公开(公告)号：US20100044016A1

公开(公告)日：2010-02-25

申请号：US12514731

申请日：2007-11-20

申请人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Markus Kerber ,  Michael Dreyhaupt ,  Carsten Colberg ,  Peter Schwebke

发明人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Markus Kerber ,  Michael Dreyhaupt ,  Carsten Colberg ,  Peter Schwebke

IPC分类号： F28D15/00

CPC分类号： H05K7/20845 ,  B64D13/06 ,  B64D2013/0614 ,  H05K7/20127 ,  H05K7/20218 ,  H05K7/20872 ,  Y02T50/44 ,  Y02T50/56

摘要： The invention discloses the multistage cooling of an aircraft electronic system (2) with at least one electronic component which delivers heat. The multistage feature results from the use of a plurality of circuits for transferring the waste heat. An internal coolant (14) circulating in a closed circuit which is thermally coupled to the electronic component carries heat from the at least one electronic component to a heat exchanger (6) which delivers the heat to an external coolant which flows and/or circulates from a source outside of the aircraft electronic system (2) through the heat exchanger (6) to a sink outside of the aircraft electronic system (2). The internal coolant flows from the heat exchanger (6) in the direction of the at least one electronic component and/or circulates in a closed circuit.

摘要翻译： 本发明公开了一种具有至少一个传递热量的电子部件的飞行器电子系统（2）的多级冷却。 多级特征是由于使用多个用于传送废热的电路。 在热耦合到电子部件的闭合回路中循环的内部冷却剂（14）将热量从至少一个电子部件运送到热交换器（6），热交换器将热量传递到外部冷却剂，所述外部冷却剂从 飞机电子系统（2）外部通过热交换器（6）到飞机电子系统（2）外的水槽的源。 内部冷却剂沿着至少一个电子部件的方向从热交换器（6）流动和/或在闭合回路中循环。

公开(公告)号：US08438865B2

公开(公告)日：2013-05-14

申请号：US12514742

申请日：2007-11-20

申请人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Carsten Colberg ,  Peter Schwebke ,  Markus Kerber ,  Michael Dreyhaupt

发明人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Carsten Colberg ,  Peter Schwebke ,  Markus Kerber ,  Michael Dreyhaupt

IPC分类号： F25B17/00 ,  F25B15/00 ,  F25B27/00 ,  B60H1/32 ,  F25D17/02 ,  F25D3/00 ,  F25C5/08

CPC分类号： H05K7/20845 ,  B64D13/06 ,  B64D2013/0614 ,  H05K7/20127 ,  H05K7/20218 ,  H05K7/20872 ,  Y02T50/44 ,  Y02T50/56

摘要： A cooling system (10) for cooling an aircraft device (12) comprises an evaporator (14, 16, 18) for receiving a fluid (F) which is to be evaporated, a first adsorber (24) which contains a medium (28) for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18), as well as a second adsorber (26) which contains a medium for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18). A control system (22) is adapted to establish or to interrupt a fluid connection between the evaporator (14, 16, 18) and the first and/or the second adsorber(s) (24, 26).

摘要翻译： 用于冷却航空器装置（12）的冷却系统（10）包括用于接收待蒸发的流体（F）的蒸发器（14,16,18），包含介质（28）的第一吸附器（24） 用于吸附在蒸发器（14,16,18）中蒸发的流体（F）以及第二吸附器（26），所述第二吸附器包含吸附流体（F）的介质，所述介质在所述蒸发器 蒸发器（14,16,18）。 控制系统（22）适于建立或中断蒸发器（14,16,18）与第一和/或第二吸附器（24,26）之间的流体连接。

公开(公告)号：US20100051237A1

公开(公告)日：2010-03-04

申请号：US12514742

申请日：2007-11-20

申请人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Carsten Colberg ,  Peter Schwebke ,  Markus Kerber ,  Michael Dreyhaupt

发明人： Andreas Frey ,  Ahmet Kayihan Kiryaman ,  Carsten Colberg ,  Peter Schwebke ,  Markus Kerber ,  Michael Dreyhaupt

IPC分类号： F28D15/00

CPC分类号： H05K7/20845 ,  B64D13/06 ,  B64D2013/0614 ,  H05K7/20127 ,  H05K7/20218 ,  H05K7/20872 ,  Y02T50/44 ,  Y02T50/56

摘要： A cooling system (10) for cooling an aircraft device (12) comprises an evaporator (14, 16, 18) for receiving a fluid (F) which is to be evaporated, a first adsorber (24) which contains a medium (28) for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18), as well as a second adsorber (26) which contains a medium for the adsorption of the fluid (F) which is evaporated in the evaporator (14, 16, 18). A control system (22) is adapted to establish or to interrupt a fluid connection between the evaporator (14, 16, 18) and the first and/or the second adsorber(s) (24, 26).

摘要翻译： 用于冷却航空器装置（12）的冷却系统（10）包括用于接收待蒸发的流体（F）的蒸发器（14,16,18），包含介质（28）的第一吸附器（24） 用于吸附在蒸发器（14,16,18）中蒸发的流体（F）以及第二吸附器（26），所述第二吸附器包含吸附流体（F）的介质，所述介质在所述蒸发器 蒸发器（14,16,18）。 控制系统（22）适于建立或中断蒸发器（14,16,18）与第一和/或第二吸附器（24,26）之间的流体连接。

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：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：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：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。