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11. 发明授权

US07920382B2 Aircraft electronics cooling apparatus for an aircraft having a liquid cooling system 有权
标题翻译：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：US07920382B2
公开(公告)日：2011-04-05
申请号：US12708647
申请日：2010-02-19
申请人： Ozan Uluc , Ahmet Kayihan Kiryaman , Andreas Frey
发明人： Ozan Uluc , Ahmet Kayihan Kiryaman , Andreas Frey
IPC分类号： H05K7/20 , F28F7/00 , F28F27/00 , B64D47/00
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 (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) 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（2）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电子设备（40a，40b，40c，40d，42,44）之间的热耦合，以使其成为冷却和飞机的液体冷却系统（2）。由液体冷却系统（2）输送的冷却剂可以通过电子设备（42）布置的散热器流过电子设备（40a，40b，40c，40d）的板，和/或通过壳体其中布置有电子设备（44）。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。

12. 发明授权

US08315053B2 Aircraft electronics cooling apparatus for an aircraft having a liquid cooling system 有权
标题翻译：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：US08315053B2
公开(公告)日：2012-11-20
申请号：US13036822
申请日：2011-02-28
申请人： Ozan Uluc , Ahmet Kayihan Kiryaman , Andreas Frey
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 (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) 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（2）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电子设备（40a，40b，40c，40d，42,44）之间的热耦合，以使其成为冷却和飞机的液体冷却系统（2）。由液体冷却系统（2）输送的冷却剂可以通过电子设备（42）布置的散热器流过电子设备（40a，40b，40c，40d）的板，和/或通过壳体其中布置有电子设备（44）。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。

13. 发明申请

US20110216505A1 Aircraft Electronics Cooling Apparatus For An Aircraft Having A Liquid Cooling System 审中-公开
公开(公告)号：US20110216505A1
公开(公告)日：2011-09-08
申请号：US13036801
申请日：2011-02-28
申请人： Ozan Uluc , Ahmet Kayihan Kiryaman , Andreas Frey
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 (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) 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.

14. 发明申请

US20080055852A1 Aircraft Electronics Cooling Apparatus For An Aircraft Having A Liquid Cooling System 失效
标题翻译：具有液体冷却系统的飞机的飞机电子冷却装置
公开(公告)号：US20080055852A1
公开(公告)日：2008-03-06
申请号：US11850712
申请日：2007-09-06
申请人： Ozan Uluc , Ahmet Kayihan Kiryaman , Andreas Frey
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 (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) is arranged. The coolant may be permanently in the liquid state in a cooling circuit. The coolant may vaporise 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（2）的飞行器的改进的飞行器电子冷却系统，所述飞行器电子冷却系统提供电子设备（40a，40b，40c，40d， 44）和飞机的液体冷却系统（2）。由液体冷却系统（2）输送的冷却剂可以通过其上布置有电子设备（42）的散热器流过电子设备（40a，40b，40c，40d）的板，和/ 或通过其中布置有电子设备（44）的壳体。在冷却回路中冷却剂可能永久处于液态。冷却剂可以在冷却电子设备的同时至少部分地蒸发。

15. 发明授权

US08336329B2 Cooling system and freight container 有权
标题翻译：冷却系统和货柜
公开(公告)号：US08336329B2
公开(公告)日：2012-12-25
申请号：US12532278
申请日：2008-03-25
申请人： Ozan Uluc , Andreas Frey , Sven Reisbach , Frank Bliemeister
发明人： Ozan Uluc , Andreas Frey , Sven Reisbach , Frank Bliemeister
IPC分类号： F25D17/04
CPC分类号： B64D13/00 , B64D2013/0614 , B64D2013/0629 , Y02T50/44 , Y02T50/56
摘要： A system (10) for cooling freight goods on board an aircraft comprises a refrigerating apparatus and a cooling station (14) to which cooling energy generated by said refrigerating apparatus is fed by means of a refrigerating medium and which is connected to an air infeed line (29) of an air-conditioning installation of the aircraft, wherein an air outlet aperture (16) of the cooling station (14) is connectable to a freight compartment (24) of the aircraft in order to discharge into said freight compartment (24) air which has been cooled down to a desired temperature.
摘要翻译：一种用于冷却飞机上的货物的系统（10），包括制冷装置和冷却站（14），所述制冷装置通过冷藏介质供给由所述制冷装置产生的冷却能量，并连接到空气进料管线（29），其中所述冷却站（14）的空气出口孔（16）可连接到所述飞行器的货舱（24），以便排放到所述货物舱（24）中）空气已被冷却到所需温度。

16. 发明申请

US20110149517A1 Aircraft Electronics Cooling Apparatus For An Aircraft Having A Liquid Cooling System 有权
标题翻译：具有液体冷却系统的飞机的飞机电子冷却装置
公开(公告)号：US20110149517A1
公开(公告)日：2011-06-23
申请号：US13036815
申请日：2011-02-28
申请人： Ozan Uluc , Ahmet Kayihan Kiryaman , Andreas Frey
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 (2), the aircraft electronics cooling system providing a thermal coupling between an electronic device (40a, 40b, 40c, 40d, 42, 44) to be cooled and the liquid cooling system (2) of the aircraft. A coolant delivered by the liquid cooling system (2) may flow through a board of the electronic device (40a, 40b, 40c, 40d), through a heat sink on which the electronic device (42) is arranged and/or through a housing in which the electronic device (44) 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（2）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电子设备（40a，40b，40c，40d，42,44）之间的热耦合，以使其成为冷却和飞机的液体冷却系统（2）。由液体冷却系统（2）输送的冷却剂可以通过电子设备（42）布置的散热器流过电子设备（40a，40b，40c，40d）的板，和/或通过壳体其中布置有电子设备（44）。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。

17. 发明申请

US20090193835A1 Cooling System and Freight Container 有权
公开(公告)号：US20090193835A1
公开(公告)日：2009-08-06
申请号：US12296350
申请日：2007-04-11
申请人： Ozan Uluc , Kayihan Ahmet Kiryaman , Matthias Witschke
发明人： Ozan Uluc , Kayihan Ahmet Kiryaman , Matthias Witschke
IPC分类号： F25D17/04 , F25D19/00
CPC分类号： B64D13/00 , Y02T50/44 , Y02T50/56
摘要： A system (10, 10′) for cooling items of freight on board an aircraft includes a refrigerating device and also a cooling station (14, 14′) to which cooling energy generated by the refrigerating device is supplied by means of a refrigerant medium. The cooling station (14, 14′) is capable of being connected to a freight compartment (24) of the aircraft or to a freight container (26′) on board the aircraft, in order to lead the cooling energy supplied to the cooling station (14, 14′) away into the freight compartment (24) or into the freight container (26′). A freight container (26′) for receiving items of freight designated for transportation on board an aircraft is capable of being connected to a cooling station (14′) of a system (10′) for cooling items of freight on board an aircraft, so that the cooling energy supplied to the cooling station (14′) is capable of being led away into the freight container (26′). An alternative system (10″) for cooling items of freight on board an aircraft includes a refrigerating device that is capable of being connected to a cooling station (14″), in order to supply cooling energy generated by the refrigerating device to the cooling station (14″) by means of a refrigerant medium. The cooling station (14″) is integrated into a freight container (26″) for receiving items of freight designated for transportation on board an aircraft and is set up to lead the cooling energy supplied to the cooling station (14″) away into the freight container (26″). A corresponding freight container (26″) includes a cooling station (14″) integrated into the freight container (26″), said cooling station being capable of being connected to a refrigerating device of a system for cooling items of freight on board an aircraft, in order to supply cooling energy generated by the refrigerating device to the cooling station (14″) by means of a refrigerant medium, said cooling energy being capable of being led away through the cooling station (14″) into the freight container (26″).

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