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11.发明申请公开(公告)号：US20180080376A1
公开(公告)日：2018-03-22
申请号：US15272050
申请日：2016-09-21
Applicant: General Electric Company
Inventor： Kenneth Robert Austin , Vineet Sethi , Raymond Kalok Fong , Jose Emmanuel Guillen , Robert Allen Baten , Donald Gordon Laing
CPC classification number: F02C6/00 , F02B63/044 , F02C3/04 , F05D2220/76 , F16M3/00 , H02K7/1823
Abstract: A system includes a first mobile body configured to support a turbine engine and an air intake section coupled to the turbine engine. The system also includes a second mobile body configured to support a generator. The first and second mobile bodies are configured to guide a removable coupling between the turbine engine and the generator. The system also includes a third mobile body configured to support one or more partially assembled components associated with the turbine engine and the generator.
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公开(公告)号：US09644496B2
公开(公告)日：2017-05-09
申请号：US13798614
申请日：2013-03-13
Applicant: General Electric Company
Inventor： Fernando Lopez-Parra , Balakrishnan Ponnuraj , Przemyslaw Drezek , Mehdi Milani Baladi , Ravinder Yerram , Donald Gordon Laing
IPC: F01D25/30
CPC classification number: F01D25/30
Abstract: The present application provides a radial diffuser exhaust system for use with a gas turbine engine. The radial diffuser exhaust system may include a radial diffuser positioned within an asymmetric exhaust collector. The asymmetric exhaust collector may include a closed end chamber and an exhaust end chamber. The closed end chamber may have a first size, the exhaust end chamber may have a second size, and the first size may be smaller than the second size.
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公开(公告)号：US10697637B2
公开(公告)日：2020-06-30
申请号：US15820739
申请日：2017-11-22
Applicant: General Electric Company
Inventor： Ravinder Yerram , Balakrishnan Ponnuraj , Yalid Mariluz Lopez Moctezuma , Donald Gordon Laing , Gerardo Plata , Timothy Martin Christensen
Abstract: A gas turbine system includes a plenum that includes an inlet and an outlet. The inlet is configured to receive a flow of oxidant and the outlet is configured to direct the flow of oxidant in a downstream direction. Additionally, a support system is coupled to the plenum and to a cone. The support system enables the cone to move along the support system from a first position to a second position. The cone includes an upstream end and the upstream end is removably coupled to the outlet of the plenum in the first position. When the cone is in the first position, the cone is configured to direct the flow of oxidant in the downstream direction to a gas turbine engine. The upstream end is disposed upstream of the outlet and is decoupled from the outlet when the cone is in the second position.
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14.发明授权公开(公告)号：US10184397B2
公开(公告)日：2019-01-22
申请号：US15272050
申请日：2016-09-21
Applicant: General Electric Company
Inventor： Kenneth Robert Austin , Vineet Sethi , Raymond Kalok Fong , Jose Emmanuel Guillen , Robert Allen Baten , Donald Gordon Laing
Abstract: A system includes a first mobile body configured to support a turbine engine and an air intake section coupled to the turbine engine. The system also includes a second mobile body configured to support a generator. The first and second mobile bodies are configured to guide a removable coupling between the turbine engine and the generator. The system also includes a third mobile body configured to support one or more partially assembled components associated with the turbine engine and the generator.
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公开(公告)号：US10125689B2
公开(公告)日：2018-11-13
申请号：US15348446
申请日：2016-11-10
Applicant: General Electric Company
Inventor： Stephen Matthew Biffle , Donald Gordon Laing , Jorge Mario Rochin Machado , Ramune Auzelyte
Abstract: A diffuser removal tool for displacing an exhaust diffuser from a gas turbine engine is provided, which includes a pair of support arms, a clamp and wedge assembly coupled to an exhaust diffuser, and a lead screw assembly coupled between the support arms and to the clamp and wedge assembly via a wedge of the clamp and wedge assembly. The tool also includes a pair of linear bearing assemblies coupled to the support arms and to the clamp and wedge assembly via wedges of the clamp and wedge assembly. The lead screw assembly is configured to displace the diffuser in an axial direction relative to a longitudinal axis of the gas turbine engine while the linear bearing assemblies are configured to both enable the displacement of the diffuser in the axial direction while vertically supporting the diffuser to maintain alignment between the diffuser and the gas turbine engine.
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Patent Agency Ranking
16.发明授权公开(公告)号：US10030579B2
公开(公告)日：2018-07-24
申请号：US15272100
申请日：2016-09-21
Applicant: General Electric Company
Inventor： Kenneth Robert Austin , Vineet Sethi , Raymond Kalok Fong , Jose Emmanuel Guillen , Robert Allen Baten , Donald Gordon Laing
IPC: F02B63/04 , F03G7/08 , H02K7/18 , F02C6/00 , F02C3/04 , B60D1/00 , B62D53/00 , F16M5/00 , F16M3/00 , F02C7/20 , E21B4/04
CPC classification number: F02C6/00 , B60D1/00 , B62D53/00 , F02B63/044 , F02C3/04 , F05D2220/76 , F16M3/00 , F16M5/00 , H02K7/1823
Abstract: A system a first mobile body configured to support a turbine engine and an auxiliary skid communicatively and fluidly coupled to the turbine engine. The auxiliary skid includes one or more interconnects configured to support a turbine engine component. The system also includes a second mobile body configured to support a generator. The first and second mobile bodies are configured to align a removable coupling between the turbine engine and the generator.
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公开(公告)号：US20180030895A1
公开(公告)日：2018-02-01
申请号：US15222123
申请日：2016-07-28
Applicant: General Electric Company
Inventor： Donald Gordon Laing , Eric Tracy Watson , Balakrishnan Ponnuraj , Ravinder Yerram
Abstract: A system includes a modularized air inlet system. The modularized air inlet system includes an air filter house section configured to receive air via an air inlet. The modularized air inlet system also includes a transition/silencer section configured to direct the air from the modularized air inlet system, via an air outlet, into an air inlet plenum coupled to a gas turbine engine enclosure. The modularized air inlet system is configured to couple directly to the air inlet plenum and the gas turbine enclosure without an expansion joint disposed between the modularized air inlet system and the air inlet plenum.
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公开(公告)号：US20170306846A1
公开(公告)日：2017-10-26
申请号：US15135874
申请日：2016-04-22
Applicant: General Electric Company
Inventor： Donald Gordon Laing , Jose Antonio Cordova Magaña , Victor Alfonso Gonzalez Tellez , Oswaldo Alberto Sanchez Rubio
CPC classification number: F02C7/18 , F01D25/14 , F02C3/04 , F02C7/00 , F02C7/12 , F05D2220/32 , F05D2260/601 , F05D2260/608 , Y02T50/675
Abstract: A ventilation system for a turbomachine enclosure includes: a bladeless airflow amplifier configured to pass an airflow through at least a portion of the turbomachine enclosure; and an amplifier airflow source fluidly coupled to the bladeless airflow amplifier for providing an operative airflow to operate the bladeless airflow amplifier. The ventilation system may be employed with or without a conventional vent fan system.
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公开(公告)号：US09410451B2
公开(公告)日：2016-08-09
申请号：US13693113
申请日：2012-12-04
Applicant: General Electric Company
Inventor： Donald Gordon Laing , Charles Michael Booth
IPC: F01K23/10
CPC classification number: F01K23/10 , F01K23/103 , Y02E20/16
Abstract: The present application provides an integrated bottoming cycle system for use with a gas turbine engine. The integrated bottoming cycle system described herein may include a compressor/pump, a cooling circuit downstream of the compressor/pump, a bottoming cycle heat exchanger, a heating circuit downstream of the bottoming cycle heat exchanger, and a number of turbine components in communication with the cooling circuit and/or the heating circuit to maximize the overall plant efficiency and economics.
Abstract translation: 本申请提供了一种用于燃气涡轮发动机的综合底循环系统。 本文所述的集成底循环系统可以包括压缩机/泵，压缩机/泵下游的冷却回路，底循环热交换器，底循环热交换器下游的加热回路，以及与 冷却回路和/或加热回路，以最大化整个设备的效率和经济性。
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公开(公告)号：US20140150443A1
公开(公告)日：2014-06-05
申请号：US13693113
申请日：2012-12-04
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Donald Gordon Laing , Charles Michael Booth
IPC: F01K23/10
CPC classification number: F01K23/10 , F01K23/103 , Y02E20/16
Abstract: The present application provides an integrated bottoming cycle system for use with a gas turbine engine. The integrated bottoming cycle system described herein may include a compressor/pump, a cooling circuit downstream of the compressor/pump, a bottoming cycle heat exchanger, a heating circuit downstream of the bottoming cycle heat exchanger, and a number of turbine components in communication with the cooling circuit and/or the heating circuit to maximize the overall plant efficiency and economics.
Abstract translation: 本申请提供了一种用于燃气涡轮发动机的综合底循环系统。 本文所述的集成底循环系统可以包括压缩机/泵，压缩机/泵下游的冷却回路，底循环热交换器，底循环热交换器下游的加热回路，以及与 冷却回路和/或加热回路，以最大化整个设备的效率和经济性。
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