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：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：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：US09188374B2

公开(公告)日：2015-11-17

申请号：US13428050

申请日：2012-03-23

申请人： Markus Piesker ,  Ahmet Kayihan Kiryaman ,  Sebastian Roering

发明人： Markus Piesker ,  Ahmet Kayihan Kiryaman ,  Sebastian Roering

IPC分类号： F25B41/00 ,  F25B1/00 ,  F25B23/00

CPC分类号： F25B41/00 ,  F25B1/00 ,  F25B23/006 ,  F25B2600/13 ,  Y02B30/745

摘要： A cooling system for cooling food on board an aircraft includes a cooling circuit adapted to supply cooling energy to at least one cooling station, a refrigerant circulating in the cooling circuit selected such that it is convertible at least partially from the liquid to the gaseous state of aggregation on releasing its cooling energy to the at least one cooling station and subsequently convertible back at least partially to the liquid state of aggregation again by an appropriate pressure and temperature control in the cooling circuit, and a refrigerant container including a receiving space arranged in an interior space of the refrigerant container which receives the refrigerant circulating in the cooling circuit, the receiving space of the refrigerant container connected to the cooling circuit by a flow line for discharging the refrigerant from the receiving space and by a return line for returning the refrigerant into the receiving space.

摘要翻译： 一种用于冷却飞机上的食物的冷却系统，包括适于向至少一个冷却站供应冷却能量的冷却回路，选择冷却回路中循环的制冷剂，使其至少部分地从液体转变为气态 在至少一个冷却站释放其冷却能量并且随后通过冷却回路中的适当的压力和温度控制再次可转换回到聚集的液体状态的聚集;以及制冷剂容器，其包括布置在 接收在冷却回路中循环的制冷剂的制冷剂容器的内部空间，通过用于从制冷剂从容纳空间排出的流路的冷却回路连接的制冷剂容器的容纳空间和用于使制冷剂返回的返回管 接收空间。

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：US07784289B2

公开(公告)日：2010-08-31

申请号：US10584901

申请日：2004-12-30

申请人： Thomas Scherer ,  Matthias Witschke ,  Ahmet Kayihan Kiryaman

发明人： Thomas Scherer ,  Matthias Witschke ,  Ahmet Kayihan Kiryaman

IPC分类号： F25D17/02

CPC分类号： B64D13/06 ,  B64D11/04 ,  B64D2013/0629 ,  B64D2013/0674 ,  F25B2400/06 ,  F25D17/02 ,  Y02T50/56

摘要： In a cooling system (10) for cooling heat-generating installations (44, 46, 48) in an aircraft, with a refrigerating installation (12), at least one refrigeration consumer (44, 46, 48) and a refrigeration transport system (14) connecting the refrigerating installation (12) and the refrigeration consumer (44,46, 48), it is provided that the refrigerating installation (12) comprises at least one refrigeration machine (18, 20) which covers the maximum refrigeration requirement of the at least one refrigeration consumer (44, 46, 48) and in that the at least one refrigeration consumer (44, 46, 48) is supplied with cold generated in the refrigerating installation (12) via a refrigerating agent circulating in the refrigeration transport system (14).

摘要翻译： 在用于冷却飞机中的发热设备（44,46,48）的冷却系统（10）中，具有冷藏设备（12），至少一个制冷消耗器（44,46,48）和制冷运输系统 14）连接制冷装置（12）和制冷消耗装置（44,46,48）时，制冷装置（12）包括至少一个制冷机（18,20） 至少一个制冷消耗器（44,46,48），并且所述至少一个制冷消耗器（44,46,48）经由在所述制冷运输系统中循环的制冷剂在所述制冷装置（12）中产生冷 （14）。

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：US20110237173A1

公开(公告)日：2011-09-29

申请号：US13124719

申请日：2009-10-13

申请人： Jügen Kelnhofer ,  Dariusz Krakowski ,  Ahmet Kayihan Kiryaman

发明人： Jügen Kelnhofer ,  Dariusz Krakowski ,  Ahmet Kayihan Kiryaman

IPC分类号： B64D13/08

CPC分类号： B64D13/08 ,  B64D2013/0655 ,  B64D2013/0688

摘要： A system (10) for air conditioning an aircraft cabin (12) comprises an air conditioning unit (14) connected to a central mixer (16) in order to supply the central mixer (16) with air at a desired low temperature. A first recirculation system (18) is designed to remove exhaust air from a first aircraft cabin region (12a) and is connected to the central mixer (16) in order to lead the exhaust air from the first aircraft cabin region (12a) into the central mixer (16). A second recirculation system (24) is designed to remove exhaust air from a second aircraft cabin region (12b) and is connected to a local mixer (20, 22) in order to lead the exhaust air from the second aircraft cabin (12b) into the local mixer (20, 22). The local mixer (20, 22) is connected to the central mixer (16) in order to supply mixed air from the central mixer (16) into the local mixer (20, 22). The second recirculation system (24) comprises a cooling unit (28) which, in relation to the flow direction of the recirculation air removed from the second aircraft cabin region (12b) in the second recirculation system (24), is arranged upstream of the local mixer (20, 22) and is designed to cool the recirculation air removed from the second aircraft cabin region (12b) to a desired temperature.

摘要翻译： 用于空调飞机机舱（12）的系统（10）包括连接到中央混合器（16）的空调单元（14），以便在期望的低温下向中央混合器（16）供应空气。 第一再循环系统（18）被设计成从第一飞机机舱区域（12a）去除排气并且连接到中央混合器（16），以将来自第一飞机机舱区域（12a）的排出空气引导到 中央混合器（16）。 第二再循环系统（24）被设计成从第二飞机机舱区域（12b）去除排出的空气，并且连接到局部混合器（20,22），以将排出的空气从第二飞机机舱（12b）引入 本地混合器（20,22）。 局部混合器（20,22）连接到中央混合器（16），以将来自中央混合器（16）的混合空气供应到本地混合器（20,22）中。 第二再循环系统（24）包括冷却单元（28），其相对于从第二再循环系统（24）中的第二飞行器舱区域（12b）移除的再循环空气的流动方向，布置在 局部混合器（20,22），并被设计成将从第二飞机机舱区域（12b）移除的再循环空气冷却到期望的温度。

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。