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公开(公告)号:US20140208769A1
公开(公告)日:2014-07-31
申请号:US13755500
申请日:2013-01-31
Applicant: GENERAL ELECTRIC COMPANY
Inventor: Corey Bourassa , William Dwight Gerstler
CPC classification number: F02C7/185 , F01D5/189 , F05D2240/129 , F05D2250/185 , F05D2260/201 , F05D2260/213 , F28D7/0058 , F28D2021/0026 , F28F13/06 , F28F2250/02
Abstract: An integrated inducer heat exchanger is provided. The integrated inducer heat exchanger includes multiple airfoil devices disposed in an annular array within an inner circular casing and an outer circular casing forming multiple passages for allowing a flow of fluid from a forward side to an aft side of the integrated inducer heat exchanger. The integrated inducer heat exchanger also includes multiple annular manifolds arranged about the outer circular casing configured for supplying a flow of coolant at low temperature from one or more coolant sources and returning the flow of coolant at high temperature to the one or more coolant sources via an external heat exchanger for dissipating heat and multiple transfer tubes connecting the multiple annular manifolds with the multiple airfoil devices for transferring the flow of coolant within the airfoil devices for exchanging heat between the coolant and the fluid passing through the multiple passages.
Abstract translation: 提供了一种综合的导流器热交换器。 集成导流器热交换器包括多个设置在内圆形壳体内的环形阵列中的翼型装置和形成多个通道的外圆形壳体,用于允许流体从一体式导流换热器的前侧流向后侧。 集成导流器热交换器还包括围绕外部圆形壳体布置的多个环形歧管,其构造成用于在低温下从一个或多个冷却剂源供应冷却剂流,并将高温下的冷却剂流通过一个或多个冷却剂源经由 用于散热的外部热交换器和将多个环形歧管与多个翼型装置连接的多个传输管,用于传递在翼型装置内的冷却剂流,以在冷却剂和通过多个通道的流体之间进行热交换。
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公开(公告)号:US20240159471A1
公开(公告)日:2024-05-16
申请号:US18545391
申请日:2023-12-19
Applicant: General Electric Company
Inventor: William Dwight Gerstler , Daniel Jason Erno , Michael Thomas Kenworthy , Jeffrey Douglas Rambo , Nicolas Kristopher Sabo
CPC classification number: F28D7/1623 , F28F1/022
Abstract: A heat exchanger is provided that can include furcating unit cells coupled with each other. Each of the unit cells can be elongated along an axis and include a sidewall that defines annular ring openings on opposite ends of the unit cell along the axis. The sidewall also can define undulating annular rings between the annular ring openings and axially separated from each other along the axis. The sidewall can further define angled openings into the unit cell both above and below each of the undulating annular rings. At least a first opening of the annular ring openings and the angled openings can be configured to be an inlet to receive a first fluid into the unit cell and at least a second opening of the annular ring openings and the angled openings configured to be an outlet through which the first fluid exits the unit cell.
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公开(公告)号:US11982497B2
公开(公告)日:2024-05-14
申请号:US17569619
申请日:2022-01-06
Applicant: General Electric Company
Inventor: Brandon Wayne Miller , Nicholas Taylor Moore , Daniel Alan Niergarth , Jeffrey Douglas Rambo , Hendrik Pieter Jacobus de Bock , William Dwight Gerstler
CPC classification number: F28F1/003 , G01M3/3227 , F28F2250/06 , F28F2265/26
Abstract: A system for heat exchange and leak detection is generally provided, the system including a heat exchanger including a first wall defining a first passage containing a first fluid. A leak detection enclosure containing a leak detection medium is defined between the first wall and a second wall surrounding the first wall.
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公开(公告)号:US20220307419A1
公开(公告)日:2022-09-29
申请号:US17215130
申请日:2021-03-29
Applicant: General Electric Company
Inventor: Christopher Edward Wolfe , Hendrik Pieter Jacobus de Bock , William Dwight Gerstler , Brian Gene Brzek , Brandon Wayne Miller , Daniel Alan Niergarth , Kevin Robert Feldmann , Kevin Edward Hinderliter
Abstract: A thermal management system for transferring heat between fluids includes a thermal transport bus through which a heat exchange fluid flows. Additionally, the system includes a heat source heat exchanger arranged along the bus such that heat is added to the fluid flowing through the heat source heat exchanger. Moreover, the system includes a plurality of heat sink heat exchangers arranged along the bus such that heat is removed from the fluid flowing through the plurality of heat sink heat exchangers. Furthermore, the system includes a bypass conduit fluidly coupled to the bus such that the bypass conduit allows the fluid to bypass one of the heat source heat exchanger or one of the heat sink heat exchangers. In addition, the system includes a valve configured to control a flow of the fluid through the bypass conduit based on a pressure of the fluid within the bus.
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公开(公告)号:US11224098B2
公开(公告)日:2022-01-11
申请号:US16177996
申请日:2018-11-01
Applicant: General Electric Company
Abstract: A system configured for operation below a threshold temperature system includes a power supply, a housing, a temperature-sensitive electronic component, and a heating circuit. The temperature-sensitive electronic component is enclosed within said housing and electrically connected to the power supply, wherein the temperature-sensitive electronic component becomes susceptible to failure when the temperature of said temperature-sensitive electronic component decreases and crosses the threshold temperature. The heating circuit is at least partially enclosed within the housing and comprising a temperature-dependent resistor, the heating circuit electrically connected to the power supply and configured to generate heat energy within the housing when the temperature within the housing decreases and approaches the threshold temperature in order to maintain the temperature of the temperature-sensitive electronic component above the threshold temperature.
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公开(公告)号:US11146146B2
公开(公告)日:2021-10-12
申请号:US16190131
申请日:2018-11-13
Applicant: General Electric Company
Inventor: William Dwight Gerstler
Abstract: Embodiments of a heat exchanger for cooling endwindings in a rotary electric machine are provided herein. In some embodiments, a heat exchanger may include a body configured to be disposed proximate the rotor endwinding and coupled to a casing and end shield of the rotating electric machine. The body defines a cavity configured to capture a heated fluid expelled from the rotor endwinding. A channel, having a cooling fluid therein, is formed in the body and fluidly coupled to a heat sink. A rotating electric machine and method for cooling endwindings in a rotating electric machine are disclosed.
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67.
公开(公告)号:US10784750B2
公开(公告)日:2020-09-22
申请号:US16006094
申请日:2018-06-12
Applicant: General Electric Company
IPC: H02K9/20 , H02K5/20 , F04D29/58 , F01D25/26 , F01D25/12 , F01D9/02 , F01D1/04 , B64D27/24 , B64D27/02
Abstract: The present disclosure pertains to electric machines such as electric propulsion systems for aircraft that integrated cooling systems, and methods of cooling such an electric machine. Exemplary electric machines include an electric motor that has a stator, a rotor, and a drive shaft operably coupled to the rotor. Exemplary electric machines further include a motor cooling conduit that defines a pathway for conveying a cooling fluid through or around at least a portion of the electric motor, a casing assembly that circumferentially surrounds at least a portion of the electric motor, a casing assembly conduit integrally formed within at least a portion of the casing assembly which defines a pathway for conveying the cooling fluid through the at least a portion of the casing assembly, and a pump or compressor operably coupled to the drive shaft and configured to circulate the cooling fluid through the motor cooling conduit and the casing assembly conduit.
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公开(公告)号:US20200173291A1
公开(公告)日:2020-06-04
申请号:US16207995
申请日:2018-12-03
Applicant: General Electric Company
Abstract: A tip for a turbine component, turbine rotor blade or tip of a blade, is disclosed. The tip includes a tip plate configured to be coupled at a tip end of an airfoil chamber; and a tip rail extending radially from the tip plate, the tip rail disposed near or at a periphery of the tip plate. The trip rail includes a cooling structure constituting at least a portion of the tip rail. The cooling structure is in fluid communication with the airfoil chamber, and includes a plurality of repeating, three dimensional unit cells. Each unit cell defines a flow passage that is in fluid communication with the flow passage of at least one other unit cell. The flow passages of the 3D unit cells create a tortuous cooling passage in at least a portion of the tip rail.
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公开(公告)号:US20200153312A1
公开(公告)日:2020-05-14
申请号:US16190131
申请日:2018-11-13
Applicant: General Electric Company
Inventor: William Dwight Gerstler
IPC: H02K9/193
Abstract: Embodiments of a heat exchanger for cooling endwindings in a rotary electric machine are provided herein. In some embodiments, a heat exchanger may include a body configured to be disposed proximate the rotor endwinding and coupled to a casing and end shield of the rotating electric machine. The body defines a cavity configured to capture a heated fluid expelled from the rotor endwinding. A channel, having a cooling fluid therein, is formed in the body and fluidly coupled to a heat sink. A rotating electric machine and method for cooling endwindings in a rotating electric machine are disclosed.
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公开(公告)号:US20190186361A1
公开(公告)日:2019-06-20
申请号:US15843260
申请日:2017-12-15
Applicant: General Electric Company
Inventor: William Dwight Gerstler , Daniel Jason Erno , Brian Lewis Devendorf , Kevin Kenneth Pruzinsky
Abstract: A recuperator includes a monolithic heat exchanger core having a first side proximal to a combustor inlet and a turbine outlet, and a second side that includes an exhaust outlet. A compressed air inlet is located on the second side, and a compressed air outlet is located on the first side. The compressed air outlet supplies air to a combustor. A first plurality of passageways connects the compressed air inlet to the compressed air outlet. A turbine exhaust inlet is located on the first side, and a turbine exhaust outlet is located on the second side. A second plurality of passageways connects the turbine exhaust inlet to the turbine exhaust outlet. The first and second plurality of passageways are defined by parting plates that extend radially outward in a spiral pattern that maintains a substantially equal distance between adjacent parting plates.
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