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1.发明授权Aircraft electronics cooling apparatus for an aircraft having a liquid cooling system 有权具有液体冷却系统的飞机用飞机电子冷却装置公开(公告)号：US09167720B2
公开(公告)日：2015-10-20
申请号：US13846184
申请日：2013-03-18
发明人： Ozan Uluc , Ahmet Kayihan Kiryaman , Andreas Frey
IPC分类号： H05K7/20
CPC分类号： H05K7/20218 , H05K7/20645 , H05K7/20681
摘要： The invention relates to an improved aircraft electronics cooling system for an aircraft having a liquid cooling system, the aircraft electronics cooling system providing a thermal coupling between an electronic device to be cooled and the liquid cooling system of the aircraft. A coolant delivered by the liquid cooling system may flow through a board of the electronic device, through a heat sink on which the electronic device is arranged and/or through a housing in which the electronic device is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporize at least partially while cooling the electronic device.
摘要翻译： 本发明涉及一种用于具有液体冷却系统的飞行器的改进的飞行器电子冷却系统，飞行器电子冷却系统提供待冷却的电子设备与飞机的液体冷却系统之间的热耦合。 由液体冷却系统输送的冷却剂可以通过电子设备布置在其上的散热器和/或通过其中布置电子设备的壳体流过电子设备的板。 在冷却回路中冷却剂可能永久处于液态。 在冷却电子设备的同时，冷却剂至少部分地蒸发。
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公开(公告)号：US09719706B2
公开(公告)日：2017-08-01
申请号：US13773214
申请日：2013-02-21
CPC分类号： F25B40/02 , F25B23/006 , F25B2339/044 , F25B2400/053
摘要： An accumulator arrangement for use in a cooling system suitable for operation with two-phase refrigerant includes a condenser having a refrigerant inlet and a refrigerant outlet. The accumulator arrangement further includes an accumulator for receiving the two-phase refrigerant therein, the accumulator having a refrigerant inlet connected to the refrigerant outlet of the condenser and a refrigerant outlet. Finally, the accumulator arrangement includes a subcooler having a refrigerant inlet and a refrigerant outlet, the refrigerant inlet of the subcooler being connected to the refrigerant outlet of the accumulators, and the subcooler being arranged at least partially within the interior of the accumulator.
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公开(公告)号：US09726404B2
公开(公告)日：2017-08-08
申请号：US13773037
申请日：2013-02-21
CPC分类号： F25B40/02 , F25B23/006
摘要： A cooling system, in particular for use on board an aircraft, includes a cooling circuit allowing circulation of a two-phase refrigerant therethrough, an evaporator disposed in the cooling circuit, and a condenser disposed in the cooling circuit. A plurality of subcoolers is arranged in series in the cooling circuit downstream of the condenser.
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4.发明申请AIRCRAFT COMPRISING A COOLING SYSTEM FOR OPERATION WITH A TWO-PHASE REFRIGERANT 审中-公开包含用于使用两相制冷剂运行的冷却系统的飞机公开(公告)号：US20130340470A1
公开(公告)日：2013-12-26
申请号：US13922013
申请日：2013-06-19
CPC分类号： F25B49/005 , B64D13/06 , B64D2013/0674 , F25B39/02 , Y02T50/56
摘要： An aircraft includes a cooling system having a cooling circuit to circulate a two-phase refrigerant therethrough, an evaporator disposed in a first section of the cooling circuit and having a refrigerant inlet and outlet, a condenser disposed in a second section of the cooling circuit and having a refrigerant inlet and outlet, a first cooling circuit control valve disposed in the cooling circuit between the refrigerant outlet of the evaporator and the refrigerant inlet of the condenser, and a second cooling circuit control valve disposed in the cooling circuit between the refrigerant outlet of the condenser and the refrigerant inlet of the evaporator. The first and the second cooling circuit control valves in their closed state seal the first section of the cooling circuit from the second section of the cooling circuit. The second section of the cooling circuit is installed in an unpressurized region of the aircraft.
摘要翻译： 飞机包括具有冷却回路以使两相制冷剂循环的冷却系统，设置在冷却回路的第一部分中并具有制冷剂入口和出口的蒸发器，设置在冷却回路的第二部分中的冷凝器， 具有制冷剂入口和出口的第一冷却回路控制阀，设置在蒸发器的制冷剂出口与冷凝器的制冷剂入口之间的冷却回路中的第一冷却回路控制阀，以及设置在冷凝回路中的第二冷却回路控制阀， 冷凝器和蒸发器的制冷剂入口。 第一和第二冷却回路控制阀处于关闭状态，从冷却回路的第二部分密封冷却回路的第一部分。 冷却回路的第二部分安装在飞机的非加压区域。
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5.发明申请公开(公告)号：US20130319650A1
公开(公告)日：2013-12-05
申请号：US13893952
申请日：2013-05-14
IPC分类号： F28F27/00
CPC分类号： F28F27/00 , B64D11/04 , B64D13/06 , B64D2013/0614 , B64D2013/0629 , Y02T50/56
摘要： In a method for operating an aircraft cooling system a cooling medium is guided through a cooling circuit, which is connected to a refrigerating machine and to at least one cooling station associated with a cooling energy consumer, to supply cooling medium cooled by the refrigerating to the cooling station. A temperature of the cooling medium upstream of the cooling station and a temperature of the cooling medium downstream of the cooling station are detected. The mass flow of cooling medium supplied to the cooling station is controlled in dependence on a thermal output of the cooling energy consumer and in dependence on a difference between the temperature of the cooling medium upstream of the cooling station and the temperature of the cooling medium downstream of the cooling station.
摘要翻译： 在用于操作飞行器冷却系统的方法中，冷却介质被引导通过冷却回路，该冷却回路连接到制冷机和至少一个与冷却能量消耗器相关联的冷却站，以将冷却剂冷却的冷却介质供应到 冷却站。 检测冷却站上游的冷却介质的温度和冷却站下游的冷却介质的温度。 供给到冷却站的冷却介质的质量流量根据冷却能量消耗器的热输出和冷却站上游的冷却介质的温度与下游冷却介质的温度之间的差异来控制 的冷却站。
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公开(公告)号：US09903672B2
公开(公告)日：2018-02-27
申请号：US13893952
申请日：2013-05-14
CPC分类号： F28F27/00 , B64D11/04 , B64D13/06 , B64D2013/0614 , B64D2013/0629 , Y02T50/56
摘要： In a method for operating an aircraft cooling system a cooling medium is guided through a cooling circuit, which is connected to a refrigerating machine and to at least one cooling station associated with a cooling energy consumer, to supply cooling medium cooled by the refrigerating to the cooling station. A temperature of the cooling medium upstream of the cooling station and a temperature of the cooling medium downstream of the cooling station are detected. The mass flow of cooling medium supplied to the cooling station is controlled in dependence on a thermal output of the cooling energy consumer and in dependence on a difference between the temperature of the cooling medium upstream of the cooling station and the temperature of the cooling medium downstream of the cooling station.
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公开(公告)号：US20130227975A1
公开(公告)日：2013-09-05
申请号：US13773037
申请日：2013-02-21
IPC分类号： F25B40/02
CPC分类号： F25B40/02 , F25B23/006
摘要： A cooling system, in particular for use on board an aircraft, includes a cooling circuit allowing circulation of a two-phase refrigerant therethrough, an evaporator disposed in the cooling circuit, and a condenser disposed in the cooling circuit. A plurality of subcoolers is arranged in series in the cooling circuit downstream of the condenser.
摘要翻译： 特别是在飞机上使用的冷却系统包括允许两相制冷剂循环的冷却回路，设置在冷却回路中的蒸发器和设置在冷却回路中的冷凝器。 在冷凝器下游的冷却回路中串联布置多个过冷却器。
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公开(公告)号：US20130233003A1
公开(公告)日：2013-09-12
申请号：US13774480
申请日：2013-02-22
CPC分类号： B64D13/06 , F25B7/00 , F25B23/006 , F25B25/005 , F25B49/02 , F25B2400/06
摘要： A cooling system, in particular for use on board an aircraft, includes a first cooling circuit allowing circulation of a two-phase refrigerant therethrough, a first evaporator disposed in the first cooling circuit, a first condenser disposed in the first cooling circuit, and a first heat sink adapted to provide cooling energy to the first condenser. The cooling system further includes a second cooling circuit allowing circulation of a two-phase refrigerant therethrough, a second evaporator disposed in the second cooling circuit, a second condenser disposed in the second cooling circuit, a second heat sink adapted to provide cooling energy to the second condenser, and a cooling energy transfer arrangement which is adapted to transfer cooling energy provided by the first heat sink and/or the first condenser to the second cooling circuit or to transfer cooling energy provided by the second heat sink and/or the second condenser to the first cooling circuit.
摘要翻译： 特别是在飞机上使用的冷却系统包括允许两相制冷剂循环通过的第一冷却回路，设置在第一冷却回路中的第一蒸发器，设置在第一冷却回路中的第一冷凝器和 第一散热器，其适于向第一冷凝器提供冷却能量。 冷却系统还包括允许二相制冷剂循环通过的第二冷却回路，设置在第二冷却回路中的第二蒸发器，设置在第二冷却回路中的第二冷凝器，适于向第二冷却回路提供冷却能量的第二散热器 第二冷凝器和冷却能量传递装置，其适于将由第一散热器和/或第一冷凝器提供的冷却能量传递到第二冷却回路或传递由第二散热器和/或第二冷凝器提供的冷却能量 到第一个冷却回路。
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