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Patent Agency Ranking
公开(公告)号：US20180010617A1
公开(公告)日：2018-01-11
申请号：US15206464
申请日：2016-07-11
Applicant: General Electric Company
Inventor： Matthew Stephen Casavant , Kenneth Damon Black , Christian Michael Hansen , Donald Earl Floyd , James Adaickalasamy , Brett Darrick Klingler , Khoa Dang Cao , Kyle Eric Benson , Devin Patrick Perkins , Damian Anthony McClelland
CPC classification number: F04D29/642 , F01D11/18 , F01D25/005 , F01D25/24 , F02C3/04 , F04D29/023 , F04D29/324 , F04D29/522 , F04D29/526 , F04D29/542 , F05D2220/32 , F05D2220/3216 , F05D2240/12 , F05D2260/97 , F05D2300/173 , F05D2300/174 , F05D2300/177 , F05D2300/50212
Abstract: A gas turbine engine is disclosed having a turbine, one or more hydrocarbon gas combustors, and a compressor. The compressor has a rotor assembly with one or more rotor blade rows extending radially outward from an inner wheel disk. The compressor also has a stator assembly with one or more stator vane rows extending radially inward from an inner casing and positioned between adjacent rotor blade rows. The inner casing extends circumferentially around the rotor assembly and is constructed from at least one low-alpha metal alloy.
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公开(公告)号：US20150345336A1
公开(公告)日：2015-12-03
申请号：US14291070
申请日：2014-05-30
Applicant: General Electric Company
Inventor： James Adaickalasamy , Pramod Akulu , Kenneth Damon Black
CPC classification number: F01D25/28 , F01D25/24 , F05D2230/644
Abstract: 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.
Abstract translation: 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：US10119471B2
公开(公告)日：2018-11-06
申请号：US14879470
申请日：2015-10-09
Applicant: General Electric Company
Inventor： Debabrata Mukhopadhyay , Pugalenthi Nandagopal , James Adaickalasamy
Abstract: A turbine engine assembly is provided. The assembly includes a compressor, and an air duct coupled in flow communication with the compressor. The air duct is configured to channel a flow of bleed air from the compressor therethrough. The assembly also includes a fluid supply system coupled in flow communication with the air duct, wherein the fluid supply system is configured to channel a flow of fluid towards the air duct to modify a temperature of the bleed air based on an operating condition of the turbine engine assembly.
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公开(公告)号：US20170101933A1
公开(公告)日：2017-04-13
申请号：US14879470
申请日：2015-10-09
Applicant: General Electric Company
Inventor： Debabrata Mukhopadhyay , Pugalenthi Nandagopal , James Adaickalasamy
CPC classification number: F02C7/185 , F01D11/24 , F01K23/10 , F02C3/04 , F02C7/14 , F05D2220/32 , F05D2220/72 , F05D2260/213
Abstract: A turbine engine assembly is provided. The assembly includes a compressor, and an air duct coupled in flow communication with the compressor. The air duct is configured to channel a flow of bleed air from the compressor therethrough. The assembly also includes a fluid supply system coupled in flow communication with the air duct, wherein the fluid supply system is configured to channel a flow of fluid towards the air duct to modify a temperature of the bleed air based on an operating condition of the turbine engine assembly.
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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
Applicant: General Electric Company
Inventor： James Adaickalasamy , Pramod Akulu , Kenneth Damon Black
CPC classification number: F01D25/28 , F01D25/24 , F05D2230/644
Abstract: 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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