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    Boiler and low-NOx combustion method
    41.
    发明授权
    Boiler and low-NOx combustion method 有权
    锅炉和低NOx燃烧法

    公开(公告)号：US07647898B2

    公开(公告)日：2010-01-19

    申请号：US11349932

    申请日：2006-02-09

    Applicant: Yuji Yoshinari ,  Osamu Tanaka ,  Yukihiro Tokunaga

    Inventor： Yuji Yoshinari ,  Osamu Tanaka ,  Yukihiro Tokunaga

    IPC: F23C5/00

    CPC classification number: F23C6/047 ,  F23C2201/401 ,  F23D14/02 ,  F24H1/40 ,  F24H1/403

    Abstract: To provide a boiler capable of realizing a reduction in O2, a reduction in NOx, and a reduction in CO. The present invention provides a boiler including: a premixed gas burner, and water tubes in close proximity to the premixed gas burner, characterized in that the premixed gas burner ejects a premixed gas toward the water tubes at a predetermined angle; and the boiler further includes a fuel supply portion capable of supplying at least one of a gas fuel and a premixed gas provided at a position on a downstream side of and spaced apart by a predetermined distance from the premixed gas burner.

    Abstract translation: 本发明提供一种锅炉，包括：预混合气体燃烧器和靠近预混气体燃烧器的水管，其特征在于， 预混燃气燃烧器以预定的角度向水管喷射预混气体; 并且所述锅炉还包括能够供给气体燃料和设置在与所述预混气体燃烧器的下游侧并与所述预混气体燃烧器隔开预定距离的位置处的预混合气中的至少一种的燃料供给部。

    Fuel nozzle assembly for reduced exhaust emissions
    45.
    发明公开
    Fuel nozzle assembly for reduced exhaust emissions 有权
    燃油喷嘴组件可减少废气排放

    公开(公告)号：EP1186832A3

    公开(公告)日：2002-04-24

    申请号：EP01307493.5

    申请日：2001-09-04

    Applicant: GENERAL ELECTRIC COMPANY

    Inventor： Hura, Harjit Singh ,  Cooper, James Neil ,  Mongia, Hukam Chand ,  Sabla, Paul Edward ,  Duncan, Beverly Stephenson ,  Lohmueller, Steven Joseph

    IPC: F23R3/34

    CPC classification number: F23R3/346 ,  F23C2201/20 ,  F23C2201/401

    Abstract: A two-stage fuel nozzle assembly (56) for a gas turbine engine. The primary combustion region (120) is centrally positioned and includes a fuel injector (122) that is surrounded by one or more swirl chambers (132, 160) to provide a fuel air mixture that is ignited to define a first stage combustion zone. A secondary combustion region is provided by an annular housing (168) that surrounds the primary combustion region (120) and it includes a secondary fuel injector (126) having a radially-outwardly-directed opening (172) and surrounded by an annular ring (128) that includes openings (194) for providing a swirl chamber for the secondary combustion region (124). Cooling air is directed angularly between the primary and secondary combustion zones to delay intermixing and thereby allow more complete combustion of the respective zones prior to their coalescing further downstream. The primary combustion region (120) is activated during idle and low engine power conditions, and both the primary (120) and secondary (124) combustion regions are activated during high engine power conditions.

    Abstract translation: 一种用于燃气涡轮发动机的两级燃料喷嘴组件（56）。 主燃烧区域（120）位于中央，并且包括被一个或多个涡流室（132,160）包围的燃料喷射器（122），以提供被点燃以限定第一阶段燃烧区域的燃料空气混合物。 二次燃烧区域由围绕主燃烧区域（120）的环形壳体（168）提供，并且其包括具有径向向外指向的开口（172）并且被环形圈（120）包围的次级燃料喷射器（126） 128），其包括用于为所述第二燃烧区域（124）提供涡流室的开口（194）。 冷却空气在初级燃烧区和次级燃烧区之间有角度地引导，以延迟混合，从而允许相应区在更下游的聚结之前更完全地燃烧。 在怠速和低发动机功率状态期间主燃烧区域（120）被激活，并且在高发动机功率状态期间主燃烧区域（120）和次燃烧区域（124）都被激活。

    LOW NOX INDIRECT FIRE BURNER
    46.
    发明申请
    LOW NOX INDIRECT FIRE BURNER 审中-公开
    低NOx间接燃烧器

    公开(公告)号：WO2011041279A3

    公开(公告)日：2011-09-29

    申请号：PCT/US2010050471

    申请日：2010-09-28

    Applicant: HONEYWELL INT INC ,  MOSIEWICZ PAWEL

    Inventor： MOSIEWICZ PAWEL

    IPC: F23D14/04 ,  F23D14/46 ,  F23D14/58

    CPC classification number: F23C6/047 ,  F23C5/08 ,  F23C2201/401 ,  F23C2900/03005 ,  F23D14/105 ,  F23D2203/1012 ,  F24H1/282

    Abstract: An air-fuel burner includes a heat-transfer tube, an air-fuel mixing chamber, and an air-fuel nozzle. The air-fuel nozzle is coupled to the air-fuel chamber to communicate a combustible air-fuel mixture into a combustion chamber defined between the air-fuel nozzle and the heat-transfer tube. The combustible air-fuel mixture, when ignited, establishes a flame in the combustion chamber to produce heat which is transferred through heat-transfer tube to an adjacent medium external to the heat-transfer tube.

    Abstract translation: 空气燃料燃烧器包括传热管，空气燃料混合室和空气燃料喷嘴。 空气燃料喷嘴连接到空气燃料室以将可燃性空气燃料混合物连通到限定在空气燃料喷嘴和传热管之间的燃烧室中。 可燃混合气在点燃时在燃烧室内形成火焰，产生热量，热量通过传热管传递到传热管外部的相邻介质。

    STAGED SUPPLEMENTAL FIRING OF HIGH VANADIUM CONTENT FUEL OILS
    48.
    发明申请
    STAGED SUPPLEMENTAL FIRING OF HIGH VANADIUM CONTENT FUEL OILS 审中-公开
    高分子量燃料油的分批补充燃烧

    公开(公告)号：WO98039599A1

    公开(公告)日：1998-09-11

    申请号：PCT/US1998/004115

    申请日：1998-03-03

    IPC: F22B1/18 ,  F23C6/04

    CPC classification number: F22B1/1815 ,  F22B1/1861 ,  F23C6/04 ,  F23C2201/30 ,  F23C2201/401

    Abstract: A heat exchanger for burning fuel oil having vanadium and for preventing melting of vanadium complexes formed from burning fuel oil includes a first (28) and a second (30) stage. Contained within each stage is a duct burner (18) that heats gas flowing through the heat exchanger by burning fuel having vanadium and a cooling component that cools gas heated by the duct burner. Within each stage the temperature of the gas is maintained about below the melting point of vanadium complexes. Consequently, the vanadium complexes do not achieve their corrosive molten state. This invention also includes a method for burning fuel oil containing vanadium and preventing the melting of vanadium complexes by heating and cooling the gas in a plurality of stages.

    Abstract translation: 用于燃烧具有钒并且用于防止燃烧燃料油形成的钒络合物熔化的燃料油的热交换器包括第一（28）和第二（30）阶段。 在每个阶段中包括管道燃烧器（18），其通过燃烧具有钒的燃料和冷却由管道燃烧器加热的气体的冷却组件来加热流过热交换器的气体。 在每个阶段，气体的温度维持在低于钒络合物的熔点。 因此，钒配合物不能达到其腐蚀性的熔融状态。 本发明还包括一种用于燃烧含钒的燃料油并通过多级加热和冷却气体来防止钒配合物熔化的方法。

    Combustor for a gas turbine engine
    50.
    发明公开
    Combustor for a gas turbine engine 有权
    燃烧器用于燃气涡轮植物

    公开(公告)号：EP2169303A3

    公开(公告)日：2014-12-24

    申请号：EP09170923.8

    申请日：2009-09-22

    Applicant: ALSTOM Technology Ltd

    Inventor： Poyyapakkam, Madhavan Narasimhan

    IPC: F23C6/04 ,  F23R3/00 ,  F23M9/10 ,  F23R3/34

    CPC classification number: F23C6/04 ,  F23C2201/401 ,  F23C2900/06041 ,  F23C2900/07002 ,  F23M9/10 ,  F23R3/00 ,  F23R3/346 ,  F23R2900/03041 ,  F23R2900/03341

    Abstract: The invention relates to a combustor (1) for a gas turbine engine, particularly for a gas turbine having sequential combustion. The combustor (1) comprises a combustor wall (4) defining a mixing region (5) and a combustion region (6). The mixing region (5) comprises at least one first inlet (2) for introducing combustion air into the mixing region (5) and at least one second inlet for introducing fuel into the mixing region (5), the combustion region (6) extending downstream of the mixing region. The mixing region (5) crossing over to the combustion region (6) in a transition region (14).
    A baffle (9) extends from the transition region (14) generally in the downstream direction (15) forming at least one space (10) between the combustor wall (4) and the baffle (9).

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