公开(公告)号：WO2017002076A1

公开(公告)日：2017-01-05

申请号：PCT/IB2016/053944

申请日：2016-06-30

Applicant: ANSALDO ENERGIA IP UK LIMITED

Inventor： MCNALLY, Joshua R. ,  PENNEL, Douglas ,  GAUTHIER, Donald ,  MATYS, Pawel ,  PASKIN, Marc ,  RUCK, Thomas R. ,  STUTTAFORD, Peter John ,  SAM, Bernard Tam-Yen ,  JORGENSEN, Stephen W.

IPC: F23R3/14 ,  F23R3/16 ,  F23R3/26 ,  F23R3/28 ,  F23R3/34 ,  F23R3/54 ,  F23L7/00 ,  F23K5/18

CPC classification number: F23R3/14 ,  F23K5/18 ,  F23L7/002 ,  F23R3/16 ,  F23R3/26 ,  F23R3/286 ,  F23R3/34 ,  F23R3/343 ,  F23R3/54 ,  F23R2900/03343

Abstract: Gas turbine combustion systems and fuel cartridge assemblies are provided. An exemplary combustion system may comprise a combustor including a cylindrical combustion liner, a flow sleeve, a main mixer, a radial inflow swirler, a combustor dome, and a fuel cartridge assembly. An exemplary combustor and/or fuel cartridge assembly may comprise first and second fuel circuits or manifolds. Methods and systems are also provided for staging and controlling a flow of fuel and/or water through different fuel circuits and pilot injectors, to allow purging and ignition using different fuel circuits, pilot injectors, and fuel sources.

Abstract translation: 提供燃气轮机燃烧系统和燃料盒组件。 示例性燃烧系统可以包括燃烧器，该燃烧器包括圆柱形燃烧衬套，流动套筒，主混合器，径向流入旋流器，燃烧器圆顶和燃料盒组件。 示例性燃烧器和/或燃料盒组件可以包括第一和第二燃料回路或歧管。 还提供了方法和系统，用于通过不同的燃料回路和引燃喷射器分级和控制燃料和/或水的流动，​​以允许使用不同的燃料回路，引燃喷射器和燃料源进行清洗和点火。

公开(公告)号：WO2017002075A3

公开(公告)日：2017-01-05

申请号：PCT/IB2016/053943

申请日：2016-06-30

Applicant: ANSALDO ENERGIA IP UK LIMITED

Inventor： MCNALLY, Joshua R. ,  PENNEL, Douglas ,  GAUTHIER, Donald ,  MATYS, Pawel ,  PASKIN, Marc ,  RUCK, Thomas R. ,  STUTTAFORD, Peter John ,  SAM, Bernard Tam-Yen ,  JORGENSEN, Stephen W.

IPC: F23R3/16 ,  F23R3/28 ,  F23R3/34 ,  F23R3/54 ,  F23R3/14 ,  F23R3/44 ,  F23R3/20

Abstract: Systems and methods for dual-fuel operation of a gas turbine combustor are provided. An exemplary gas turbine combustor may comprise one or more components, such as a cylindrical combustion liner, a flow sleeve, a main mixer, a radial inflow swirler, a combustor dome, and a fuel cartridge assembly, one or more of which may be configured to supply either a gaseous or a liquid fuel to the combustion liner, depending on whether gaseous fuel operation or liquid fuel operation of the combustor is desired.

公开(公告)号：WO2017002075A2

公开(公告)日：2017-01-05

申请号：PCT/IB2016/053943

申请日：2016-06-30

Applicant: ANSALDO ENERGIA IP UK LIMITED

Inventor： MCNALLY, Joshua R. ,  PENNEL, Douglas ,  GAUTHIER, Donald ,  MATYS, Pawel ,  PASKIN, Marc ,  RUCK, Thomas R. ,  STUTTAFORD, Peter John ,  SAM, Bernard Tam-Yen ,  JORGENSEN, Stephen W.

CPC classification number: F23R3/346 ,  F02C7/222 ,  F02C7/232 ,  F05D2220/32 ,  F05D2230/237 ,  F05D2260/14 ,  F05D2260/30 ,  F05D2260/99 ,  F23R3/002 ,  F23R3/14 ,  F23R3/20 ,  F23R3/283 ,  F23R3/286 ,  F23R3/343 ,  F23R3/36 ,  F23R3/44 ,  F23R3/54

Abstract: Systems and methods for dual-fuel operation of a gas turbine combustor are provided. An exemplary gas turbine combustor may comprise one or more components, such as a cylindrical combustion liner, a flow sleeve, a main mixer, a radial inflow swirler, a combustor dome, and a fuel cartridge assembly, one or more of which may be configured to supply either a gaseous or a liquid fuel to the combustion liner, depending on whether gaseous fuel operation or liquid fuel operation of the combustor is desired.

Abstract translation: 提供了用于燃气轮机燃烧器的双燃料操作的系统和方法。 示例性的燃气轮机燃烧器可以包括一个或多个部件，诸如圆柱形燃烧衬套，流动套筒，主混合器，径向流入旋流器，燃烧器圆顶和燃料盒组件，其中的一个或多个可以被配置 根据是否需要气体燃料操作或燃烧器的液体燃料操作，将气体或液体燃料供应到燃烧衬套。

公开(公告)号：WO2017002074A1

公开(公告)日：2017-01-05

申请号：PCT/IB2016/053942

申请日：2016-06-30

Applicant: ANSALDO ENERGIA IP UK LIMITED

Inventor： MCNALLY, Joshua R. ,  PENNEL, Douglas ,  GAUTHIER, Donald ,  MATYS, Pawel ,  PASKIN, Marc ,  RUCK, Thomas R. ,  STUTTAFORD, Peter John ,  SAM, Bernard Tam-Yen ,  JORGENSEN, Stephen W.

IPC: F23R3/16 ,  F23R3/28 ,  F23R3/34 ,  F23R3/54 ,  F23R3/14

CPC classification number: F23R3/16 ,  F23R3/14 ,  F23R3/286 ,  F23R3/34 ,  F23R3/343 ,  F23R3/54

Abstract: Gas turbine combustion systems and fuel cartridge assemblies are provided. An exemplary combustion system may comprise a combustor including one or more components, such as a cylindrical combustion liner, a flow sleeve, a main mixer, a radial inflow swirler, a combustor dome, and a fuel cartridge assembly. An exemplary fuel cartridge assembly may comprise first and second fuel manifolds which are connected to respective fuel circuits which supply fuel, such as liquid fuel, through a plurality of fuel passages within the fuel cartridge assembly or to other locations within an associated combustor. The fuel cartridge assembly may further include a plurality of fuel injector tips located at a tip plate of the fuel cartridge assembly through which fuel may be supplied to an associated combustor.

Abstract translation: 提供燃气轮机燃烧系统和燃料盒组件。 示例性燃烧系统可包括包括一个或多个部件的燃烧器，例如圆柱形燃烧衬套，流动套筒，主混合器，径向流入旋流器，燃烧器圆顶和燃料盒组件。 示例性的燃料盒组件可以包括第一和第二燃料歧管，其连接到通过燃料盒组件内的多个燃料通道或相关燃烧器内的其它位置供应诸如液体燃料的燃料的各个燃料回路。 燃料盒组件还可以包括位于燃料盒组件的顶板处的多个燃料喷射器尖端，燃料可以通过燃料喷射器提供给相关联的燃烧器。