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    • 1. 发明授权
    • Integrated turbomachine oxygen plant
    • 综合涡轮机氧气厂
    • US08752391B2
    • 2014-06-17
    • US12941553
    • 2010-11-08
    • Ashok Kumar AnandRichard Anthony DePuyVeerappan Muthaiah
    • Ashok Kumar AnandRichard Anthony DePuyVeerappan Muthaiah
    • F02C6/00
    • B01D53/22B01D2256/12B01D2257/102F02C3/28F02C6/00F02C6/18Y02E20/18
    • 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.
    • 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。
    • 4. 发明申请
    • Integrated Turbomachine Oxygen Plant
    • 综合涡轮机氧气厂
    • US20120111021A1
    • 2012-05-10
    • US12941553
    • 2010-11-08
    • Ashok Kumar AnandRichard Anthony DePuyVeerappan Muthaiah
    • Ashok Kumar AnandRichard Anthony DePuyVeerappan Muthaiah
    • F02C6/00
    • B01D53/22B01D2256/12B01D2257/102F02C3/28F02C6/00F02C6/18Y02E20/18
    • 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.
    • 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。
    • 6. 发明授权
    • Integrated gasification combined cycle power plant with kalina bottoming cycle
    • 综合气化联合循环发电厂与卡利纳底循环
    • US06216436B1
    • 2001-04-17
    • US09173122
    • 1998-10-15
    • Jatila RanasingheAshok Kumar AnandRaub Warfield Smith
    • Jatila RanasingheAshok Kumar AnandRaub Warfield Smith
    • F02C328
    • F01K23/068F01K25/065F02C3/28Y02E20/16Y02E20/18
    • An integrated gasification combined cycle plant is combined with a Kalina bottoming cycle. High thermal energy streams 31, 69, 169 from the gasification system are provided in heat exchange relation with the two component working fluid mixture at appropriate locations along the Kalina bottoming cycle units to supplement the thermal energy from the gas turbine exhaust 28 which heats the working fluid supplied to the vapor turbines. Particularly, low temperature heat recovery fluid from the low temperature cooling section 50b of the gasification system lies in heat exchange relation 27 with the condensed working fluid from the distillation/condensation sub-system of the Kalina cycle to preheat the working fluid prior to entry into the heat recovery vapor generator 12. Heat recovery fluid from the high temperature gas cooling section 50a of the gasification system is placed in heat exchange relation 23 and 65 with the working fluid at an intermediate location along the heat recovery vapor generator 12. By supplementing the heat of the gas turbine exhaust with available heat from the gasification system, and optimal integration, increased power output and improved efficiency are obtained.
    • 综合气化联合循环设备与Kalina底循环相结合。 提供来自气化系统的高热能流31,69,169与沿着Kalina底循环单元的适当位置处的两组分工作流体混合物以热交换关系提供,以补充来自加热工作的燃气轮机排气28的热能 提供给蒸汽涡轮机的流体。 特别地,来自气化系统的低温冷却部分50b的低温热回收流体与热交换关系27与来自Kalina循环的蒸馏/冷凝子系统的冷凝的工作流体在进入之前预热工作流体 热回收蒸汽发生器12.来自气化系统的高温气体冷却部分50a的热回收流体与工作流体沿着热回收蒸汽发生器12位于中间位置处于热交换关系23和65中。通过补充 获得了来自气化系统的可用热量的燃气轮机废气的热量,并且获得最佳的积分,增加的功率输出和提高的效率。