利索-全球专利检索

  1. 登录
  2. 注册

搜索结果

20 条记录 (耗时 0.016 秒)

    HEAT PUMP FOR SUPPLEMENTAL HEAT
    2.
    发明申请
    HEAT PUMP FOR SUPPLEMENTAL HEAT 审中-公开
    热泵用于补充热量

    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。

    THERMAL SPREADER WITH PHASE CHANGE THERMAL CAPACITOR FOR ELECTRICAL COOLING
    3.
    发明申请
    THERMAL SPREADER WITH PHASE CHANGE THERMAL CAPACITOR FOR ELECTRICAL COOLING 审中-公开
    具有相变热电热器的热膨胀器用于电冷却

    公开(公告)号：US20120206880A1

    公开(公告)日：2012-08-16

    申请号：US13026727

    申请日：2011-02-14

    申请人： Michael J. Andres ,  Robert Scott Downing

    发明人： Michael J. Andres ,  Robert Scott Downing

    IPC分类号： H05K7/20

    CPC分类号： H01L23/4275 ,  H01L2924/0002 ,  H01L2924/00

    摘要： A cooling assembly comprises an electronic component, a thermal spreader, a cold plate, and a phase change thermal capacitor. The thermal spreader conducts heat freely between the electronic component, the phase change thermal capacitor, and the cold plate. The cold plate dissipates heat. The phase change thermal capacitor stores undissipated heat in a phase transition of a phase change material.

    摘要翻译： 冷却组件包括电子部件，散热器，冷板和相变热电容器。 散热器在电子部件，相变热电容器和冷板之间自由传导。 冷板散热。 相变热电容器在相变材料的相变中存储不散热。

    Enhanced EDU Energy Redistribution
    5.
    发明申请
    Enhanced EDU Energy Redistribution 审中-公开
    增强EDU能源再分配

    公开(公告)号：US20120013176A1

    公开(公告)日：2012-01-19

    申请号：US12835169

    申请日：2010-07-13

    申请人： Charles Shepard ,  Michael J. Andres

    发明人： Charles Shepard ,  Michael J. Andres

    IPC分类号： B60L1/00

    CPC分类号： B64C13/50 ,  H02J1/14 ,  H02J4/00

    摘要： An enhanced electrical distribution unit (EDU) of an aircraft includes power control circuitry disposed to communicate with a power source, a regenerative load control circuit in communication with the power control circuitry and disposed to communicate with a regenerative load, and a passive load control circuit in communication with the power control circuitry and the regenerative load control circuit, the passive load control circuit disposed to communicate with a passive load. The regenerative load control circuit and the passive load control circuit are disposed to arrange a conductive path between the regenerative load and the passive load in response to operation of the regenerative load.

    摘要翻译： 飞机的增强配电单元（EDU）包括设置为与电源通信的功率控制电路，与功率控制电路通信并被设置为与再生负载通信的再生负载控制电路，以及无源负载控制电路 与功率控制电路和再生负载控制电路通信，被动负载控制电路设置成与被动负载通信。 再生负载控制电路和无源负载控制电路被布置成响应于再生负载的操作而在再生负载和被动负载之间布置导电路径。

    Heat pump for supplemental heat
    6.
    发明授权
    Heat pump for supplemental heat 有权

    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

    IPC分类号： B60H1/00 ,  B60H1/14 ,  F25B5/02 ,  B64D13/06 ,  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.

    FLUID HEAT SINK POWERED VAPOR CYCLE SYSTEM
    7.
    发明申请
    FLUID HEAT SINK POWERED VAPOR CYCLE SYSTEM 审中-公开
    流体热泵动力蒸汽循环系统

    公开(公告)号：US20110219786A1

    公开(公告)日：2011-09-15

    申请号：US12721598

    申请日：2010-03-11

    申请人： Michael J. Andres ,  Kris H. Campbell

    发明人： Michael J. Andres ,  Kris H. Campbell

    IPC分类号： B64D13/08 ,  F25B27/00 ,  F25B23/00 ,  F25B41/00

    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。

    ELECTRICAL STORAGE DEVICE THERMAL MANAGEMENT SYSTEMS
    8.
    发明申请
    ELECTRICAL STORAGE DEVICE THERMAL MANAGEMENT SYSTEMS 有权
    电气存储设备热管理系统

    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。

    Expendable turbine driven compression cycle cooling system
    9.
    发明授权
    Expendable turbine driven compression cycle cooling system 有权
    消耗涡轮驱动压缩循环冷却系统

    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。

    GAS TURBINE ENGINE AIR CYCLE SYSTEM
    10.
    发明申请
    GAS TURBINE ENGINE AIR CYCLE SYSTEM 审中-公开
    气体涡轮发动机空气循环系统

    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。