SYSTEM FOR VENTILATING A GAS TURBINE ENCLOSURE
    3.
    发明申请
    SYSTEM FOR VENTILATING A GAS TURBINE ENCLOSURE 有权
    气体涡轮机外壳通风系统

    公开(公告)号:US20150276247A1

    公开(公告)日:2015-10-01

    申请号:US14735963

    申请日:2015-06-10

    Abstract: A turbine ventilation system includes at least one fan configured to provide a first air flow into a gas turbine enclosure, a fan bypass configured to circumvent the at least one fan to provide a second air flow into the gas turbine enclosure, and an eductor configured to draw the first or second air flows through and out of the gas turbine enclosure.

    Abstract translation: 涡轮机通风系统包括至少一个风扇,其被配置为将第一空气流提供到燃气涡轮机外壳中,风扇旁路,其构造成绕过所述至少一个风扇以提供第二空气流进入所述燃气涡轮机壳体;以及喷射器, 将第一或第二空气流过和流出燃气轮机外壳。

    Air inlet silencer for turbomachines
    9.
    发明授权
    Air inlet silencer for turbomachines 有权
    用于涡轮机的进气消音器

    公开(公告)号:US09309842B2

    公开(公告)日:2016-04-12

    申请号:US13761305

    申请日:2013-02-07

    CPC classification number: F02M35/12 F04D29/664 F04D29/665 F04D29/668

    Abstract: An air inlet silencer for turbomachines is provided. In one embodiment, the air inlet silencer includes a body, and a plurality of concentric baffles coupled to and axially surrounding the body. In another embodiment, an air inlet system for a turbomachine includes the air inlet silencer, as discussed herein, positioned within a silencer housing. The air inlet system may also include a deflector positioned within the silencer housing adjacent the air inlet silencer. In a further embodiment, a turbomachine includes a turbine coupled to a compressor, and an air inlet system, as described herein, coupled to the compressor.

    Abstract translation: 提供了用于涡轮机的进气消音器。 在一个实施例中,空气入口消音器包括主体和耦合到并且轴向包围主体的多个同心挡板。 在另一个实施例中,用于涡轮机的进气系统包括位于消声器壳体内的如本文所讨论的进气消音器。 空气入口系统还可以包括定位在邻近空气入口消声器的消音器壳体内的偏转器。 在进一步的实施例中,涡轮机包括联接到压缩机的涡轮机和联接到压缩机的如本文所述的空气入口系统。

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