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公开(公告)号：US20180142956A1
公开(公告)日：2018-05-24
申请号：US15358310
申请日：2016-11-22
Applicant: General Electric Company
Inventor： Sebastian Walter Freund
CPC classification number: F28D1/0435 , F28B1/06 , F28D1/05308 , F28D1/05341 , F28D21/0014 , F28D2021/0026 , F28D2021/0064 , F28F1/12 , F28F1/24 , F28F2250/106
Abstract: The present application provides a heat exchanger for exchanging heat between two fluid flows in cross-flow arrangement. The heat exchanger includes at least one heat exchanging module including a first heat exchanging component and a second heat exchanging component. The first heat exchanging component including a fluid inlet header, a fluid outlet header, and at least one heat exchanging passageway defining a first tube-side fluid flow path of a first portion of a fluid in a first direction. The second heat exchanging component including a fluid inlet header, a fluid outlet header, and at least one heat exchanging passageway defining a second tube-side fluid flow path in a second direction for an additional portion of the fluid, wherein the first direction is opposed to the second direction. The opposing first tube-side fluid flow path and the second tube-side fluid flow path equalizing the temperature distribution over the cross-section of a cross-flow fluid exiting the module.
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Patent Agency Ranking
公开(公告)号：US20170328234A1
公开(公告)日：2017-11-16
申请号：US15155823
申请日：2016-05-16
Applicant: General Electric Company
Inventor： Rodrigo Rodriguez Erdmenger , Sebastian Walter Freund , Ismail Hakki Sezal , Aneesh Sridhar Vadvadgi
CPC classification number: F01D17/141 , F01D9/041 , F01D9/045 , F01D17/148 , F01D25/24 , F02B33/40 , F02B39/16 , F05D2220/40 , F05D2240/128 , F05D2250/90
Abstract: A nozzle assembly of a turbocharger includes a nozzle and a ring-shaped body. The nozzle has flow passages extending through the nozzle and configured to direct air received from a volute housing of the turbocharger through the nozzle to turbine blades of the turbocharger. The ring-shaped body is coupled with the nozzle and is configured to rotate around the nozzle. The ring-shaped body includes blocking segments that block the flow of the air and openings between the blocking segments that permit the air to flow through the ring-shaped body. The ring-shaped body is configured to rotate relative to the nozzle to change how many of the flow passages in the nozzle are blocked by the blocking segments of the ring-shaped body.
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13.发明申请公开(公告)号：US20160281604A1
公开(公告)日：2016-09-29
申请号：US14671147
申请日：2015-03-27
Applicant: General Electric Company
Inventor： Sebastian Walter Freund
CPC classification number: F02C7/143 , F01K23/103 , F02C7/16 , F25B9/008 , F25B9/06 , Y02E20/16 , Y02P80/152
Abstract: An integrated heat recovery and cooling cycle system for use with a gas turbine engine, including a heat-to-power portion and an inlet cooling portion. The heat-to-power portion including a two-stage intercooled pump/compressor, a low-temperature heat source configured to receive a first portion of a flow of working fluid, one or more recuperators configured in parallel with the intercooler to receive a second portion of the flow of working fluid. The inlet cooling cycle including a chiller expander, a chiller compressor coupled to the chiller expander, a motor coupled to the chiller compressor and an inlet air heat exchanger in fluid communication with the chiller expander and the chiller compressor. The inlet cooling portion configured to receive a portion of the flow of working fluid. The system further including a working fluid condenser and an accumulator in fluid communication with the heat-to-power portion and the inlet cooling portion.
Abstract translation: 一种与燃气涡轮发动机一起使用的集成热回收和冷却循环系统，包括热功率部分和入口冷却部分。 热功率部分包括两级中间冷却泵/压缩机，构造成接收工作流体流的第一部分的低温热源，与中间冷却器并联构造的一个或多个回热器，以接收第二 部分工作流体流动。 入口冷却循环包括冷却器膨胀器，联接到冷却器膨胀器的冷却器压缩机，耦合到冷却器压缩机的电动机和与冷却器膨胀器和冷却器压缩机流体连通的入口空气热交换器。 入口冷却部分构造成接收工作流体流的一部分。 该系统还包括工作流体冷凝器和与热功率部分和入口冷却部分流体连通的蓄能器。
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公开(公告)号：US20180066548A1
公开(公告)日：2018-03-08
申请号：US15257917
申请日：2016-09-07
Applicant: General Electric Company
Inventor： Sebastian Walter Freund
CPC classification number: F01K23/10 , F01K7/16 , F02C6/18 , F02C7/10 , F05D2250/312 , F16T1/00 , Y02E20/16
Abstract: A combined cycle power plant is provided. The combined cycle power plant includes a gas turbine and a heat recovery steam generator disposed in fluid communication with the gas turbine and including one or more steam heater units. Additionally, the combined cycle power plant includes a recuperator unit integrated with the heat recovery steam generator and configured to use gas turbine exhaust from the gas turbine to preheat compressor discharge air from the compressor and supply the preheated compressor discharge air to the combustor, where a first subset of the one or more steam heater units is disposed in parallel to the recuperator unit, and where a second subset of the one or more steam heater units is disposed in series with the first subset of the one or more steam heater units and the recuperator unit with respect to a direction of flow of gas turbine exhaust.
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公开(公告)号：US09903284B1
公开(公告)日：2018-02-27
申请号：US15338941
申请日：2016-10-31
Applicant: General Electric Company
Inventor： Thomas Michael Lavertu , Roy James Primus , Venu Gummadavelli Gupta , Sebastian Walter Freund , Omowoleola Chukwuemeka Akinyemi , Adam Edgar Klingbeil , Victor Manuel Salazar
CPC classification number: F02D19/08 , F02D41/0027 , F02D41/005 , F02D41/38 , F02D2041/389 , F02M26/33 , F02M26/47
Abstract: Dual-fuel engine system includes cylinders in which the cylinders have an intake valve and an exhaust valve that control a flow of fluid into and out of a combustion chamber of the corresponding cylinder. The intake valve is configured to have an intake valve closure (IVC) timing. The dual-fuel engine system is configured to operate in a single-fuel mode and a dual-fuel mode. The combustion chamber and a piston are designed to provide a compression ratio. The dual-fuel engine system also includes one or more processors that are operably coupled to and configured to control operation of the first fuel injector. The compression ratio and the IVC timing are selected to achieve a target pre-combustion temperature. The target pre-combustion temperature permits the dual-fuel engine system to operate at a high substitution rate in the dual-fuel mode and at a sufficient fuel efficiency in the single-fuel mode.
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公开(公告)号：US20140117670A1
公开(公告)日：2014-05-01
申请号：US13660536
申请日：2012-10-25
Applicant: GENERAL ELECTRIC COMPANY
Inventor： Sebastian Walter Freund , Matthew Alexander Lehar , William Joseph Antel, Jr. , Pierre Sébastien Huck , Hannes Christopher Buck , Trevor James Kirsten , Kenneth William Kohl , Matthew Michael Lampo , Charles Michael Jones , Amit Gaikwad , Lars Olof Nord
IPC: F01D15/10
CPC classification number: F01K13/02 , F01K1/02 , F01K3/00 , F01K3/26 , F01K7/44 , F01K17/00 , F01K21/00 , F04B19/24 , F04F1/04
Abstract: A system and method for generating electric power using a generator coupled to a turboexpander is disclosed. The system includes one or more thermal pumps configured for heating a fluid to generate a pressurized gas. A portion of the pressurized gas is discharged to a buffer chamber for further utilization in a Rankine system. A further portion of the pressurized gas is expanded in a turboexpander for driving a generator for generating electric power. Optionally, the system includes a pump to pressurize a portion of the fluid depending on the systems operating condition. The system further includes one or more sensors for sensing temperature and pressure and outputs one or more signals representative of the sensed state. The system includes a control unit for receiving the signals and outputs one or more control signals for controlling the flow of gases and liquid in the valves and the check valve.
Abstract translation: 公开了一种使用耦合到涡轮膨胀机的发电机产生电力的系统和方法。 该系统包括被配置用于加热流体以产生加压气体的一个或多个热泵。 一部分加压气体被排放到缓冲室中以便在兰金系统中进一步利用。 加压气体的另一部分在涡轮膨胀机中膨胀，用于驱动用于发电的发电机。 可选地，系统包括泵，以根据系统运行状况对流体的一部分进行加压。 该系统还包括用于感测温度和压力的一个或多个传感器，并且输出表示感测状态的一个或多个信号。 该系统包括用于接收信号并输出一个或多个控制信号的控制单元，用于控制阀和止回阀中的气体和液体的流动。
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