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1.发明公开公开(公告)号：US20230193825A1
公开(公告)日：2023-06-22
申请号：US18112296
申请日：2023-02-21
Applicant: General Electric Company
IPC: F02C7/05
CPC classification number: F02C7/05 , F05D2240/35 , F05D2250/221 , F05D2260/607
Abstract: An inlet filter housing includes a plurality of components that collectively form a complete filtering and conditioning system for filtering and conditioning a fluid along a housing flow path. Each component is fitted within an external structure of an International Organization of Standards (ISO) shipping container, which provides a rectangular cuboid enclosure. Each component includes operative structure of at least one of: a) only a portion of an axial extent of the filtering and conditioning system, and b) only a portion of a lateral cross-sectional area of the housing flow path.
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公开(公告)号：US20170350278A1
公开(公告)日：2017-12-07
申请号：US15171838
申请日：2016-06-02
Applicant: General Electric Company
Inventor： Likhith Reddy Asani , Dinesh Venugopal Setty , Jeffrey Patrick Mills , Nicholas Demianovich
CPC classification number: F01D25/28 , F05D2220/30 , F05D2260/02 , F16M1/04 , F16M5/00 , F16M7/00
Abstract: A support assembly supports a gas turbine in a manufacturing configuration, a shipping configuration and an operating configuration. The support assembly includes a stand leg securable to a base, where the stand leg includes a turbine casing interface with a slot sized to receive a turbine casing pin. A support plate attachable to the turbine casing interface includes a pin aperture that is sized to fit over the turbine casing pin in the slot.
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公开(公告)号：US09890713B2
公开(公告)日：2018-02-13
申请号：US14638472
申请日：2015-03-04
Applicant: General Electric Company
Inventor： Hua Zhang , Dinesh Venugopal Setty , Laxmikant Merchant , Valery Ivanovich Ponyavin
CPC classification number: F02C7/045 , B64D29/00 , F02C3/30 , F02C7/047 , F05D2260/96
Abstract: A silencer apparatus for a gas turbine inlet system ducting is disclosed. The inlet ducting contains a main silencer and a pre-silencer, and Inlet Bleed Heat (“IBH”) located between the silencers. The pre-silencer decreases the noise level from the turbine compressor and makes the air flow/temperature profiles more uniform. The main silencer reduces noise from the IBH and the remaining noise from the compressor to an appropriate level. The main silencer is comprised of a first plurality of sound-absorbing splitters disposed along the gas flow direction in the gas turbine inlet ducting. The pre-silencer is comprised of a second plurality of sound-absorbing splitters disposed along the gas flow direction in the gas turbine inlet ducting, but staggered with respect to the first plurality of splitters to thereby block a direct line of travel for noise acoustical waves from the compressor travelling opposite the gas flow direction in the inlet ducting.
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公开(公告)号：US09771865B2
公开(公告)日：2017-09-26
申请号：US14525494
申请日：2014-10-28
Applicant: General Electric Company
Inventor： Laxmikant Merchant , Richard Lynn Loud , Valery Ivanovich Ponyavin , Dinesh Venugopal Setty , Hua Zhang
Abstract: An inlet bleed heat (IBH) system manifold for a compressor inlet housing is provided. The manifold includes: a plurality of feed pipes for delivering a compressor discharge air, each feed pipe extending across a duct of the compressor inlet housing. Each feed pipe includes: an elongated inner feed pipe for delivering the compressor discharge air, the inner feed pipe including a plurality of orifices along at least a portion of a length of the inner feed pipe, each orifice extending through a wall of the inner feed pipe allowing the compressor discharge air to exit the inner feed pipe; and a noise attenuating material disposed about the inner feed pipe and the plurality of orifices, the noise attenuating material configured to attenuate noise created by the compressor discharge air exiting the plurality of orifices.
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公开(公告)号：US20140311160A1
公开(公告)日：2014-10-23
申请号：US13960155
申请日：2013-08-06
Applicant: General Electric Company
Inventor： Kiran Swarup Kasturi , Antoine Hochar , Dinesh Venugopal Setty
IPC: F02C7/20
CPC classification number: F02C7/20 , E04H5/02 , F02C7/00 , F16M9/00 , Y10T29/49229
Abstract: A hybrid turbomachine enclosure includes a plurality of walls interconnected to form an interior configured and disposed to receive a turbomachine, the plurality of walls including a first wall having a panel on frame construction and a hybrid wall including a first portion having a panel on frame structure and a second portion having a stiffened frame panel structure.
Abstract translation: 混合涡轮机壳体包括互连的多个壁，以形成配置和设置成容纳涡轮机的内部，所述多个壁包括具有框架结构的面板的第一壁和包括第一部分的混合壁，所述第一部分具有框架结构上的面板 以及具有加强的框架面板结构的第二部分。
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Patent Agency Ranking
公开(公告)号：US11988142B2
公开(公告)日：2024-05-21
申请号：US18112296
申请日：2023-02-21
Applicant: General Electric Company
IPC: F02C7/05
CPC classification number: F02C7/05 , F05D2240/35 , F05D2250/221 , F05D2260/607
Abstract: An inlet filter housing includes a plurality of components that collectively form a complete filtering and conditioning system for filtering and conditioning a fluid along a housing flow path. Each component is fitted within an external structure of an International Organization of Standards (ISO) shipping container, which provides a rectangular cuboid enclosure. Each component includes operative structure of at least one of: a) only a portion of an axial extent of the filtering and conditioning system, and b) only a portion of a lateral cross-sectional area of the housing flow path.
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公开(公告)号：US10240482B2
公开(公告)日：2019-03-26
申请号：US15222102
申请日：2016-07-28
Applicant: General Electric Company
Inventor： Laxmikant Merchant , Dinesh Venugopal Setty , Avishetti Srinivas , S. T. Deepak
Abstract: A gas turbine system includes a load coupling connecting a gas turbine to a generator. A load coupling guard surrounds the load coupling to define an enclosed spaced around the load coupling. The load coupling guard includes a porous sleeve such that hydrogen coolant leaked into the load coupling guard from the generator is vented to ambient air.
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公开(公告)号：US10196199B2
公开(公告)日：2019-02-05
申请号：US15169974
申请日：2016-06-01
Applicant: General Electric Company
Inventor： Nicholas Demianovich , Dinesh Venugopal Setty , Jeffrey Patrick Mills , Likhith Reddy Asani
Abstract: A progressive shipping stand includes a stage one assembly, and a stage two assembly. The stage one assembly and the stage two assembly together define a first profile, and the stage two assembly alone defines a second profile, smaller than the first profile. The stage two assembly may be attachable directly to a load. The stage two assembly is operable independently in a discrete support configuration and is selectively cooperable with the stage one assembly in a full support configuration. The shipping support allows for large machinery such as a turbine or the like to meet at least one shipping criteria that would not otherwise be feasible using a standard shipping support.
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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
Applicant: General Electric Company
Inventor： Dinesh Venugopal Setty , Richard Lynn Loud , Pramod Akulu , Haribalakrishnan Sankarakumar , Shubhra Bhatnagar , Laxmikant Merchant
CPC classification number: F02C7/045 , F02C7/24 , F05D2240/14 , F05D2250/232 , F05D2250/51 , F05D2260/96 , F05D2260/963
Abstract: 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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公开(公告)号：US20170074289A1
公开(公告)日：2017-03-16
申请号：US14855902
申请日：2015-09-16
Applicant: General Electric Company
Inventor： Laxmikant Merchant , Javeed Iqbaluddin Mohammed , Valery Ivanovich Ponyavin , Dinesh Venugopal Setty , Hua Zhang
Abstract: A silencer duct that may be part of, for example, a turbomachine inlet and may include a duct body, and a silencer element extending axially through the duct body. A first portion of a coupler may extend axially from a first side of the duct body. A second portion of a coupler may extend axially from a second side of the duct body. At least one of the first portion of the coupler and the second portion of the coupler are configured to couple to at least one of an adjacent silencer duct and an inlet.
Abstract translation: 可以是例如涡轮机入口的一部分的消音器管道，并且可以包括管道主体和沿轴向延伸穿过管道主体的消音器元件。 耦合器的第一部分可以从导管主体的第一侧轴向延伸。 耦合器的第二部分可以从导管主体的第二侧轴向延伸。 耦合器的第一部分和耦合器的第二部分中的至少一个被配置成耦合到相邻的消声器导管和入口中的至少一个。
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