： F23R3/286 ,  F23R3/343 ,  F23R3/346

摘要： A turbomachine combustor portion includes a combustion chamber. A center injection nozzle is arranged within the combustion chamber and includes a center nozzle inlet and a center nozzle outlet. An outer premixed injection nozzle is positioned radially outward of the center injection nozzle and includes an outer nozzle inlet and an outer nozzle outlet that is arranged upstream of the center nozzle outlet. A late lean injector is positioned downstream of the center nozzle and the outer premixed nozzle. The combustor portion includes a first combustion zone arranged downstream of the outer nozzle outlet, a second combustion zone arranged downstream of the center nozzle outlet, and a third combustion zone arranged further downstream of the center nozzle outlet. The center injection nozzle, outer premixed injection nozzle, and late lean injector are selectively operated to establish a combustion flame front in the first, second, and third combustion zones.

摘要翻译： 涡轮机燃烧器部分包括燃烧室。 中心喷嘴设置在燃烧室内，并包括中心喷嘴入口和中心喷嘴出口。 外部预混合喷嘴位于中心喷嘴的径向外侧，并且包括布置在中心喷嘴出口上游的外喷嘴入口和外喷嘴出口。 后期的稀薄喷射器位于中心喷嘴和外部预混喷嘴的下游。 燃烧器部分包括布置在外部喷嘴出口下游的第一燃烧区域，布置在中心喷嘴出口下游的第二燃烧区域和布置在中心喷嘴出口下游的第三燃烧区域。 选择性地操作中心注射喷嘴，外部预混合喷嘴和后部稀薄喷射器，以在第一，第二和第三燃烧区域中建立燃烧火焰前沿。

公开(公告)号：US20110240769A1

公开(公告)日：2011-10-06

申请号：US12750192

申请日：2010-03-30

申请人： Abdul Rafey Khan ,  Joseph Citeno ,  Christian Xavier Stevenson ,  Baifang Zuo

发明人： Abdul Rafey Khan ,  Joseph Citeno ,  Christian Xavier Stevenson ,  Baifang Zuo

IPC分类号： F02M61/20 ,  B05B1/30

CPC分类号： F23D11/38 ,  F23D14/48 ,  F23R3/36 ,  F23R2900/00002

摘要： A nozzle is provided and includes a circuit by which fuel is delivered to a nozzle part and a valve, interposed between the circuit and the nozzle part and upon which the fuel impinges, an opening and closing of the valve being passively responsive to a fuel pressure in the circuit such that the valve thereby modulates a size of an area through which a corresponding quantity of the fuel flows from the circuit to the nozzle part.

摘要翻译： 提供喷嘴并且包括燃料被输送到喷嘴部分的电路和介于电路和喷嘴部分之间并且燃料撞击的阀门，被动地响应于燃料压力的阀的打开和关闭 在电路中使得阀由此调制相应数量的燃料从电路流到喷嘴部分的区域的尺寸。

公开(公告)号：US07891192B2

公开(公告)日：2011-02-22

申请号：US11892859

申请日：2007-08-28

申请人： Geoffrey David Myers ,  Lewis Berkley Davis, Jr. ,  Joseph Citeno

发明人： Geoffrey David Myers ,  Lewis Berkley Davis, Jr. ,  Joseph Citeno

IPC分类号： F02C1/00

CPC分类号： F23N1/002 ,  F02C9/263 ,  F02C9/28 ,  F05D2270/071 ,  F05D2270/08 ,  F23N5/022 ,  F23N5/082 ,  F23N5/16 ,  F23N2027/04 ,  F23N2035/14 ,  F23N2037/02 ,  F23N2041/20 ,  F23R3/286

摘要： A combustor assembly for a gas turbine engine includes a combustor endcover having at least one fuel circuit and mounted thereto a plurality of pre-mixers and at least one control valve. The at least one control valve is fluidly connected to the at least one fuel circuit and operatively connected to a controller. The controller selectively operates the at least one control valve to deliver fuel through the at least one fuel circuit to the plurality of pre-mixers in order to achieve an enhanced level of operational flexibility by providing individual combustion chamber control.

摘要翻译： 用于燃气涡轮发动机的燃烧器组件包括具有至少一个燃料回路并且安装到其上的多个预混合器和至少一个控制阀的燃烧器端盖。 所述至少一个控制阀流体地连接到所述至少一个燃料回路并可操作地连接到控制器。 控制器选择性地操作至少一个控制阀以将燃料通过至少一个燃料回路输送到多个预混合器，以通过提供单独的燃烧室控制来实现增强的操作灵活性水平。

公开(公告)号：US20100043387A1

公开(公告)日：2010-02-25

申请号：US11933898

申请日：2007-11-01

申请人： Geoffrey David Myers ,  David August Snider ,  Eric Motter ,  Daniel R. Tegel ,  James Harper ,  Stephen R. Watts ,  Joseph Citeno

发明人： Geoffrey David Myers ,  David August Snider ,  Eric Motter ,  Daniel R. Tegel ,  James Harper ,  Stephen R. Watts ,  Joseph Citeno

IPC分类号： F02C9/00 ,  F02C7/22

CPC分类号： F02C7/228

摘要： Methods and systems for delivering fuel in a gas turbine engine are provided. The system includes a plurality of can annular combustors that includes at least a first set of combustors of the plurality of can annular combustors and at least a second set of combustors of the plurality of can annular combustors wherein each set of combustors is supplied by a separately controllable respective fuel delivery system. The method includes supplying fuel at a first fuel schedule to the first set of combustors and supplying fuel at a second fuel schedule to the second set of combustors during a first mode of operation wherein the second fuel schedule is different than the first fuel schedule, and supplying fuel at the second fuel schedule to the first and second sets of combustors during a second mode of operation.

摘要翻译： 提供了用于在燃气涡轮发动机中输送燃料的方法和系统。 该系统包括多个罐式环形燃烧器，其包括多个罐环形燃烧器中的至少第一组燃烧器和多个罐形环形燃烧器的至少第二组燃烧器，其中每组燃烧器由单独的 可控的燃油输送系统。 该方法包括以第一燃料排程向第一组燃料供应燃料，并在第一燃料运行方式下将第二燃料的燃料供应给第二组燃烧器，其中第二燃料计划与第一燃料排程不同，以及 在第二工作模式期间将第二燃料计划的燃料供应给第一和第二组燃烧器。