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公开(公告)号:US09309842B2
公开(公告)日:2016-04-12
申请号:US13761305
申请日:2013-02-07
Applicant: General Electric Company
Inventor: Eric Tracy Watson , Robert Allen Baten , Doyle Jackson Marrs
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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公开(公告)号:US20140219781A1
公开(公告)日:2014-08-07
申请号:US13761305
申请日:2013-02-07
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Eric Tracy Watson , Robert Allen Baten , Doyle Jackson Marrs
IPC: F02M35/12
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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