Fuel Insert
    3.
    发明申请
    Fuel Insert 审中-公开
    燃油插入

    公开(公告)号:US20110136067A1

    公开(公告)日:2011-06-09

    申请号:US13058429

    申请日:2009-05-14

    Applicant: Thomas Grieb

    Inventor: Thomas Grieb

    CPC classification number: F23D11/383

    Abstract: A fuel nozzle for imparting swirl to a fuel/fuel-air mixture is provided. The fuel nozzle includes a holding unit and a nozzle insert, wherein the holding unit and the nozzle insert form a flow path and subsequently a swirl chamber, wherein the nozzle insert includes an inlet start and an inlet end. The inlet start and the inlet end are bent in a substantially circular manner such that an unbroken circle is formed, such that a fuel flowing into the swirl chamber has imparted to it a radially inwardly directed circular, in particular spiral movement. A burner and a gas turbine are also provided.

    Abstract translation: 提供了用于向燃料/燃料 - 空气混合物施加涡流的燃料喷嘴。 燃料喷嘴包括保持单元和喷嘴插件,其中保持单元和喷嘴插件形成流动路径,随后形成涡流室,其中喷嘴插件包括入口开口和入口端。 入口开始和入口端以基本圆形的方式弯曲,使得形成不间断的圆,使得流入涡流室的燃料赋予它径向向内的圆形,特别是螺旋运动。 还提供燃烧器和燃气轮机。

    Burner arrangement
    7.
    发明授权
    Burner arrangement 有权
    燃烧器安排

    公开(公告)号:US08955328B2

    公开(公告)日:2015-02-17

    申请号:US13029246

    申请日:2011-02-17

    CPC classification number: F23R3/283 F23C2900/07021 F23D23/00 F23R2900/00018

    Abstract: A burner arrangement is provided. The burner arrangement includes a support and at least two fuel nozzles attached to the support in the direction of flow, with each fuel nozzle including a support-side section which includes a contact surface on the support side with which it rests on a supporting surface of the support, with at least two fuel nozzle tips embodied in one piece extending out from the support-side section in the direction of flow and the support-side contact surface including at least two extension parts projecting in the direction of the support, with the extension parts each embodying a channel through which fuel is fed in each case to the fuel nozzle tips through passages which are arranged in the support-side contact surface of the support-side section.

    Abstract translation: 提供燃烧器装置。 燃烧器装置包括支撑件和沿流动方向附接到支撑件的至少两个燃料喷嘴,每个燃料喷嘴包括支撑侧部分,该支撑侧部分包括在支撑侧上的接触表面,支撑侧支撑在支撑面的支撑表面上 所述支撑件具有至少两个燃料喷嘴尖端,所述至少两个燃料喷嘴尖端沿着流动方向从所述支撑侧部分延伸出一体,并且所述支撑侧接触表面包括至少两个在所述支撑件的方向上突出的延伸部分, 延伸部分各自包括通道,通过该通道将燃料在每种情况下通过布置在支撑侧部分的支撑侧接触表面中的通道供应到燃料喷嘴尖端。

    BURNER ASSEMBLY
    8.
    发明申请
    BURNER ASSEMBLY 审中-公开
    燃烧器总成

    公开(公告)号:US20130104554A1

    公开(公告)日:2013-05-02

    申请号:US13806895

    申请日:2011-07-01

    CPC classification number: F23R3/343 F23C2900/07021 F23D11/38 F23R3/286

    Abstract: A burner assembly for a gas turbine is provided. The burner assembly has a combustor, a centrally arranged pilot burner and plurality of main burners surrounding the pilot burner. Each main burner has a cylindrical housing having a lance which is centrally arranged therein and has a fuel channel for liquid fuel. The lance is supported on the housing by swirl blades and an attachment is arranged on the lance in the direction of the combustor. The liquid fuel nozzle is arranged in the attachment downstream of the swirl blades and connected to the fuel channel. For the improved mixing of the fuel with the air, the liquid fuel nozzle is designed as a full jet nozzle and the full jet nozzle has a length and a diameter, the ratio of the length to the diameter is at least 1.5.

    Abstract translation: 提供了一种用于燃气轮机的燃烧器组件。 燃烧器组件具有燃烧器,中心布置的引燃燃烧器和围绕引燃燃烧器的多个主燃烧器。 每个主燃烧器具有圆柱形壳体,其具有中心地布置在其中的喷枪,并具有用于液体燃料的燃料通道。 喷枪通过旋流叶片支撑在壳体上,并且喷枪沿燃烧器的方向设置附件。 液体燃料喷嘴布置在涡旋叶片下游的附件中并且连接到燃料通道。 为了改善燃料与空气的混合,液体燃料喷嘴设计为全喷嘴,全喷嘴具有长度和直径,长度与直径之比至少为1.5。

    BURNER ARRANGEMENT
    10.
    发明申请
    BURNER ARRANGEMENT 有权
    燃烧器装置

    公开(公告)号:US20110203285A1

    公开(公告)日:2011-08-25

    申请号:US13029246

    申请日:2011-02-17

    CPC classification number: F23R3/283 F23C2900/07021 F23D23/00 F23R2900/00018

    Abstract: A burner arrangement is provided. The burner arrangement includes a support and at least two fuel nozzles attached to the support in the direction of flow, with each fuel nozzle including a support-side section which includes a contact surface on the support side with which it rests on a supporting surface of the support, with at least two fuel nozzle tips embodied in one piece extending out from the support-side section in the direction of flow and the support-side contact surface including at least two extension parts projecting in the direction of the support, with the extension parts each embodying a channel through which fuel is fed in each case to the fuel nozzle tips through passages which are arranged in the support-side contact surface of the support-side section.

    Abstract translation: 提供燃烧器装置。 燃烧器装置包括支撑件和沿流动方向附接到支撑件的至少两个燃料喷嘴,每个燃料喷嘴包括支撑侧部分,该支撑侧部分包括在支撑侧上的接触表面,支撑侧支撑在支撑面的支撑表面上 所述支撑件具有至少两个燃料喷嘴尖端,所述至少两个燃料喷嘴尖端沿着流动方向从所述支撑侧部分延伸出一体,并且所述支撑侧接触表面包括至少两个在所述支撑件的方向上突出的延伸部分, 延伸部分各自包括通道,通过该通道将燃料在每种情况下通过布置在支撑侧部分的支撑侧接触表面中的通道供应到燃料喷嘴尖端。

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