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    DAMPER ARRANGEMENT FOR REDUCING COMBUSTION-CHAMBER PULSATION
    1.
    发明申请
    DAMPER ARRANGEMENT FOR REDUCING COMBUSTION-CHAMBER PULSATION 审中-公开
    用于减少燃烧室冲击的阻尼器装置

    公开(公告)号：US20140109591A1

    公开(公告)日：2014-04-24

    申请号：US14061954

    申请日：2013-10-24

    Applicant: ALSTOM TECHNOLOGY LTD.

    Inventor： Mirko Ruben BOTHIEN ,  Jaan HELLAT ,  Bruno SCHUERMANS

    IPC: F23M99/00 ,  F02C6/02

    Abstract: The invention concerns a damper arrangement for reducing combustion-chamber pulsation arising inside a gas turbine, wherein the gas turbine includes at least one compressor, a primary combustor which is connected downstream to the compressor, and the hot gases of the primary combustor are admitted at least to an intermediate turbine or directly or indirectly to a secondary combustor. The hot gases of the secondary combustor are admitted to a further turbine or directly or indirectly to an energy recovery, wherein at least one combustor is arranged in a can-architecture. At least one combustor liner includes air passages, wherein at least one of the air passages is formed as a damper neck. The damper neck being actively connected to a damper volume, and the damper volume is part of a connecting duct extending between a compressor air plenum and the combustor.

    Abstract translation: 本发明涉及一种用于减少在燃气轮机内部产生的燃烧室脉动的阻尼装置，其中燃气轮机包括至少一个压缩机，连接在压缩机下游的主燃烧器和主燃烧室的热气体 至少到中间涡轮机，或直接或间接地连接到二级燃烧器。 次级燃烧器的热气体被允许进一步涡轮机，或直接地或间接地进入能量回收，其中至少一个燃烧器以罐式结构设置。 至少一个燃烧器衬套包括空气通道，其中至少一个空气通道形成为阻尼颈部。 阻尼器颈部主动地连接到阻尼器体积，并且阻尼器体积是在压缩机空气室和燃烧器之间延伸的连接管道的一部分。

    METHOD OF OPERATING A GAS TURBINE POWER PLANT WITH EXHAUST GAS RECIRCULATION AND CORRESPONDING GAS TURBINE POWER PLANT
    3.
    发明申请
    METHOD OF OPERATING A GAS TURBINE POWER PLANT WITH EXHAUST GAS RECIRCULATION AND CORRESPONDING GAS TURBINE POWER PLANT 有权
    具有排气再循环和相应气体涡轮发电厂的气体涡轮发电厂的运行方法

    公开(公告)号：US20140360199A1

    公开(公告)日：2014-12-11

    申请号：US14467500

    申请日：2014-08-25

    Applicant: ALSTOM Technology Ltd

    Inventor： Jaan HELLAT ,  Eribert Benz ,  Frank Graf ,  Torsten Wind ,  Felix Guethe ,  Klaus Doebbeling

    IPC: F02C3/30 ,  F02C3/06

    CPC classification number: F02C3/30 ,  F01D5/141 ,  F02C3/06 ,  F02C3/34 ,  F02C6/003 ,  F02C6/08 ,  F02C6/18 ,  F02C7/04

    Abstract: The invention relates to a method for operating a gas turbine, in which an oxygen-reduced gas and fresh air are delivered to a compressor of the gas turbine in a radially staged manner, the fresh air being delivered via an outer sector of the inlet cross section in relation to the axis of rotation of the compressor, and the oxygen-reduced gas being delivered via an inner sector of the inlet cross section in relation to the axis of rotation of the compressor.The invention relates, further, to a gas turbine power plant with a gas turbine having a compressor inlet which is followed by the flow duct of the compressor and which is divided into an inner sector and an outer sector, a feed for an oxygen-reduced gas being connected to the inner sector of the compressor inlet, and a fresh air feed being connected to the outer sector of the compressor inlet.

    Abstract translation: 本发明涉及一种用于操作燃气轮机的方法，其中将氧气还原气体和新鲜空气以径向分级的方式输送到燃气轮机的压缩机，新鲜空气经由入口十字架的外部扇区输送 相对于压缩机的旋转轴线的截面，相对于压缩机的旋转轴线，通过入口横截面的内部扇区输送的氧还原气体。 本发明还涉及具有燃气轮机的燃气轮机发电厂，该燃气轮机具有压缩机入口，其后面是压缩机的流动管道，并且分为内部扇区和外部扇区，用于氧气还原 气体连接到压缩机入口的内部扇区，新鲜空气进料连接到压缩机入口的外部扇区。

    SEQUENTIAL COMBUSTION WITH DILUTION GAS MIXER
    4.
    发明申请
    SEQUENTIAL COMBUSTION WITH DILUTION GAS MIXER 审中-公开
    与稀释气体混合器连续燃烧

    公开(公告)号：US20150226122A1

    公开(公告)日：2015-08-13

    申请号：US14693045

    申请日：2015-04-22

    Applicant: ALSTOM Technology Ltd

    Inventor： Michael DUESING ,  Luis TAY WO CHONG HILARES ,  Mirko Ruben BOTHIEN ,  Jaan HELLAT ,  Bruno SCHUERMANS

    IPC: F02C7/141 ,  F02C3/04 ,  F23R3/42

    CPC classification number: F23R3/06 ,  F02C6/02 ,  F05D2220/32 ,  F05D2240/35 ,  F05D2260/964 ,  F23M20/005 ,  F23R3/002 ,  F23R2900/00014 ,  F23R2900/03341 ,  Y02E20/16

    Abstract: The invention refers to a sequential combustor arrangement including a first burner, a first combustion chamber, a mixer for admixing a dilution gas to the hot gases leaving the first combustion chamber during operation, a second burner, and a second combustion chamber arranged sequentially in a fluid flow connection. The mixer includes a plurality of injection pipes pointing inwards from the side walls of the mixer for admixing the dilution gas to cool the hot flue gases leaving the first combustion chamber with a low pressure drop. The disclosure further refers to a method for operating a gas turbine with such a combustor arrangement.

    Abstract translation: 本发明涉及一种连续的燃烧器装置，其包括第一燃烧器，第一燃烧室，混合器，用于将稀释气体混合到在运行期间离开第一燃烧室的热气体，第二燃烧器和第二燃烧室， 流体流动连接。 混合器包括从混合器的侧壁向内指向的多个注入管，用于混合稀释气体以以低压降将离开第一燃烧室的热烟道气冷却。 本发明还涉及一种用这种燃烧器装置操作燃气轮机的方法。

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