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公开(公告)号:US20180135514A1
公开(公告)日:2018-05-17
申请号:US15276904
申请日:2016-09-27
发明人: Dinesh Venugopal Setty , Richard Lynn Loud , Pramod Akulu , Haribalakrishnan Sankarakumar , Shubhra Bhatnagar , Laxmikant Merchant
CPC分类号: F02C7/045 , F02C7/24 , F05D2240/14 , F05D2250/232 , F05D2250/51 , F05D2260/96 , F05D2260/963
摘要: The present disclosure is directed to a sound attenuation system for a gas turbine engine. The sound attenuation system includes a compressor inlet casing having a compressor inlet casing inner surface and defining a compressor inlet passage extending therethrough. An inlet plenum body couples to the compressor inlet casing. The inlet plenum body includes an inlet body inner surface and defines an inlet plenum therein. One or more sound attenuating panels couple to at least one of the compressor inlet casing inner surface and the inlet plenum body inner surface of the duct. Each sound attenuating panel includes a first sheet defining a first plurality of apertures extending therethrough and a solid second sheet spaced apart from the first sheet.
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2.
公开(公告)号:US20150345336A1
公开(公告)日:2015-12-03
申请号:US14291070
申请日:2014-05-30
CPC分类号: F01D25/28 , F01D25/24 , F05D2230/644
摘要: A support assembly for externally adjusting an inner casing with respect to an outer casing for a turbomachine includes a carrier plate, a carrier block that is fixedly connected to the carrier plate, a restrictor block fixedly connected to the carrier plate, a rod coupled to the carrier plate, and a plate threadably connected to the rod. The carrier block includes an inclined side and a carrier side. The restrictor block includes a restrictor side and an inclined side. The restrictor side is generally oriented towards the carrier side. A vertical gap for receiving a support arm of an inner turbine casing is defined between the restrictor side and the carrier side. The plate may be rotated about the rod to cause simultaneous movement of the rod, the carrier plate, the carrier block and the restrictor block, thus adjusting the inner casing with respect to the outer casing.
摘要翻译: 用于相对于用于涡轮机的外壳外部调节内壳的支撑组件包括承载板,固定地连接到承载板的承载块,固定地连接到承载板的限制块,连接到所述承载板的杆 承载板和螺纹连接到杆的板。 载体块包括倾斜侧和载体侧。 限流块包括限流器侧和倾斜侧。 限流器侧通常朝向载体侧定向。 用于接收内涡轮机壳体的支撑臂的垂直间隙限定在限流器侧和载体侧之间。 板可以围绕杆旋转以引起杆,承载板,承载块和限制块的同时移动,从而相对于外壳调节内壳。
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公开(公告)号:US09611759B2
公开(公告)日:2017-04-04
申请号:US14291070
申请日:2014-05-30
CPC分类号: F01D25/28 , F01D25/24 , F05D2230/644
摘要: A support assembly for externally adjusting an inner casing with respect to an outer casing for a turbomachine includes a carrier plate, a carrier block that is fixedly connected to the carrier plate, a restrictor block fixedly connected to the carrier plate, a rod coupled to the carrier plate, and a plate threadably connected to the rod. The carrier block includes an inclined side and a carrier side. The restrictor block includes a restrictor side and an inclined side. The restrictor side is generally oriented towards the carrier side. A vertical gap for receiving a support arm of an inner turbine casing is defined between the restrictor side and the carrier side. The plate may be rotated about the rod to cause simultaneous movement of the rod, the carrier plate, the carrier block and the restrictor block, thus adjusting the inner casing with respect to the outer casing.
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