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397 条记录 (耗时 0.019 秒)

    FUEL NOZZLE
    92.
    发明申请
    FUEL NOZZLE 审中-公开
    燃油喷嘴

    公开(公告)号：US20160097537A1

    公开(公告)日：2016-04-07

    申请号：US14505778

    申请日：2014-10-03

    申请人： PRATT & WHITNEY CANADA CORP.

    发明人： Yen-Wen WANG ,  Nigel Davenport ,  Eduardo Hawie

    IPC分类号： F23R3/28

    CPC分类号： F23R3/286 ,  F23D14/20 ,  F23D2206/10 ,  F23D2900/11101 ,  F23R3/04 ,  F23R3/10 ,  F23R3/12 ,  F23R3/30

    摘要： A fuel nozzle for a combustor of a gas turbine engine includes a body defining an axial direction and a radial direction, an air passageway defined axially in the body, and a fuel passageway defined axially in the body radially outwardly from the air passageway. The fuel passageway has an outer wall including an exit lip at a downstream portion of the outer wall. The lip generally increases in diameter as it extends downstream.

    摘要翻译： 用于燃气涡轮发动机的燃烧器的燃料喷嘴包括限定轴向方向和径向方向的主体，在主体中轴向限定的空气通道，以及从该空气通道径向向外在该体内轴向限定的燃料通道。 燃料通道具有在外壁的下游部分包括出口的外壁。 嘴唇通常在下游延伸时直径增加。

    ATOMIZING FUEL NOZZLE
    93.
    发明申请
    ATOMIZING FUEL NOZZLE 审中-公开
    引燃燃油喷嘴

    公开(公告)号：US20160047315A1

    公开(公告)日：2016-02-18

    申请号：US14458533

    申请日：2014-08-13

    申请人： PRATT & WHITNEY CANADA CORP.

    发明人： Kian McCaldon ,  Oleg Morenko

    IPC分类号： F02C7/22

    CPC分类号： F02C7/22 ,  F23D2900/11101 ,  F23R3/12 ,  F23R3/28

    摘要： A fuel nozzle for a gas turbine engine. The nozzle has a body and a center axis. The body has an inner circumferential surface circumscribing a central passageway which is coaxial with the center axis. The nozzle also has air passages which extend predominantly radially inward through the body. The air passage outlets of each air passage are circumferentially spaced apart from one another along the inner circumferential surface. Each air passage conveys air through the body toward the nozzle center axis and into the central passageway. The nozzle also has fuel passages which extend through the body. Each fuel passage is disposed within the body between adjacent circumferentially spaced apart air passages and is transverse to the direction of extension of its neighboring air passages.

    摘要翻译： 一种用于燃气涡轮发动机的燃料喷嘴。 喷嘴具有主体和中心轴线。 主体具有围绕与中心轴线同轴的中心通道的内圆周表面。 喷嘴还具有主要径向向内延伸通过主体的空气通道。 每个空气通道的空气通道出口沿着内圆周表面沿周向间隔开。 每个空气通道将空气通过主体朝向喷嘴中心轴线传送到中心通道中。 喷嘴还具有延伸穿过主体的燃料通道。 每个燃料通道在相邻的周向间隔开的空气通道之间设置在主体内，并且横向于其相邻空气通道的延伸方向。

    INJECTORS FOR MULTIPOINT INJECTION
    94.
    发明申请
    INJECTORS FOR MULTIPOINT INJECTION 审中-公开
    注射器多点注射

    公开(公告)号：US20150361896A1

    公开(公告)日：2015-12-17

    申请号：US14835654

    申请日：2015-08-25

    申请人： Delavan Inc

    发明人： Lev Alexander Prociw ,  Jason Ryon

    IPC分类号： F02C7/22

    CPC分类号： F23R3/14 ,  F02C7/22 ,  F23D11/107 ,  F23D2900/11101 ,  F23R3/10 ,  F23R3/12 ,  F23R3/28 ,  F23R3/286 ,  F23R3/30

    摘要： An injector for a multipoint combustor system includes an inner air swirler which defines an interior flow passage and a plurality of swirler inlet ports in an upstream portion thereof. The inlet ports are configured and adapted to impart swirl on flow in the interior flow passage. An outer air cap is mounted outboard of the inner swirler. A fuel passage is defined between the inner air swirler and the outer air cap, and includes a discharge outlet between downstream portions of the inner air swirler and the outer air cap for issuing fuel for combustion. The outer air cap defines an outer air circuit configured for substantially unswirled injection of compressor discharge air outboard of the interior flow passage.

    摘要翻译： 用于多点燃烧器系统的喷射器包括内部空气旋流器，其在其上游部分中限定内部流动通道和多个旋流器入口。 入口端口被配置和适于在内部流动通道中产生流动的漩涡。 外部空气盖安装在内旋流器的外侧。 在内部空气旋流器和外部空气帽之间限定有燃料通道，并且在内部空气旋流器的下游部分和用于燃烧燃料的外部空气帽之间包括排出口。 外部空气帽限定了外部空气回路，该外部空气回路经配置以基本上不加注入内部流动通道外侧的压缩机排放空气。

    Swirler for mixing fuel and air
    95.
    发明授权
    Swirler for mixing fuel and air 有权
    旋流器用于混合燃料和空气

    公开(公告)号：US09188339B2

    公开(公告)日：2015-11-17

    申请号：US13057190

    申请日：2009-06-24

    申请人： Paul Headland

    发明人： Paul Headland

    IPC分类号： F23R3/14 ,  F23R3/12 ,  F23C7/00 ,  F23R3/28

    CPC分类号： F23R3/14 ,  F23C7/004 ,  F23C2900/07001 ,  F23R3/12 ,  F23R3/286

    摘要： A swirler for mixing fuel and air is provided. The swirler includes a plurality of vanes arranged on a reference circle diameter which, together with a first longitudinal end face of the vanes disposed on a first wall and a second wall disposed on an opposing second longitudinal end face of the vanes, form a flow channel. In this arrangement at least one injection orifice in the first wall and at least one further injection orifice in the second wall open into a flow channel. The arrangement of the at least two mutually opposing injection orifices in the wall of the swirler makes for a homogeneous distribution of the fuel in the flow channel and ensures a uniform mixing of the air with the fuel. This results in uniform and low-NOx combustion of the fuel/air mixture in a burner.

    摘要翻译： 提供了用于混合燃料和空气的旋流器。 旋流器包括布置在参考圆直径上的多个叶片，其与设置在第一壁上的叶片的第一纵向端面和设置在叶片的相对的第二纵向端面上的第二壁一起形成流动通道 。 在该布置中，第一壁中的至少一个喷射孔和第二壁中的至少一个另外的喷射孔开放到流动通道中。 在旋流器的壁中的至少两个相互相对的喷射孔的布置使得燃料在流动通道中均匀分布，并确保空气与燃料的均匀混合。 这导致燃烧器中燃料/空气混合物的均匀和低NOx燃烧。

    Injectors for multipoint injection
    96.
    发明授权
    Injectors for multipoint injection 有权
    注射器用于多点注射

    公开(公告)号：US09188063B2

    公开(公告)日：2015-11-17

    申请号：US13665497

    申请日：2012-10-31

    申请人： DELAVAN INC

    发明人： Lev Alexander Prociw ,  Jason Ryon

    IPC分类号： F23R3/14 ,  F23R3/28 ,  F23R3/30 ,  F02C7/22 ,  F23D11/10

    CPC分类号： F23R3/14 ,  F02C7/22 ,  F23D11/107 ,  F23D2900/11101 ,  F23R3/10 ,  F23R3/12 ,  F23R3/28 ,  F23R3/286 ,  F23R3/30

    摘要： An injector for a multipoint combustor system includes an inner air swirler which defines an interior flow passage and a plurality of swirler inlet ports in an upstream portion thereof. The inlet ports are configured and adapted to impart swirl on flow in the interior flow passage. An outer air cap is mounted outboard of the inner swirler. A fuel passage is defined between the inner air swirler and the outer air cap, and includes a discharge outlet between downstream portions of the inner air swirler and the outer air cap for issuing fuel for combustion. The outer air cap defines an outer air circuit configured for substantially unswirled injection of compressor discharge air outboard of the interior flow passage.

    摘要翻译： 用于多点燃烧器系统的喷射器包括内部空气旋流器，其在其上游部分中限定内部流动通道和多个旋流器入口。 入口端口被配置和适于在内部流动通道中产生流动的漩涡。 外部空气盖安装在内旋流器的外侧。 在内部空气旋流器和外部空气帽之间限定有燃料通道，并且在内部空气旋流器的下游部分和用于燃烧燃料的外部空气帽之间包括排出口。 外部空气帽限定了外部空气回路，该外部空气回路经配置以基本上不加注入内部流动通道外侧的压缩机排放空气。

    Combustor and Method of Fuel Supply and Converting Fuel Nozzle for Advanced Humid Air Turbine
    99.
    发明申请
    Combustor and Method of Fuel Supply and Converting Fuel Nozzle for Advanced Humid Air Turbine 审中-公开
    用于先进湿度空气涡轮机的燃料供应和燃料喷嘴转换的燃烧器和方法

    公开(公告)号：US20150075174A1

    公开(公告)日：2015-03-19

    申请号：US14549809

    申请日：2014-11-21

    申请人： Mitsubishi Hitachi Power Systems, Ltd.

    发明人： Kazuki ABE ,  Tomomi KOGANEZAWA

    IPC分类号： F02C9/28 ,  F02C7/22

    CPC分类号： F02C9/28 ,  F02C6/18 ,  F02C7/22 ,  F23L7/005 ,  F23R3/12 ,  F23R3/28 ,  F23R3/346

    摘要： A fuel control device and method of a gas turbine combustor, for advanced humid air turbines, in which plural combustion units comprising plural fuel nozzles for supplying fuel and plural air nozzles for supplying air for combustion are provided. A part of the plural combustion units are more excellent in flame stabilizing performance than the other combustion units. A fuel ratio, at which fuel is fed to the part of the combustion units is set on the basis of internal temperature of the humidification tower and internal pressure of the humidification tower to control a flow ratio of the fuel fed to the plural combustion units.

    摘要翻译： 提供一种用于先进湿式空气涡轮机的燃气轮机燃烧器的燃料控制装置和方法，其中包括用于供应燃料的多个燃料喷嘴和用于供给燃烧空气的多个空气喷嘴的多个燃烧单元。 多个燃烧单元的一部分在火焰稳定性方面优于其它燃烧单元。 基于加湿塔的内部温度和加湿塔的内部压力来设定向燃烧单元的一部分供给燃料的燃料比，以控制供给到多个燃烧单元的燃料的流量比。