MULTI-STAGE COMPRESSOR
    1.
    发明申请
    MULTI-STAGE COMPRESSOR 有权
    多级压缩机

    公开(公告)号:US20120100015A1

    公开(公告)日:2012-04-26

    申请号:US13280789

    申请日:2011-10-25

    Abstract: Provided is a multi-stage compressor which includes: a first-stage compressing unit which includes a first compressing element with an impeller and a second compressing element with an impeller, the first and second compressing elements being connected to each other; and a rear-stage compressing unit which includes at least one rear compressing element with an impeller, wherein the rear-stage compressing unit receives a fluid compressed and output from the first-stage compressing unit.

    Abstract translation: 提供一种多级压缩机,其包括:第一级压缩单元,其包括具有叶轮的第一压缩元件和具有叶轮的第二压缩元件,所述第一和第二压缩元件彼此连接; 以及后级压缩单元,其包括具有叶轮的至少一个后部压缩元件,其中后级压缩单元接收从第一级压缩单元压缩并输出的流体。

    TURBINE SYSTEM
    2.
    发明申请
    TURBINE SYSTEM 有权
    涡轮系统

    公开(公告)号:US20110225977A1

    公开(公告)日:2011-09-22

    申请号:US12831768

    申请日:2010-07-07

    Abstract: A turbine system includes a compressor unit which compresses a fluid; a combustor unit which burns fuel with the compressed fluid; a turbine unit which is driven due to a combustion gas that is generated when the combustor unit burns the fuel; and a first device which receives power that is generated when the turbine unit is driven. The at least one compressor unit operates using at least the generated power, and is separately disposed from at least one of the turbine unit and the first device.

    Abstract translation: 涡轮机系统包括压缩流体的压缩机单元; 燃烧器单元,其用压缩流体燃烧燃料; 涡轮单元,其由燃烧器单元燃烧燃料时产生的燃烧气体驱动; 以及第一装置,其接收在所述涡轮机单元被驱动时产生的功率。 所述至少一个压缩机单元至少使用所产生的功率进行操作,并且与所述涡轮机单元和所述第一设备中的至少一个单独设置。

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