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    COMBUSTOR FOR GAS TURBINE ENGINE
    3.
    发明申请
    COMBUSTOR FOR GAS TURBINE ENGINE 审中-公开

    公开(公告)号：US20170082291A1

    公开(公告)日：2017-03-23

    申请号：US15363414

    申请日：2016-11-29

    Applicant: KAWASAKI JUKOGYO KABUSHIKI KAISHA ,  B&B AGEMA GmbH

    Inventor： Atsushi HORIKAWA ,  Masahide KAZARI ,  Kunio OKADA ,  Junichi KITAJIMA ,  Harald FUNKE ,  Karsten KUSTERER ,  Anis Haj AYED

    IPC: F23R3/28 ,  F02C7/22 ,  F23R3/16 ,  F23R3/00 ,  F23R3/10

    Abstract: A combustor includes: a combustion liner having a combustion chamber formed therein; and a fuel injector mounted to a top portion of the combustion liner, and including a fuel injection member having a plurality of fuel injection annular portions and an air guide member including a plurality of combustion air annular portions that guide air for combustion. The fuel injection annular portions and the combustion air annular portions are arranged concentrically and alternately. The fuel injector injects fuel and air into the combustion chamber. Each of the fuel injection annular portions includes a plurality of fuel injection holes that are open in a radial direction thereof, and each of the combustion air annular portions includes a plurality of air guide grooves that are open in an axial direction thereof, and guide the air to the fuel jetted from the fuel injection holes.

    DOUBLE-JET FILM COOLING STRUCTURE AND METHOD FOR MANUFACTURING SAME
    5.
    发明申请
    DOUBLE-JET FILM COOLING STRUCTURE AND METHOD FOR MANUFACTURING SAME 有权
    双盖冷却结构及其制造方法

    公开(公告)号：US20160069192A1

    公开(公告)日：2016-03-10

    申请号：US14944503

    申请日：2015-11-18

    Applicant: KAWASAKI JUKOGYO KABUSHIKI KAISHA ,  B&B AGEMA GmbH

    Inventor： Ryozo TANAKA ,  Takao SUGIMOTO ,  Masahide KAZARI ,  Tomoki TANIGUCHI ,  Karsten KUSTERER ,  Dieter BOHN ,  Nurettin TEKIN

    IPC: F01D5/18 ,  B23H1/04

    CPC classification number: F01D5/186 ,  B23H1/04 ,  B23H9/10 ,  B23H9/14 ,  F01D9/065 ,  F05D2230/12 ,  F05D2240/11 ,  F05D2240/81 ,  F05D2250/14 ,  F05D2250/231 ,  F05D2250/75 ,  F05D2260/202 ,  F23R3/06 ,  F23R2900/03042

    Abstract: A double-jet film cooling structure includes: an injection port, formed on a wall surface facing a high-temperature gas passage; a main passage as a straight round hole to supply cooling medium to the injection port; a pair of branch passages as straight round holes; and communication passages connecting the main passage to the branch passages. The main passage and the branch passages have same constant inner diameters. Each communication passages has an envelope surface obtained by continuously arranging straight round holes each passing a branch point and having the constant inner diameter. Transverse injection angles of the branch passages relative to gas flow along the wall surface are oriented in opposite directions. An angle between axial direction of the main passage and the wall surface is greater than an angle formed between axial direction of branch passage and the wall surface.

    Abstract translation: 双喷射薄膜冷却结构包括：形成在面向高温气体通道的壁面上的喷射口; 主通道作为直的圆孔向冷却介质供给喷射口; 一对分支通道为直圆孔; 以及将主通道连接到分支通道的连通通道。 主通道和分支通道具有相同的恒定内径。 每个连通通道具有通过连续地布置通过分支点并具有恒定内径的直圆孔而获得的包络面。 分支通道相对于沿着壁表面的气流的横向喷射角度被定向在相反的方向。 主通道的轴向与壁面之间的角度大于在分支通道的轴向方向和壁面之间形成的角度。

    SUNLIGHT-UTILIZING GAS TURBINE POWER GENERATION SYSTEM PROVIDED WITH HYDROGEN-GENERATING UNIT
    8.
    发明申请
    SUNLIGHT-UTILIZING GAS TURBINE POWER GENERATION SYSTEM PROVIDED WITH HYDROGEN-GENERATING UNIT 审中-公开
    用氢气发电机组提供的天然气涡轮发电系统

    公开(公告)号：US20150226119A1

    公开(公告)日：2015-08-13

    申请号：US14695192

    申请日：2015-04-24

    Applicant: KAWASAKI JUKOGYO KABUSHIKI KAISHA ,  B&B AGEMA GmbH

    Inventor： Kazuhiko TANIMURA ,  Takao SUGIMOTO ,  Karsten KUSTERER

    IPC: F02C3/22 ,  F02C6/00 ,  F02C7/32 ,  F02C7/22 ,  F24J2/42 ,  F02C6/10 ,  F02C3/04 ,  F02C7/08

    CPC classification number: F02C3/22 ,  F02C1/05 ,  F02C3/04 ,  F02C6/00 ,  F02C6/10 ,  F02C6/18 ,  F02C7/08 ,  F02C7/22 ,  F02C7/32 ,  F03G6/04 ,  F05D2220/32 ,  F05D2220/60 ,  F05D2260/20 ,  F24S90/00 ,  Y02E10/46

    Abstract: A power generation system having a gas turbine engine that utilizes sunlight, includes a compressor configured to compress an air which is a working medium, a solar heater configured to heat the air compressed by the compressor, utilizing sunlight as a heat source, a hydrogen combustor configured to burn the air compressed by the compressor utilizing hydrogen as a fuel, a turbine configured to output a motive power from a high-temperature gas heated by at least one of the solar heater and the hydrogen combustor, a power generator configured to be driven by the turbine, and at least one hydrogen-generating unit configured to generate hydrogen by utilizing an output of the turbine or exhaust heat from the turbine to decompose a water, and supply the hydrogen so generated to the hydrogen combustor.

    Abstract translation: 具有利用太阳光的燃气涡轮发动机的发电系统包括压缩构造成压缩作为工作介质的空气的压缩机，被配置为加热由压缩机压缩的空气的太阳能加热器，利用太阳光作为热源，氢燃烧器 被配置为燃烧利用氢气作为燃料而被压缩机压缩的空气，所述涡轮机构造成从由所述太阳能加热器和所述氢燃烧器中的至少一个加热的高温气体输出动力;被配置为被驱动的发电机 以及至少一个氢气发生单元，其被配置为通过利用涡轮机的输出或者来自涡轮机的排气来产生氢，以分解水，并且将如此产生的氢气供应给氢燃烧器。

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