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公开(公告)号:US08770269B2
公开(公告)日:2014-07-08
申请号:US12813963
申请日:2010-06-11
Applicant: David Russell Scott
Inventor: David Russell Scott
CPC classification number: F01D25/12 , F01M5/002 , F16N39/02 , F28D1/0233 , F28F3/022 , F28F2215/00 , Y02T50/675
Abstract: A surface cooler is provided and includes an oil layer, through which oil flows, a separating plate disposed in heat transfer communication with the oil and fins extending into an air flow pathway and being disposed in heat transfer communication with the separating plate, the fins being arranged with varied configurations at each of two or more sections sequentially defined along a predominant direction of air flow along the air flow pathway.
Abstract translation: 提供了表面冷却器,其包括油层,油层通过该油层分离,该分离板设置成与油的传热连通,翅片延伸到空气流动通道中并且与分隔板传热连通地设置,翅片是 沿着沿着空气流动路径的空气流的主要方向顺序地限定的两个或更多个部分中的每一个排列有不同的构造。
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公开(公告)号:US20130048261A1
公开(公告)日:2013-02-28
申请号:US13219246
申请日:2011-08-26
Applicant: David Russell Scott , Berwyn Owain Pollard
Inventor: David Russell Scott , Berwyn Owain Pollard
IPC: F28F7/00
CPC classification number: F28D9/0043 , F28F3/086
Abstract: A heat exchanger is provided through which first and second fluids flow in a heat transfer arrangement. The heat exchanger includes a plurality of laminates. Each laminate includes a plurality of primary heat transfer surfaces disposed to contact the first and second fluids and a plurality of secondary heat transfer surfaces disposed to contact the first and/or second fluid. The respective pluralities of the primary and secondary heat transfer surfaces are configured to form respective pluralities of first and second flow pathways along which the first and second fluids flow, respectively, in the heat transfer arrangement. At least one of the plurality of the primary heat transfer surfaces is corrugated along a length of at least one of the plurality of the first flow pathways.
Abstract translation: 提供了热交换器,第一和第二流体通过该换热器在热传递装置中流动。 热交换器包括多个层压板。 每个层压板包括设置成接触第一和第二流体的多个主要传热表面和设置成接触第一和/或第二流体的多个次级传热表面。 相应的多个主传热表面和次传热表面被配置成形成相应的多个第一和第二流动通道,第一和第二流体沿着该第一和第二流动通道分别在传热装置中流动。 多个主要传热表面中的至少一个沿着多个第一流动路径中的至少一个的长度是波纹状的。
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公开(公告)号:US20110303405A1
公开(公告)日:2011-12-15
申请号:US12813963
申请日:2010-06-11
Applicant: David Russell Scott
Inventor: David Russell Scott
CPC classification number: F01D25/12 , F01M5/002 , F16N39/02 , F28D1/0233 , F28F3/022 , F28F2215/00 , Y02T50/675
Abstract: A surface cooler is provided and includes an oil layer, through which oil flows, a separating plate disposed in heat transfer communication with the oil and fins extending into an air flow pathway and being disposed in heat transfer communication with the separating plate, the fins being arranged with varied configurations at each of two or more sections sequentially defined along a predominant direction of air flow along the air flow pathway.
Abstract translation: 提供了表面冷却器,其包括油层,油层通过该油层分离,该分离板设置成与油的传热连通,翅片延伸到空气流动通道中并且与分隔板传热连通地设置,翅片是 沿着沿着空气流动路径的空气流的主要方向顺序地限定的两个或更多个部分中的每一个排列有不同的构造。
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公开(公告)号:US09417016B2
公开(公告)日:2016-08-16
申请号:US12985064
申请日:2011-01-05
Applicant: David Russell Scott
Inventor: David Russell Scott
CPC classification number: F28F3/02 , F28D9/005 , F28D9/0056 , F28D9/0075 , F28F3/022
Abstract: A laminated heat exchanger includes at least one heat exchange layer that includes a plurality of side members that define a frame having an interior portion. A plurality of heat exchange members extend between at least two of the plurality of side members across the interior portion. The plurality of heat exchange members are linked by a ligament member to form a heat exchange member chain.
Abstract translation: 层压热交换器包括至少一个热交换层,其包括限定具有内部部分的框架的多个侧部构件。 多个热交换构件在所述多个侧构件的至少两个之间穿过所述内部部分延伸。 多个热交换构件通过韧带构件连接以形成热交换构件链。
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公开(公告)号:US20130186100A1
公开(公告)日:2013-07-25
申请号:US13354689
申请日:2012-01-20
Applicant: William E. Rhoden , Peter L. Jalbert , Rudolph Thomas Beaupre , David Russell Scott
Inventor: William E. Rhoden , Peter L. Jalbert , Rudolph Thomas Beaupre , David Russell Scott
Abstract: A system for managing thermal transfer in an aircraft includes a fuel stabilization unit, a fuel-air heat exchanger, and a turbine. The fuel-air heat exchanger is located downstream from the fuel stabilization unit. The fuel-air heat exchanger places deoxygenized fuel in a heat exchange relationship with compressor bleed air to produce heated deoxygenized fuel and cooled bleed air. The turbine is operationally connected to the engine compressor and receives cooled bleed air from the fuel-air heat exchanger.
Abstract translation: 用于管理飞行器中的热转印的系统包括燃料稳定单元,燃料 - 空气热交换器和涡轮机。 燃料空气热交换器位于燃料稳定单元的下游。 燃料 - 空气热交换器将脱氧燃料与压缩机排气进行热交换,产生加热的脱氧燃料和冷却的排放空气。 涡轮机可操作地连接到发动机压缩机并接收来自燃料 - 空气热交换器的冷却的排出空气。
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公开(公告)号:US20120168112A1
公开(公告)日:2012-07-05
申请号:US12985064
申请日:2011-01-05
Applicant: David Russell Scott
Inventor: David Russell Scott
IPC: F28F7/00
CPC classification number: F28F3/02 , F28D9/005 , F28D9/0056 , F28D9/0075 , F28F3/022
Abstract: A laminated heat exchanger includes at least one heat exchange layer that includes a plurality of side members that define a frame having an interior portion. A plurality of heat exchange members extend between at least two of the plurality of side members across the interior portion. The plurality of heat exchange members are linked by a ligament member to form a heat exchange member chain.
Abstract translation: 层压热交换器包括至少一个热交换层,其包括限定具有内部部分的框架的多个侧部构件。 多个热交换构件在所述多个侧构件的至少两个之间穿过所述内部部分延伸。 多个热交换构件通过韧带构件连接以形成热交换构件链。
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公开(公告)号:US08544531B2
公开(公告)日:2013-10-01
申请号:US12813941
申请日:2010-06-11
Applicant: David Russell Scott , Berwyn Owain Pollard
Inventor: David Russell Scott , Berwyn Owain Pollard
CPC classification number: F28F3/022 , F01M5/002 , F28D2021/0049 , F28F3/02 , F28F2265/28
Abstract: A surface cooler is provided and includes an oil layer through which oil flows, fins extending into an air flow pathway and being disposed at a first side of the oil layer in heat transfer communication with the oil, an acoustic lining to reduce noise present in or transmitted by the air flow pathway, which is disposed at a second side of the oil layer opposite the first side and noise transfer tubes extending through the oil layer to transfer the noise present in or transmitted by the air flow pathway to the acoustic lining.
Abstract translation: 提供了一个表面冷却器,它包括一个油层流过的油层,延伸到空气流动通道中的翅片,并设置在油层的第一侧,与油的传热连通;声学衬里, 通过设置在与第一侧相对的油层的第二侧的空气流动通道传送,并且延伸穿过油层的噪声转移管,以将存在于或由空气流动通道传递的噪声传递到声学衬里。
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公开(公告)号:US20130048243A1
公开(公告)日:2013-02-28
申请号:US13219252
申请日:2011-08-26
Applicant: Berwyn Owain Pollard , David Russell Scott
Inventor: Berwyn Owain Pollard , David Russell Scott
IPC: F28F7/00
CPC classification number: B64D13/00 , F28D1/0246 , F28F3/086
Abstract: A heat exchanger apparatus is provided and is configured to be disposed within a first pathway along which a first fluid flows. The heat exchanger apparatus includes a component disposed in the first pathway and including heat transfer surfaces configured to define at least one or more second pathways along which a second fluid flows. The heat transfer surfaces are configured to form an exterior surface of the component and are disposed to contact the first and/or second fluids.
Abstract translation: 提供了一种热交换器装置,并且被配置成设置在第一流体沿其流动的第一通道内。 热交换器装置包括设置在第一路径中并包括配置成限定第二流体沿其流动的至少一个或多个第二路径的传热表面的部件。 传热表面被构造成形成部件的外表面并且设置成接触第一和/或第二流体。
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公开(公告)号:US20110303398A1
公开(公告)日:2011-12-15
申请号:US12813941
申请日:2010-06-11
Applicant: David Russell Scott , Berwyn Owain Pollard
Inventor: David Russell Scott , Berwyn Owain Pollard
IPC: F28F99/00
CPC classification number: F28F3/022 , F01M5/002 , F28D2021/0049 , F28F3/02 , F28F2265/28
Abstract: A surface cooler is provided and includes an oil layer through which oil flows, fins extending into an air flow pathway and being disposed at a first side of the oil layer in heat transfer communication with the oil, an acoustic lining to reduce noise present in or transmitted by the air flow pathway, which is disposed at a second side of the oil layer opposite the first side and noise transfer tubes extending through the oil layer to transfer the noise present in or transmitted by the air flow pathway to the acoustic lining.
Abstract translation: 提供了一个表面冷却器,它包括一个油层流过的油层,延伸到空气流动通道中的翅片,并设置在油层的第一侧,与油的传热连通;声学衬里, 通过设置在与第一侧相对的油层的第二侧的空气流动通道传送,并且延伸穿过油层的噪声转移管,以将存在于或由空气流动通道传递的噪声传递到声学衬里。
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公开(公告)号:US09580185B2
公开(公告)日:2017-02-28
申请号:US13354689
申请日:2012-01-20
Applicant: William E. Rhoden , Peter L. Jalbert , Rudolph Thomas Beaupre , David Russell Scott
Inventor: William E. Rhoden , Peter L. Jalbert , Rudolph Thomas Beaupre , David Russell Scott
Abstract: A system for managing thermal transfer in an aircraft includes a fuel stabilization unit, a fuel-air heat exchanger, and a turbine. The fuel-air heat exchanger is located downstream from the fuel stabilization unit. The fuel-air heat exchanger places deoxygenized fuel in a heat exchange relationship with compressor bleed air to produce heated deoxygenized fuel and cooled bleed air. The turbine is operationally connected to the engine compressor and receives cooled bleed air from the fuel-air heat exchanger.
Abstract translation: 用于管理飞行器中的热转印的系统包括燃料稳定单元,燃料 - 空气热交换器和涡轮机。 燃料空气热交换器位于燃料稳定单元的下游。 燃料 - 空气热交换器将脱氧燃料与压缩机排气进行热交换,产生加热的脱氧燃料和冷却的排放空气。 涡轮机可操作地连接到发动机压缩机并接收来自燃料 - 空气热交换器的冷却的排出空气。
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