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1. 发明申请

US20130215572A1 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：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。

2. 发明申请

US20100101262A1 COOLING SYSTEM AND FREIGHT CONTAINER 有权
标题翻译：冷却系统和货柜
公开(公告)号：US20100101262A1
公开(公告)日：2010-04-29
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 , B65D88/00
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，并且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。

3. 发明授权

US07697292B2 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用飞机电子冷却装置
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。

4. 发明授权

US08225622B2 Cooling system and freight container 有权
标题翻译：冷却系统和货柜
公开(公告)号：US08225622B2
公开(公告)日：2012-07-24
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： B60H1/32
CPC分类号： B64D13/00 , Y02T50/44 , Y02T50/56
摘要： A system for cooling items of freight on board an aircraft includes a refrigerating device and also a cooling station to which cooling energy generated by the refrigerating device is supplied by a refrigerant medium. The cooling station is capable of being connected to a freight compartment of the aircraft or to a freight container on board the aircraft, in order to lead the cooling energy supplied to the cooling station away into the freight compartment or into the freight container. A freight container for receiving items of freight designated for transportation on board an aircraft is capable of being connected to a cooling station of a system for cooling items of freight on board an aircraft, so that the cooling energy supplied to the cooling station is capable of being led away into the freight container.
摘要翻译：用于冷却飞机上的货物的系统包括制冷装置和冷却站，冷藏装置由制冷剂介质供给冷却装置产生的冷却能量。冷却站能够连接到飞机的货舱或飞机上的货物集装箱，以便将供应到冷却站的冷却能量送入货舱或货物集装箱。用于接收指定用于在飞机上运输的货物的货物容器能够连接到用于冷却飞机上的货物的系统的冷却站，以便供应到冷却站的冷却能量能够被带进货柜。

5. 发明申请

US20110170263A1 Aircraft Electronics Cooling Apparatus For An Aircraft Having A Liquid Cooling System 有权
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.

6. 发明申请

US20100202108A1 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：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。

7. 发明申请

US20130075055A1 SYSTEM AND METHOD FOR COOLING AND/OR HEATING AIRCRAFT DEVICES 有权
标题翻译：用于冷却和/或加热飞机装置的系统和方法
公开(公告)号：US20130075055A1
公开(公告)日：2013-03-28
申请号：US13432733
申请日：2012-03-28
申请人： Marc HOELLING , Werner ROTHAMMER , Jan DITTMAR , Carsten COLBERG , Wilson WIlly CASAS NORIEGA , Ozan ULUC , Sebastian ROERING , Holger WOLF
发明人： Marc HOELLING , Werner ROTHAMMER , Jan DITTMAR , Carsten COLBERG , Wilson WIlly CASAS NORIEGA , Ozan ULUC , Sebastian ROERING , Holger WOLF
IPC分类号： B64D13/08
CPC分类号： B64D13/08 , B64D13/00 , B64D2013/0655 , F25B49/02 , Y02T50/44 , Y02T50/56
摘要： A system for cooling and/or heating aircraft devices to be cooled and/or heated includes a first individual cooling and/or heating system associated with a first aircraft device to be cooled and/or heated, a second individual cooling and/or heating system associated with a second aircraft device to be cooled and/or heated, a cooling and/or heating energy supply apparatus adapted to supply cooling and/or heating energy generated by the first and/or the second individual cooling and/or heating system to the first and/or the second aircraft device to be cooled and/or heated, a control device adapted to receive and process signals characteristic of the cooling and/or heating requirements of the first and/or the second aircraft device to be cooled and/or heated and of the load condition of the first and/or the second individual cooling and/or heating system.
摘要翻译：用于冷却和/或加热待冷却和/或加热的飞行器装置的系统包括与要冷却和/或加热的第一飞行器装置相关联的第一单独冷却和/或加热系统，第二单独冷却和/或加热系统与要冷却和/或加热的第二飞行器装置相关联的冷却和/或加热能量供应装置，其适于将由第一和/或第二单独冷却和/或加热系统产生的冷却和/或加热能量提供给第一和/或待冷却和/或加热的第二飞行器装置，适于接收和处理特征于待冷却的第一和/或第二飞行器装置的冷却和/或加热要求的信号的控制装置和/或加热和第一和/或第二单独冷却和/或加热系统的负载状态。

8. 发明授权

US08331093B2 Aircraft electronics cooling apparatus for an aircraft having a liquid cooling system 有权
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.

9. 发明申请

US20120279680A1 System and method for controlling an aircraft cooling system 有权
标题翻译：用于控制飞机冷却系统的系统和方法
公开(公告)号：US20120279680A1
公开(公告)日：2012-11-08
申请号：US13434396
申请日：2012-03-29
申请人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
发明人： Marc Hoelling , Werner Rothammer , Jan Dittmar , Carsten Colberg , Wilson Willy Casas Noriega , Ozan Uluc , Sebastian Roering , Holger Wolf
IPC分类号： F28F27/00
CPC分类号： B64D13/08 , B64D13/00 , B64D2013/0655 , F25B49/02 , Y02T50/44 , Y02T50/56
摘要： A system for controlling a cooling system comprises an operating state detection unit adapted to detect operating signals characteristic of the operating state of the cooling system and/or the operating state of a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system and a database in which priority data dependent on the operating state and characteristic of the priority to be given to the cooling energy consumers in terms of the cooling energy to be supplied in various operating states of the cooling system and/or of the cooling energy consumers, is stored for a plurality of cooling energy consumers to be supplied with cooling energy by the cooling system.
摘要翻译：一种用于控制冷却系统的系统，包括操作状态检测单元，其适于检测冷却系统的运行状态的特性的运行信号和/或多个冷却能量消耗器的运行状态，以供冷却系统的冷却能量以及数据库，其中根据要在冷却系统和/或冷却能量消耗器的各种操作状态下供应的冷却能量，依赖于给予冷却能量消耗器的优先级的操作状态和特性的优先级数据被储存用于多个冷却能量消耗器以由冷却系统供应冷却能量。

10. 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。

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