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公开(公告)号：US10690422B2
公开(公告)日：2020-06-23
申请号：US16528966
申请日：2019-08-01
Applicant: General Electric Company , Unison Industries, LLC
Inventor： Michael Ralph Storage , Scott Richard Lawrence , Ronald Eugene Bruskotter , Walter Arthur Hundley, Jr. , Dennis Alan McQueen , Ronald Bruce Schofield
Abstract: A method and assembly for conveying heat from a heat exchanger having a housing defining a fluid pathway including at least one fluid passageway leading from an inlet port of the heat exchanger to an outlet port of the heat exchanger, the housing have a first side and a second side, opposite the first side where the housing includes at least one aperture extending through the housing from the first side to the second side and where the aperture is fluidly separate from the fluid pathway and heat from liquid flowing through the fluid pathway is transferred via at least one of conduction or convection to the housing.
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公开(公告)号：US20170191750A1
公开(公告)日：2017-07-06
申请号：US15392914
申请日：2016-12-28
Applicant: General Electric Company
Inventor： Ian Alexandre Araujo De Barros , Michael Ralph Storage , Paul Richmond , Paul R. Angel , David Stanley
CPC classification number: F25J1/0283 , F01D15/005 , F02C3/06 , F02C7/143 , F02C7/185 , F05D2220/32 , F05D2260/211 , F25J1/0012 , F25J1/0022 , F25J1/0236 , F25J1/0284 , F25J3/04127 , F25J3/04612 , F25J2240/80 , F28D7/0041 , F28D7/005 , F28D2021/0026 , F28F1/022 , F28F1/26 , F28F7/02 , F28F9/26 , F28F2215/00
Abstract: A method includes compressing an air flow to a first pressure, transferring heat from the air flow to a liquefaction fluid via an intercooler heat exchanger, compressing the air flow to a second pressure greater than the first pressure, combusting the air flow and a fuel to generate a combustion product flow, and driving a turbine with the combustion product flow. The turbine is configured to drive machinery of a liquefaction system. The liquefaction fluid includes at least one of a pre-cooling fluid, a refrigerant, and a liquefied product of the liquefaction system.
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3.发明申请METHOD AND APPARATUS FOR DECONGEALING A LUBRICATING FLUID IN A HEAT EXCHANGER APPARATUS 有权用于在热交换器装置中分解润滑油的方法和装置公开(公告)号：US20160090863A1
公开(公告)日：2016-03-31
申请号：US14502750
申请日：2014-09-30
Applicant: General Electric Company
Inventor： Carlos Enrique Diaz , William Dwight Gerstler , Michael Ralph Storage
CPC classification number: F01D25/18 , F02C7/00 , F28D20/003
Abstract: A decongealing channel for use in a heat exchanger apparatus, including a supersaturated solution contained therein and an actuation component in fluid communication with a lubricating fluid coupled to the decongealing channel. The actuation component is responsive to a change in pressure exerted thereon by the lubricating fluid so as to actuate an exothermic response in the supersaturated solution. The heat exchanger apparatus is disposed in a bypass fan duct of an aircraft engine. The heat exchanger apparatus including a manifold portion, one or more flow through openings extending therethrough the manifold portion to define one or more flow through channels having contained therein the lubricating fluid. In addition, the manifold portion including one or more additional openings extending therethrough to define one or more decongealing channels. Further disclosed is an engine including the heat exchanger apparatus and a method of decongealing a lubricating fluid in the heat exchanger apparatus.
Abstract translation: 一种在热交换器装置中使用的去饱和通道，包括其中所含的过饱和溶液和与连接到去饱和通道的润滑流体流体连通的致动部件。 致动部件响应于润滑流体施加在其上的压力变化，以便致动过饱和溶液中的放热响应。 热交换器装置设置在飞机发动机的旁路风扇管道中。 所述热交换器装置包括歧管部分，一个或多个流过所述歧管部分的流过开口以限定一个或多个通过其中包含润滑流体的通道。 此外，歧管部分包括一个或多个延伸穿过其中的附加开口，以限定一个或多个去饱和通道。 还公开了一种发动机，其包括热交换器装置和在热交换器装置中使润滑流体退热的方法。
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公开(公告)号：US20150083367A1
公开(公告)日：2015-03-26
申请号：US14143233
申请日：2013-12-30
Applicant: General Electric Company
Inventor： Carlos Enrique Diaz , William Dwight Gerstler , Michael Ralph Storage
CPC classification number: F16K31/002 , F01D25/125 , F02C7/18 , F02K3/115 , F03G7/065 , F05D2260/606 , F05D2300/505 , F28F27/02 , Y02T50/671 , Y02T50/675
Abstract: An aviation bypass valve for use in a heat exchanger apparatus, including a shape memory alloy material. The heat exchanger apparatus further including an air-cooled oil cooler disposed in a bypass fan duct of an aircraft engine. The heat exchanger apparatus including a bypass valve in fluid communication with the air cooled oil cooler. The bypass valve including a valve body, a piston disposed in the valve body and moveable therein and an actuation component. The actuation component including a shape memory alloy. The actuation component responsive to a change in at least one of a thermal condition and a pressure exerted thereon so as to move the piston, thereby opening and closing the bypass valve.
Abstract translation: 一种用于热交换器装置的航空旁通阀，包括形状记忆合金材料。 该热交换器装置还包括设置在飞机发动机的旁通风扇导管中的空气冷却油冷却器。 该热交换器装置包括与空气冷却油冷却器流体连通的旁通阀。 旁通阀包括阀体，设置在阀体中并可在其中移动的活塞和致动部件。 致动部件包括形状记忆合金。 致动部件响应于热条件和施加在其上的压力中的至少一个的变化，以便移动活塞，从而打开和关闭旁通阀。
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Patent Agency Ranking
公开(公告)号：US20200041219A1
公开(公告)日：2020-02-06
申请号：US16528966
申请日：2019-08-01
Applicant: General Electric Company , Unison Industries, LLC
Inventor： Michael Ralph Storage , Scott Richard Lawrence , Ronald Eugene Bruskotter , Walter Arthur Hundley, JR. , Dennis Alan McQueen , Ronald Bruce Schofield
Abstract: A method and assembly for conveying heat from a heat exchanger having a housing defining a fluid pathway including at least one fluid passageway leading from an inlet port of the heat exchanger to an outlet port of the heat exchanger, the housing have a first side and a second side, opposite the first side where the housing includes at least one aperture extending through the housing from the first side to the second side and where the aperture is fluidly separate from the fluid pathway and heat from liquid flowing through the fluid pathway is transferred via at least one of conduction or convection to the housing.
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公开(公告)号：US09903274B2
公开(公告)日：2018-02-27
申请号：US14535614
申请日：2014-11-07
Applicant: General Electric Company
Inventor： Carlos Enrique Diaz , William Dwight Gerstler , Michael Ralph Storage , Michael Thomas Kenworthy
IPC: F02C1/00 , F02C7/14 , B64D33/12 , F02C7/18 , F28F27/02 , F28D1/047 , F28D7/08 , F02K3/02 , F28F13/00 , F02K3/06 , F28F1/12 , F28D21/00
CPC classification number: F02C7/14 , B64D33/12 , F02C7/18 , F02K3/025 , F02K3/06 , F05D2250/90 , F05D2300/505 , F28D1/047 , F28D7/08 , F28D2021/0021 , F28D2021/0026 , F28F1/12 , F28F13/00 , F28F27/02 , F28F2255/04 , F28F2280/10 , Y02T50/675
Abstract: A heat exchanger apparatus including a surface cooler and a passive automatic retraction and extension system coupled to the surface cooler. The surface cooler having disposed therein one or more fluid flow channels configured for the passage therethrough of a heat transfer fluid to be cooled. The heat transfer fluid in a heat transfer relation on an interior side of said one or more fluid flow channels. The surface cooler including a plurality of fins projecting from an outer surface thereof. The passive automatic retraction and extension system including a thermal actuation component responsive to a change in temperature of at least one of the heat transfer fluid and a cooling fluid flow so as to actuate a change in a geometry of the surface cooler. Further disclosed is an engine including the heat exchanger apparatus.
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公开(公告)号：US09890868B2
公开(公告)日：2018-02-13
申请号：US14143233
申请日：2013-12-30
Applicant: General Electric Company
Inventor： Carlos Enrique Diaz , William Dwight Gerstler , Michael Ralph Storage
CPC classification number: F16K31/002 , F01D25/125 , F02C7/18 , F02K3/115 , F03G7/065 , F05D2260/606 , F05D2300/505 , F28F27/02 , Y02T50/671 , Y02T50/675
Abstract: An aviation bypass valve for use in a heat exchanger apparatus, including a shape memory alloy material. The heat exchanger apparatus further including an air-cooled oil cooler disposed in a bypass fan duct of an aircraft engine. The heat exchanger apparatus including a bypass valve in fluid communication with the air cooled oil cooler. The bypass valve including a valve body, a piston disposed in the valve body and moveable therein and an actuation component. The actuation component including a shape memory alloy. The actuation component responsive to a change in at least one of a thermal condition and a pressure exerted thereon so as to move the piston, thereby opening and closing the bypass valve.
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8.发明授权Method and apparatus for decongealing a lubricating fluid in a heat exchanger apparatus 有权在热交换器装置中使润滑流体脱水的方法和装置公开(公告)号：US09593594B2
公开(公告)日：2017-03-14
申请号：US14502750
申请日：2014-09-30
Applicant: General Electric Company
Inventor： Carlos Enrique Diaz , William Dwight Gerstler , Michael Ralph Storage
CPC classification number: F01D25/18 , F02C7/00 , F28D20/003
Abstract: A decongealing channel for use in a heat exchanger apparatus, including a supersaturated solution contained therein and an actuation component in fluid communication with a lubricating fluid coupled to the decongealing channel. The actuation component is responsive to a change in pressure exerted thereon by the lubricating fluid so as to actuate an exothermic response in the supersaturated solution. The heat exchanger apparatus is disposed in a bypass fan duct of an aircraft engine. The heat exchanger apparatus including a manifold portion, one or more flow through openings extending therethrough the manifold portion to define one or more flow through channels having contained therein the lubricating fluid. In addition, the manifold portion including one or more additional openings extending therethrough to define one or more decongealing channels. Further disclosed is an engine including the heat exchanger apparatus and a method of decongealing a lubricating fluid in the heat exchanger apparatus.
Abstract translation: 一种在热交换器装置中使用的去饱和通道，包括其中所含的过饱和溶液和与连接到去饱和通道的润滑流体流体连通的致动部件。 致动部件响应于润滑流体施加在其上的压力变化，以便致动过饱和溶液中的放热响应。 热交换器装置设置在飞机发动机的旁路风扇管道中。 所述热交换器装置包括歧管部分，一个或多个流过所述歧管部分的流过开口以限定一个或多个通过其中包含润滑流体的通道。 此外，歧管部分包括一个或多个延伸穿过其中的附加开口，以限定一个或多个去饱和通道。 还公开了一种发动机，其包括热交换器装置和在热交换器装置中使润滑流体退热的方法。
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公开(公告)号：US20160131035A1
公开(公告)日：2016-05-12
申请号：US14535614
申请日：2014-11-07
Applicant: General Electric Company
Inventor： Carlos Enrique Diaz , William Dwight Gerstler , Michael Ralph Storage , Michael Thomas Kenworthy
CPC classification number: F02C7/14 , B64D33/12 , F02C7/18 , F02K3/025 , F02K3/06 , F05D2250/90 , F05D2300/505 , F28D1/047 , F28D7/08 , F28D2021/0021 , F28D2021/0026 , F28F1/12 , F28F13/00 , F28F27/02 , F28F2255/04 , F28F2280/10 , Y02T50/675
Abstract: A heat exchanger apparatus including a surface cooler and a passive automatic retraction and extension system coupled to the surface cooler. The surface cooler having disposed therein one or more fluid flow channels configured for the passage therethrough of a heat transfer fluid to be cooled. The heat transfer fluid in a heat transfer relation on an interior side of said one or more fluid flow channels. The surface cooler including a plurality of fins projecting from an outer surface thereof. The passive automatic retraction and extension system including a thermal actuation component responsive to a change in temperature of at least one of the heat transfer fluid and a cooling fluid flow so as to actuate a change in a geometry of the surface cooler. Further disclosed is an engine including the heat exchanger apparatus.
Abstract translation: 一种包括表面冷却器和耦合到表面冷却器的被动自动缩回和延伸系统的热交换器装置。 所述表面冷却器在其中设置有一个或多个流体流动通道，所述流体流动通道构造成用于通过其中待冷却的传热流体。 在所述一个或多个流体流动通道的内侧上的传热关系的传热流体。 所述表面冷却器包括从其外表面突出的多个翅片。 被动自动缩回和延伸系统包括响应于至少一个传热流体和冷却流体流的温度变化的热致动部件，以致致动表面冷却器几何形状的变化。 还公开了一种包括热交换器装置的发动机。
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