Modified gas turbine system with advanced pressurized fluidized bed
combustor cycle
    1.
    发明授权
    Modified gas turbine system with advanced pressurized fluidized bed combustor cycle 失效
    改进型燃气轮机系统采用先进的加压流化床燃烧器循环

    公开(公告)号:US6101983A

    公开(公告)日:2000-08-15

    申请号:US371169

    申请日:1999-08-11

    CPC classification number: F01K23/067 F01K23/062 F02C3/205 Y02E20/18

    Abstract: A modified gas turbine system is provided that adapts an advanced pressurized fluidized bed combustor cycle for use with existing combustion turbine technology. To accommodate current combustion turbine technology, the air extracted from the compressor discharge is limited, e.g. to about 20% of the total. The additional air required for the APFBC cycle is provided by an auxiliary source of compressed air. The compressor discharge air that is not extracted is used for combustion of the fuel gas produced by the carbonizer and also provides internal cooling as required by conventional combustion turbine design. A separate expander turbine is used to recover energy from the vitiated air from the PFBC. Energy from the vitiated air may further be recovered by directing the expander exhaust to an HRSG.

    Abstract translation: 提供了一种改进的燃气轮机系统,其适应先进的加压流化床燃烧器循环以与现有燃气轮机技术一起使用。 为了适应目前的燃气轮机技术,从压缩机排放物抽出的空气是有限的。 至约20%。 APFBC循环所需的额外空气由辅助压缩空气源提供。 未提取的压缩机排出空气用于由碳化器生产的燃料气体的燃烧,并且还根据常规燃气轮机设计的要求提供内部冷却。 单独的膨胀机涡轮机用于从PFBC中的空气中回收能量。 来自膨胀空气的能量可以通过将膨胀机排气引导至HRSG进一步回收。

    Integrated turbomachine plant
    2.
    发明授权
    Integrated turbomachine plant 有权
    综合涡轮机厂

    公开(公告)号:US08943838B2

    公开(公告)日:2015-02-03

    申请号:US13216939

    申请日:2011-08-24

    Abstract: An integrated turbomachine plant is provided and includes a combustor a turbomachine operably connected to the combustor and including a compressor and a turbine expander, a pathway to flow compressed air from the compressor through the turbine expander to heat the compressed air, an additional pathway by which high temperature fluids output from the turbomachine are employed to heat the compressed air and an air separation unit operably connected to the pathway and configured to separate the heated compressed air into oxygen and oxygen-depleted air.

    Abstract translation: 提供了一种集成的涡轮机械设备并且包括可操作地连接到燃烧器并且包括压缩机和涡轮膨胀器的涡轮机的燃烧器,用于将来自压缩机的压缩空气通过涡轮膨胀机流过以加压压缩空气的通路, 使用从涡轮机输出的高温流体用于加热压缩空气和空气分离单元,其可操作地连接到该通道并且构造成将加热的压缩空气分离成氧气和贫氧空气。

    METHOD OF USING EXTERNAL FLUID FOR COOLING HIGH TEMPERATURE COMPONENTS OF GAS TURBINE FOR A PROCESS POWER PLANT
    4.
    发明申请
    METHOD OF USING EXTERNAL FLUID FOR COOLING HIGH TEMPERATURE COMPONENTS OF GAS TURBINE FOR A PROCESS POWER PLANT 审中-公开
    使用外部流体冷却气体涡轮机用于过程发电厂的高温部件的方法

    公开(公告)号:US20130186101A1

    公开(公告)日:2013-07-25

    申请号:US13356677

    申请日:2012-01-24

    CPC classification number: F02C7/18 Y02E20/16 Y02E20/18

    Abstract: An external fluid in a closed loop is used to cool hot gas path components of gas turbine. After cooling the turbine components, the heated external fluid is dumped either in the compressor discharge casing or in the one of the turbine's stages. Where the external fluid is nitrogen to be dumped in the turbine compressor's discharge casing, the nitrogen is compressed using diluent nitrogen compressors. Alternatively, where the external fluid is nitrogen to be dumped in one of the stages of the turbine, the nitrogen is not compressed at all. The turbine blade heat exchangers in the turbine stages through which the nitrogen passes can be connected in parallel or in series for cooling the hot gas path components in the turbine stages. The nitrogen can optionally be mixed with air or steam or not mixed at all.

    Abstract translation: 闭环中的外部流体用于冷却燃气轮机的热气路径部件。 在冷却涡轮机部件之后,被加热的外部流体被倾倒在压缩机排放壳体或涡轮机的一个级中。 在外部流体是要倾倒在涡轮压缩机的排放套管中的氮气的情况下,使用稀释氮压缩机来压缩氮气。 或者,当外部流体是要被倾倒在涡轮机的一个级中的氮气时,氮气根本不被压缩。 氮气通过的涡轮级中的涡轮机叶片式热交换器可以并联或串联连接以冷却涡轮级中的热气体路径部件。 氮气可以任选地与空气或蒸汽混合或根本不混合。

    POWER PLANT
    5.
    发明申请
    POWER PLANT 有权
    发电厂

    公开(公告)号:US20130086882A1

    公开(公告)日:2013-04-11

    申请号:US13269356

    申请日:2011-10-07

    Abstract: A power plant is provided and includes a gas turbine engine having a combustor in which compressed gas and fuel are mixed and combusted, first and second supply lines respectively coupled to the combustor and respectively configured to supply the compressed gas and the fuel to the combustor and an exhaust gas recirculation (EGR) system to re-circulate exhaust gas produced by the gas turbine engine toward the combustor. The EGR system is coupled to the first and second supply lines and configured to combine first and second portions of the re-circulated exhaust gas with the compressed gas and the fuel at the first and second supply lines, respectively.

    Abstract translation: 提供一种动力装置,包括具有燃烧室的燃气轮机,燃气轮机将压缩气体和燃料混合燃烧,分别与燃烧器连接的第一和第二供给管路,分别构成为将压缩气体和燃料供给到燃烧器, 废气再循环(EGR)系统,用于将由燃气涡轮发动机产生的废气再循环到燃烧器。 EGR系统耦合到第一和第二供应管线并且被配置成将再循环废气的第一和第二部分分别与第一和第二供应管线处的压缩气体和燃料组合。

    Method and system for heat recovery from dirty gaseous fuel in gasification power plants
    7.
    发明授权
    Method and system for heat recovery from dirty gaseous fuel in gasification power plants 失效
    气化发电厂肮脏气体燃料热回收方法及系统

    公开(公告)号:US07665291B2

    公开(公告)日:2010-02-23

    申请号:US11396684

    申请日:2006-04-04

    CPC classification number: F02C3/22 F02C7/224 F05D2220/75 Y02E20/16 Y02E20/18

    Abstract: A system and method for recovering heat from dirty gaseous fuel (syngas), wherein the pressure of clean fuel gas is elevated to a pressure higher than that of the dirty syngas and then the pressurized clean fuel gas is fed to a heat recovery unit for heat exchange with the dirty syngas. Consequently, in the event of a leak in the heat recovery unit, the flow is from the clean fuel side to the dirty syngas side, thereby avoiding the possibility of contamination of the clean fuel gas.

    Abstract translation: 一种用于从脏气体燃料(合成气)回收热量的系统和方法,其中清洁燃料气体的压力升高到高于污水合成气的压力,然后加压的清洁燃料气体被供给到热回收单元以进行加热 与脏的合成气交换。 因此,在热回收单元发生泄漏的情况下,流动从清洁燃料侧到污水合成气侧,从而避免污染清洁燃料气体的可能性。

    Method of using fuel gas expander in power generating plants
    9.
    发明授权
    Method of using fuel gas expander in power generating plants 失效
    发电厂使用燃气膨胀机的方法

    公开(公告)号:US06167692A

    公开(公告)日:2001-01-02

    申请号:US09106499

    申请日:1998-06-29

    CPC classification number: F02C3/22 F02C1/00 Y02E20/16

    Abstract: In a power generating plant which utilizes fuel gas for combustion at a predetermined pressure to drive a primary load, and where the fuel gas is supplied at a pressure higher than the predetermined pressure, an improvement is provided wherein a fuel gas expander is located downstream of a source of the fuel gas and upstream of a combustor for decreasing the pressure of the fuel gas, and wherein excess energy from the expander is used to drive a secondary load.

    Abstract translation: 在利用燃料气体以预定压力燃烧以驱动初级负荷并且在高于预定压力的压力下供给燃料气体的发电厂中,提供了一种燃料气体膨胀器位于 燃料气源和用于降低燃料气体压力的燃烧器上游,并且其中使用来自膨胀机的过量能量来驱动次级负荷。

    Integrated turbomachine oxygen plant
    10.
    发明授权
    Integrated turbomachine oxygen plant 失效
    综合涡轮机氧气厂

    公开(公告)号:US08752391B2

    公开(公告)日:2014-06-17

    申请号:US12941553

    申请日:2010-11-08

    Abstract: An integrated turbomachine oxygen plant includes a turbomachine and an air separation unit. One or more compressor pathways flow compressed air from a compressor through one or more of a combustor and a turbine expander to cool the combustor and/or the turbine expander. An air separation unit is operably connected to the one or more compressor pathways and is configured to separate the compressed air into oxygen and oxygen-depleted air. A method of air separation in an integrated turbomachine oxygen plant includes compressing a flow of air in a compressor of a turbomachine. The compressed flow of air is flowed through one or more of a combustor and a turbine expander of the turbomachine to cool the combustor and/or the turbine expander. The compressed flow of air is directed to an air separation unit and is separated into oxygen and oxygen-depleted air.

    Abstract translation: 集成的涡轮机氧气设备包括涡轮机和空气分离单元。 一个或多个压缩机通道将来自压缩机的压缩空气通过燃烧器和涡轮膨胀器中的一个或多个,以冷却燃烧器和/或涡轮膨胀机。 空气分离单元可操作地连接到一个或多个压缩机路径,并且被配置为将压缩空气分离成氧气和贫氧空气。 集成涡轮机氧气设备中的空气分离方法包括压缩涡轮机的压缩机中的空气流。 压缩的空气流动流过涡轮机的燃烧器和涡轮膨胀机中的一个或多个,以冷却燃烧器和/或涡轮膨胀机。 压缩的空气流被引导到空气分离单元并被分离成氧和贫氧的空气。

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