公开(公告)号：US20130215572A1

公开(公告)日：2013-08-22

申请号：US13846184

申请日：2013-03-18

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, 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。

公开(公告)号：US07697292B2

公开(公告)日：2010-04-13

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 ,  F28F7/00 ,  F28F27/00 ,  F28D15/00

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。

公开(公告)号：US08331093B2

公开(公告)日：2012-12-11

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 ,  F28F7/00

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.

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。

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。

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.

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。

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。

公开(公告)号：US20110170263A1

公开(公告)日：2011-07-14

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.

公开(公告)号：US20100202108A1

公开(公告)日：2010-08-12

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

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。