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1.发明授权Liquid cartridge with passively fueled premixed air blast circuit for gas operation 有权液体盒带有被动燃料的预混气鼓风回路用于气体操作公开(公告)号：US09261279B2
公开(公告)日：2016-02-16
申请号：US13480896
申请日：2012-05-25
摘要： A gas/liquid fuel nozzle assembly includes a premixing tube bundle having an array of mixing tubes, a fuel plenum delivering fuel to the mixing tubes, a cartridge tube disposed within the fuel plenum, and a liquid fuel cartridge disposed in the cartridge tube. The liquid fuel cartridge is spaced from the cartridge tube to define an annulus. The cartridge tube and the fuel plenum are constructed in fluid communication such that gas fuel in the plenum is injected into the annulus.
摘要翻译： 气体/液体燃料喷嘴组件包括具有混合管阵列的预混合管束，将燃料输送到混合管的燃料增压室，设置在燃料增压室内的筒管和设置在筒管中的液体燃料盒。 液体燃料盒与筒管间隔开以限定环形空间。 筒管和燃料增压室被构造成流体连通，使得气室中的气体燃料被注入到环空中。
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2.发明申请Liquid Cartridge with Passively Fueled Premixed Air Blast Circuit for Gas Operation 有权用于气体操作的带有被动燃料预混气爆炸电路的液体盒公开(公告)号：US20130312422A1
公开(公告)日：2013-11-28
申请号：US13480896
申请日：2012-05-25
摘要： A gas/liquid fuel nozzle assembly includes a premixing tube bundle having an array of mixing tubes, a fuel plenum delivering fuel to the mixing tubes, a cartridge tube disposed within the fuel plenum, and a liquid fuel cartridge disposed in the cartridge tube. The liquid fuel cartridge is spaced from the cartridge tube to define an annulus. The cartridge tube and the fuel plenum are constructed in fluid communication such that gas fuel in the plenum is injected into the annulus.
摘要翻译： 气体/液体燃料喷嘴组件包括具有混合管阵列的预混合管束，将燃料输送到混合管的燃料增压室，设置在燃料增压室内的筒管和设置在筒管中的液体燃料盒。 液体燃料盒与筒管间隔开以限定环形空间。 筒管和燃料增压室被构造成流体连通，使得气室中的气体燃料被注入到环空中。
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公开(公告)号：US09163839B2
公开(公告)日：2015-10-20
申请号：US13423894
申请日：2012-03-19
CPC分类号： F23R3/286
摘要： Embodiments of the present application can provide systems and methods for a micromixer combustion head end assembly. The micromixer may include one or more base nozzle structures. The base nozzle structures may include coaxial tubes. The coaxial tubes may include an inner tube and an outer tube. The micromixer may also include one or more segmented mixing tube bundles at least partially supported by a respective base nozzle structure. Moreover, the micromixer may include an end cap assembly disposed about the one or more segmented mixing tube bundles.
摘要翻译： 本申请的实施例可以提供用于微混合器燃烧头端组件的系统和方法。 微混合器可以包括一个或多个基本喷嘴结构。 基座喷嘴结构可以包括同轴管。 同轴管可包括内管和外管。 微混合器还可以包括至少部分由相应的基座喷嘴结构支撑的一个或多个分段的混合管束。 此外，微混合器可以包括围绕一个或多个分段的混合管束设置的端盖组件。
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公开(公告)号：US20130247581A1
公开(公告)日：2013-09-26
申请号：US13425950
申请日：2012-03-21
IPC分类号： F02C7/24
CPC分类号： F23R3/286 , F02C7/24 , F05D2260/963 , F23M20/005 , F23R3/32 , F23R2900/00014 , F23R2900/03044
摘要： Embodiments of the present application can provide systems and methods for dampening combustor dynamics. According to one embodiment, the system may include a micromixer. The system may also include at least one annular resonator disposed within the micromixer adjacent to a cap face plate or an impingement plate of the micromixer. The at least one annular resonator may include a first side including a number of holes forming a cold side hole pattern, a second side including a number of holes forming a hot side hole pattern, and a cavity substantially defined by the first side and the second side.
摘要翻译： 本申请的实施例可以提供用于衰减燃烧室动力学的系统和方法。 根据一个实施例，系统可以包括微混合器。 该系统还可以包括设置在微型混合器内的至少一个环形谐振器，其邻近盖板或微型混合器的冲击板。 所述至少一个环形谐振器可以包括包括形成冷侧孔图案的多个孔的第一侧，包括形成热侧孔图案的多个孔的第二侧和基本上由第一侧和第二侧形成的空腔 侧。
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5.发明授权公开(公告)号：US09188342B2
公开(公告)日：2015-11-17
申请号：US13425950
申请日：2012-03-21
CPC分类号： F23R3/286 , F02C7/24 , F05D2260/963 , F23M20/005 , F23R3/32 , F23R2900/00014 , F23R2900/03044
摘要： Embodiments of the present application can provide systems and methods for dampening combustor dynamics. According to one embodiment, the system may include a micromixer. The system may also include at least one annular resonator disposed within the micromixer adjacent to a cap face plate or an impingement plate of the micromixer. The at least one annular resonator may include a first side including a number of holes forming a cold side hole pattern, a second side including a number of holes forming a hot side hole pattern, and a cavity substantially defined by the first side and the second side.
摘要翻译： 本申请的实施例可以提供用于衰减燃烧室动力学的系统和方法。 根据一个实施例，系统可以包括微混合器。 该系统还可以包括设置在微型混合器内的至少一个环形谐振器，其邻近盖板或微型混合器的冲击板。 所述至少一个环形谐振器可以包括包括形成冷侧孔图案的多个孔的第一侧，包括形成热侧孔图案的多个孔的第二侧和基本上由第一侧和第二侧形成的空腔 侧。
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6.发明申请TURBOMACHINE COMBUSTOR NOZZLE INCLUDING A MONOLITHIC NOZZLE COMPONENT AND METHOD OF FORMING THE SAME 有权涡轮喷雾器喷嘴，包括单声道喷嘴组件及其形成方法公开(公告)号：US20130318975A1
公开(公告)日：2013-12-05
申请号：US13482540
申请日：2012-05-29
申请人： Lucas John Stoia , Patrick Benedict Melton , Thomas Edward Johnson , Christian Xavier Stevenson , John Drake Vanselow , James Harold Westmoreland
发明人： Lucas John Stoia , Patrick Benedict Melton , Thomas Edward Johnson , Christian Xavier Stevenson , John Drake Vanselow , James Harold Westmoreland
CPC分类号： F23R3/283 , F23R3/286 , F23R2900/00017 , F23R2900/00018 , Y10T29/49323
摘要： A turbomachine combustor nozzle includes a monolithic nozzle component having a plate element and a plurality of nozzle elements. Each of the plurality of nozzle elements includes a first end extending from the plate element to a second end. The plate element and plurality of nozzle elements are formed as a unitary component. A plate member is joined with the nozzle component. The plate member includes an outer edge that defines first and second surfaces and a plurality of openings extending between the first and second surfaces. The plurality of openings are configured and disposed to register with and receive the second end of corresponding ones of the plurality of nozzle elements.
摘要翻译： 涡轮机燃烧器喷嘴包括具有板元件和多个喷嘴元件的单片喷嘴部件。 多个喷嘴元件中的每一个包括从板元件延伸到第二端的第一端。 板元件和多个喷嘴元件形成为整体部件。 板构件与喷嘴部件接合。 板构件包括限定第一和第二表面的外边缘和在第一和第二表面之间延伸的多个开口。 多个开口被配置和设置成与多个喷嘴元件中对应的喷嘴元件的对应的第二端对准并接收。
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公开(公告)号：US20130318976A1
公开(公告)日：2013-12-05
申请号：US13482584
申请日：2012-05-29
CPC分类号： F23D14/62 , F23R3/283 , F23R3/286 , F23R2900/00018 , Y10T29/49323
摘要： A turbomachine combustor nozzle includes a first plate member having a first plurality of openings, and a second plate member having a second plurality of openings that are configured and disposed to be in alignment with the first plurality of openings. A plurality of nozzle members extends through corresponding ones of the first plurality of openings and the second plurality of openings. Each of the plurality of nozzle members includes a solid core.
摘要翻译： 涡轮机燃烧器喷嘴包括具有第一多个开口的第一板构件和具有第二多个开口的第二板构件，第二多个开口被构造和设置成与第一多个开口对准。 多个喷嘴构件延伸穿过第一多个开口和第二多个开口中的相应的开口。 多个喷嘴构件中的每一个包括实芯。
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公开(公告)号：US20130241089A1
公开(公告)日：2013-09-19
申请号：US13423894
申请日：2012-03-19
CPC分类号： F23R3/286
摘要： Embodiments of the present application can provide systems and methods for a micromixer combustion head end assembly. The micromixer may include one or more base nozzle structures. The base nozzle structures may include coaxial tubes. The coaxial tubes may include an inner tube and an outer tube. The micromixer may also include one or more segmented mixing tube bundles at least partially supported by a respective base nozzle structure. Moreover, the micromixer may include an end cap assembly disposed about the one or more segmented mixing tube bundles.
摘要翻译： 本申请的实施例可以提供用于微混合器燃烧头端组件的系统和方法。 微混合器可以包括一个或多个基本喷嘴结构。 基座喷嘴结构可以包括同轴管。 同轴管可包括内管和外管。 微混合器还可以包括至少部分由相应的基座喷嘴结构支撑的一个或多个分段的混合管束。 此外，微混合器可以包括围绕一个或多个分段的混合管束设置的端盖组件。
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9.发明授权Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same 有权涡轮机燃烧器喷嘴包括单片喷嘴部件及其形成方法公开(公告)号：US09267690B2
公开(公告)日：2016-02-23
申请号：US13482540
申请日：2012-05-29
申请人： Lucas John Stoia , Patrick Benedict Melton , Thomas Edward Johnson , Christian Xavier Stevenson , John Drake Vanselow , James Harold Westmoreland
发明人： Lucas John Stoia , Patrick Benedict Melton , Thomas Edward Johnson , Christian Xavier Stevenson , John Drake Vanselow , James Harold Westmoreland
CPC分类号： F23R3/283 , F23R3/286 , F23R2900/00017 , F23R2900/00018 , Y10T29/49323
摘要： A turbomachine combustor nozzle includes a monolithic nozzle component having a plate element and a plurality of nozzle elements. Each of the plurality of nozzle elements includes a first end extending from the plate element to a second end. The plate element and plurality of nozzle elements are formed as a unitary component. A plate member is joined with the nozzle component. The plate member includes an outer edge that defines first and second surfaces and a plurality of openings extending between the first and second surfaces. The plurality of openings are configured and disposed to register with and receive the second end of corresponding ones of the plurality of nozzle elements.
摘要翻译： 涡轮机燃烧器喷嘴包括具有板元件和多个喷嘴元件的单片喷嘴部件。 多个喷嘴元件中的每一个包括从板元件延伸到第二端的第一端。 板元件和多个喷嘴元件形成为整体部件。 板构件与喷嘴部件接合。 板构件包括限定第一和第二表面的外边缘和在第一和第二表面之间延伸的多个开口。 多个开口被配置和设置成与多个喷嘴元件中对应的喷嘴元件的对应的第二端对准并接收。
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