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41.发明申请公开(公告)号：US20220082051A1
公开(公告)日：2022-03-17
申请号：US17019415
申请日：2020-09-14
Applicant: General Electric Company
IPC: F02C7/05
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：US20200284261A1
公开(公告)日：2020-09-10
申请号：US16883536
申请日：2020-05-26
Applicant: General Electric Company
Inventor： Laxmikant Merchant , Valery Ivanovich Ponyavin , Jeffrey Patrick Mills , Divya Reddy Kothakapu , Weilun Yu , Joshua Adam Bagwell
Abstract: A liquid injection apparatus for use with a compressor having a rotor shaft and a casing part is provided. The liquid injection apparatus includes at least one conduit and at least one nozzle coupled to the conduit(s). The liquid injection apparatus is panel-shaped and has a first panel segment, a second panel segment, and at least one of: a passage defined between the first panel segment and the second panel segment, the passage sized to receive at least one of the rotor shaft and the casing part; and a third panel segment positioned between the first panel segment and the second panel segment. The third panel segment is at least in part detachable from the first panel segment and/or the second panel segment for receiving at least one of the rotor shaft and the casing part between the first panel segment and the second panel segment.
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公开(公告)号：US10465714B2
公开(公告)日：2019-11-05
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.
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Patent Agency Ranking
公开(公告)号：US20190003387A1
公开(公告)日：2019-01-03
申请号：US15636811
申请日：2017-06-29
Applicant: General Electric Company
Inventor： Valery Ivanovich Ponyavin , Bradly Aaron Kippel , Laxmikant Merchant , Hua Zhang , Naveen Parmeshwar
CPC classification number: F02C7/047 , F02C3/04 , F02C6/08 , F02C7/042 , F02C7/045 , F02C7/24 , F02C9/18 , F04D27/0215 , F04D29/023 , F04D29/5853 , F04D29/663 , F04D29/665 , F04D29/701 , F05D2220/32 , F05D2260/231 , F05D2300/611
Abstract: An inlet bleed heat (IBH) system for use in a turbine engine including a silencer assembly. The inlet bleed heat (IBH) system includes a feed pipe for delivering compressor discharge air. The feed pipe includes a plurality of orifices along at least a portion of a length of the feed pipe, and each orifice of the plurality of orifices extends through a wall of the feed pipe for allowing the compressor discharge air to exit the feed pipe. The system also includes a heat shielding component that extends across the feed pipe, wherein the heat shielding component is configured to reduce heat transfer between the feed pipe and the silencer assembly of the turbine engine.
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公开(公告)号：US20170254222A1
公开(公告)日：2017-09-07
申请号：US15062958
申请日：2016-03-07
Applicant: General Electric Company
Inventor： Hua Zhang , Laxmikant Merchant , Bradly Aaron Kippel , Valery Ivanovich Ponyavin
CPC classification number: F01D25/305 , F01D9/065 , F02C7/141 , F02C7/18 , F05D2220/32 , F05D2240/35
Abstract: A gas turbine system includes an exhaust processing system that may process exhaust gas generated by a gas turbine engine, the exhaust processing system includes an exhaust diffuser that may receive the exhaust gas from a turbine of the gas turbine engine and having an annular passage disposed between an inner annular wall and an outer annular wall, and an air injection assembly disposed within the exhaust diffuser. The air injection assembly includes one or more air injection conduits disposed within the annular passage of the exhaust diffuser and including fluid injection holes that may direct a cooling fluid into a first mixing region of the exhaust diffuser.
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公开(公告)号：US20170074288A1
公开(公告)日：2017-03-16
申请号：US14855901
申请日：2015-09-16
Applicant: General Electric Company
Inventor： Dinesh Venugopal Setty , Dale Joel Davis , Laxmikant Merchant , Valery Ivanovich Ponyavin , Hua Zhang
CPC classification number: F04D29/664 , F02C7/045 , F04D29/522 , F04D29/545 , F05D2250/132 , F05D2250/191 , F05D2260/96
Abstract: A silencer duct that may be part of, for example, a turbomachine inlet may include a duct body. A first perforated wall extends within the duct body and substantially parallel to an interior surface of the duct body. A first acoustic absorbing material may be positioned between the duct body and the first perforated wall. A silencer element may extend axially through the duct body, the silencer element including a second perforated wall having a second acoustic absorbing material adjacent thereto.
Abstract translation: 可以是例如涡轮机入口的一部分的消音器管道可以包括管道主体。 第一穿孔壁在管道主体内延伸并基本上平行于管体的内表面。 第一吸声材料可以定位在管道主体和第一穿孔壁之间。 消声器元件可以轴向延伸穿过管道主体，消声器元件包括具有与其相邻的第二吸声材料的第二穿孔壁。
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公开(公告)号：US20170037781A1
公开(公告)日：2017-02-09
申请号：US14821031
申请日：2015-08-07
Applicant: General Electric Company
Inventor： Valery Ivanovich Ponyavin , Hua Zhang , Dinesh Venugopal Setty , Laxmikant Merchant
IPC: F02C7/045
CPC classification number: F02C7/045 , F05D2220/32 , F05D2260/96
Abstract: An inlet system for a gas turbine includes an inlet duct, a silencer assembly disposed downstream from the inlet duct and an outlet duct disposed downstream from the silencer assembly. The silencer assembly may include a duct and a plurality of laterally spaced baffles disposed within the duct. The baffles may be arranged substantially parallel to a flow of air flowing through the inlet system. Each baffle includes a leading edge portion, a trailing edge portion that is longitudinally spaced from the leading edge portion and a pair of laterally opposing side walls that extend between the leading and trailing edges. Each baffle includes at least one acoustic panel that extends at least partially across one side wall of the pair of side walls.
Abstract translation: 用于燃气涡轮机的入口系统包括入口管道，设置在入口管道下游的消音器组件和设置在消声器组件下游的出口管道。 消音器组件可以包括管道和设置在管道内的多个横向隔开的挡板。 挡板可以布置成基本上平行于流过入口系统的空气流。 每个挡板包括前缘部分，与前缘部分纵向间隔开的后缘部分和在前缘和后缘之间延伸的一对横向相对的侧壁。 每个挡板包括至少一个至少部分地跨过该对侧壁的一个侧壁延伸的隔音板。
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公开(公告)号：US09506835B2
公开(公告)日：2016-11-29
申请号：US14259716
申请日：2014-04-23
Applicant: General Electric Company
Inventor： Rajesh Reddy Konatham , Len Alan Wolf , Laxmikant Merchant , Rajakumar Alagappan , Lakshmi Bettadapura Shankar
Abstract: A fuel leak detection system for use in a turbine enclosure is provided. The system includes a ventilation duct extending through an interior cavity of the turbine enclosure such that an extended portion of the ventilation duct is positioned within a bottom portion of the turbine enclosure. The ventilation duct includes a plurality of openings configured to allow air from within the turbine enclosure to be drawn into the ventilation duct through the plurality of openings. The system also includes a sensor system coupled in flow communication with the air drawn into the ventilation duct, the sensor system configured to detect fuel in the air.
Abstract translation: 提供了一种用于涡轮机外壳的燃油泄漏检测系统。 该系统包括延伸穿过涡轮机壳体的内部空腔的通气管道，使得通风管道的延伸部分位于涡轮机壳体的底部内。 通风管道包括多个开口，其被配置为允许来自涡轮机壳体内的空气通过多个开口被吸入通风管道。 该系统还包括传感器系统，该传感器系统与被吸入到通风管道中的空气流动连通地耦合，所述传感器系统构造成检测空气中的燃料。
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