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公开(公告)号：US09300190B2
公开(公告)日：2016-03-29
申请号：US13279230
申请日：2011-10-21
摘要： A free-surface liquid transfer apparatus for rotating machinery includes a stationary member. The stationary member includes a main surface configured to align to a rotating member, a landing surface arranged around the main surface configured to receive and slow a continuous film of working fluid transferred from the rotating member, an annular gap arranged around the landing surface, and a hollow torus cavity arranged proximate the annular gap configured to receive the slowed continuous film of working fluid transmitted through the annular gap.
摘要翻译： 用于旋转机械的自由表面液体输送装置包括固定构件。 固定构件包括构造成与旋转构件对准的主表面，围绕主表面布置的着陆表面，构造成接收和减缓从旋转构件转移的工作流体的连续膜，围绕着落表面布置的环形间隙， 靠近所述环形间隙设置的空心圆环腔，其构造成接收通过所述环形间隙传输的工作流体的减速的连续薄膜。
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公开(公告)号：US20130098585A1
公开(公告)日：2013-04-25
申请号：US13279230
申请日：2011-10-21
IPC分类号： F28D15/00
摘要： A free-surface liquid transfer apparatus for rotating machinery includes a stationary member. The stationary member includes a main surface configured to align to a rotating member, a landing surface arranged around the main surface configured to receive and slow a continuous film of working fluid transferred from the rotating member, an annular gap arranged around the landing surface, and a hollow torus cavity arranged proximate the annular gap configured to receive the slowed continuous film of working fluid transmitted through the annular gap.
摘要翻译： 用于旋转机械的自由表面液体输送装置包括固定构件。 固定构件包括构造成与旋转构件对准的主表面，围绕主表面布置的着陆表面，构造成接收和减缓从旋转构件转移的工作流体的连续膜，围绕着落表面布置的环形间隙， 靠近所述环形间隙设置的空心圆环腔，其构造成接收通过所述环形间隙传输的工作流体的减速的连续薄膜。
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公开(公告)号：US20110219786A1
公开(公告)日：2011-09-15
申请号：US12721598
申请日：2010-03-11
CPC分类号： B64D13/08 , B64D13/06 , B64D2013/0674
摘要： An aircraft cooling system includes a refrigerant cycle including a first heat exchanger, a second heat exchanger, and a compressor. A component of the aircraft is in thermal communication with the first heat exchanger. A heat sink fluid passes through the second heat exchanger to absorb heat from the refrigerant cycle. A hydraulic motor is mechanically connected with the compressor and powered by the heat sink fluid, which is circulated by a pump.
摘要翻译： 飞机冷却系统包括包括第一热交换器，第二热交换器和压缩机的制冷剂循环。 飞机的部件与第一热交换器热连通。 散热器流体通过第二热交换器以吸收来自制冷剂循环的热量。 液压马达与压缩机机械连接，并由通过泵循环的散热器流体驱动。
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公开(公告)号：US20140342201A1
公开(公告)日：2014-11-20
申请号：US13896529
申请日：2013-05-17
申请人： Michael J. Andres
发明人： Michael J. Andres
IPC分类号： H01M10/66 , H01M10/6567 , H01M10/613
CPC分类号： H01M10/613 , H01G2/08 , H01G11/18 , H01G11/78 , H01M2/1077 , H01M2/1241 , H01M10/625 , H01M10/63 , H01M10/643 , H01M10/6551 , H01M10/6554 , H01M10/6567 , H01M10/6569 , H01M10/658 , H01M2220/20 , Y02E60/13
摘要： A thermal management system for a high density power source is disclosed. The system includes a housing with an interior divided into first and second compartments. The first compartment is configured and adapted to house at least one electrical battery and the second compartment defines a coolant reservoir. A fluid release member connects the first and second compartments. Upon the first compartment reaching a temperature in excess of a predetermined limit, the fluid release member releases coolant form the second compartment into the first compartment to cool the at least one battery within the first compartment.
摘要翻译： 公开了一种用于高密度电源的热管理系统。 该系统包括具有被分成第一和第二隔室的内部的壳体。 第一隔室被配置和适于容纳至少一个电池，而第二隔室限定冷却剂储存器。 流体释放构件连接第一和第二隔室。 当第一隔室达到超过预定极限的温度时，流体释放构件将冷却剂从第二隔室释放到第一隔室中，以冷却第一隔间内的至少一个电池。
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公开(公告)号：US07987683B2
公开(公告)日：2011-08-02
申请号：US11358791
申请日：2006-02-20
申请人： Michael J. Andres
发明人： Michael J. Andres
IPC分类号： F25D9/00
CPC分类号： F25B27/00 , B64D13/06 , B64D2013/0674 , F25B1/00 , F25B9/004 , F25B2341/0661 , F25B2400/0751
摘要： A cooling system with a compression cooling cycle for a working fluid that passes an expendable fluid through a warm side heat exchanger for the cooling system to cause the expendable fluid to vaporise and thus absorb heat from the working fluid by way of latent heat or enthalpy of vaporisation and then running the vaporised expendable through a turbine that drives a compressor for the cooling system.
摘要翻译： 一种具有用于工作流体的压缩冷却循环的冷却系统，该工作流体将消耗性流体通过用于冷却系统的暖侧热交换器，以使得消耗性流体蒸发并因此通过潜热或焓的方式从工作流体吸收热量 蒸发，然后通过驱动冷却系统的压缩机的涡轮运行蒸发的消耗品。
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公开(公告)号：US10266034B2
公开(公告)日：2019-04-23
申请号：US13162152
申请日：2011-06-16
申请人： Michael J. Andres
发明人： Michael J. Andres
摘要： A system for providing heating and cooling to an aircraft has a single compressor for compressing and heating a fluid, a first zone and a second zone. The first zone has a first expansion valve without a condenser and a first heat exchanger removing heat from or adding heat to the first zone. The compressed fluid passes through the first zone and the first expansion valve. The second zone requires cooling and has a second expansion valve without a condenser and a second heat exchanger for removing heat from the zone. The compressed fluid passes through the second expansion valve after going through the first expansion valve and before passing through the second heat exchanger.
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公开(公告)号：US20130055724A1
公开(公告)日：2013-03-07
申请号：US13223578
申请日：2011-09-01
申请人： Adam M. Finney , Michael J. Andres
发明人： Adam M. Finney , Michael J. Andres
IPC分类号： F02C6/08
CPC分类号： F01D25/12 , F02C3/365 , F05D2220/74 , F05D2260/213
摘要： An air cycle system for a gas turbine engine includes a compressor, a turbine and a heat exchanger fluidly connected between the compressor and the turbine. A fluid source communicates a fluid through the heat exchanger. The heat exchanger exchanges heat between the fluid and an airflow communicated through the heat exchanger from the compressor to provide a conditioned airflow.
摘要翻译： 用于燃气涡轮发动机的空气循环系统包括压缩机，涡轮机和流体连接在压缩机和涡轮机之间的热交换器。 流体源通过热交换器连通流体。 热交换器在流体与通过热交换器从压缩机传递的气流之间交换热量，以提供经调节的气流。
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公开(公告)号：US07466045B2
公开(公告)日：2008-12-16
申请号：US11364906
申请日：2006-02-14
申请人： Michael J. Andres
发明人： Michael J. Andres
IPC分类号： H02K9/00
CPC分类号： H02K55/04 , H02K55/00 , Y02E40/62 , Y02E40/625
摘要： An in-shaft cryogenic cooler mounts entirely within the shaft of a dynamoelectric machine that has a rotor comprising a high temperature superconductor.
摘要翻译： 轴内低温冷却器完全安装在具有包括高温超导体的转子的电动机的轴内。
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公开(公告)号：US09912021B2
公开(公告)日：2018-03-06
申请号：US13896529
申请日：2013-05-17
申请人： Michael J. Andres
发明人： Michael J. Andres
IPC分类号： H01M10/50 , H01M10/66 , H01G2/08 , H01M10/6551 , H01M10/6567 , H01M10/613 , H01M10/658 , H01G11/18 , H01G11/78 , H01M2/10 , H01M10/63 , H01M10/6569 , H01M10/6554 , H01M2/12 , H01M10/625 , H01M10/643
CPC分类号： H01M10/613 , H01G2/08 , H01G11/18 , H01G11/78 , H01M2/1077 , H01M2/1241 , H01M10/625 , H01M10/63 , H01M10/643 , H01M10/6551 , H01M10/6554 , H01M10/6567 , H01M10/6569 , H01M10/658 , H01M2220/20 , Y02E60/13
摘要： A thermal management system for a high density power source is disclosed. The system includes a housing with an interior divided into first and second compartments. The first compartment is configured and adapted to house at least one electrical battery and the second compartment defines a coolant reservoir. A fluid release member connects the first and second compartments. Upon the first compartment reaching a temperature in excess of a predetermined limit, the fluid release member releases coolant form the second compartment into the first compartment to cool the at least one battery within the first compartment.
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公开(公告)号：US20120322354A1
公开(公告)日：2012-12-20
申请号：US13162152
申请日：2011-06-16
申请人： Michael J. Andres
发明人： Michael J. Andres
IPC分类号： B60H1/00
CPC分类号： B60H1/00907 , B60H1/143 , B60H2001/00949 , B64D13/06 , B64D2013/0614 , B64D2013/0674 , F25B5/02 , F25B41/04
摘要： A system for providing heating and cooling to an aircraft has a single compressor for compressing and heating a fluid, a first zone and a second zone. The first zone has a first expansion valve without a condenser and a first heat exchanger removing heat from or adding heat to the first zone. The compressed fluid passes through the first zone and the first expansion valve. The second zone requires cooling and has a second expansion valve without a condenser and a second heat exchanger for removing heat from the zone. The compressed fluid passes through the second expansion valve after going through the first expansion valve and before passing through the second heat exchanger.
摘要翻译： 用于向飞行器提供加热和冷却的系统具有用于压缩和加热流体，第一区域和第二区域的单个压缩机。 第一区域具有没有冷凝器的第一膨胀阀和从第一区域除热或加热的第一热交换器。 压缩流体通过第一区域和第一膨胀阀。 第二区域需要冷却并且具有没有冷凝器的第二膨胀阀和用于从区域去除热量的第二热交换器。 压缩流体在经过第一膨胀阀并通过第二热交换器之前通过第二膨胀阀。
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