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1. 发明授权

US08528348B2 Cooling system for cooling heat loads on board an aircraft and method for operating such a cooling system 有权
标题翻译：用于冷却飞机上的热负荷的冷却系统和用于操作这种冷却系统的方法
公开(公告)号：US08528348B2
公开(公告)日：2013-09-10
申请号：US12438489
申请日：2007-08-17
申请人： Wolfgang Ebigt , Wilson Willy Casas Noriega , Andreas Frey , Dirk Kastell
发明人： Wolfgang Ebigt , Wilson Willy Casas Noriega , Andreas Frey , Dirk Kastell
IPC分类号： F25B7/00
CPC分类号： F25B25/005 , B64D13/06 , B64D2013/0629 , B64D2013/064 , B64D2013/0674 , Y02T50/44 , Y02T50/56
摘要： An aircraft cooling system for cooling heat loads on board an aircraft includes a cold producing device, a first cold carrier fluid circuit thermally coupled to the cold producing device and connected to a first heat load in order to carry off heat from the first heat load, a second cold carrier fluid circuit connected to a second heat load in order to carry off heat from the second heat load, a heat exchanger disposed in the second cold carrier fluid circuit and configured to thermally couple the second cold carrier fluid circuit to an ambient temperature surrounding the aircraft, and a coupling system configured to selectively thermally couple the first cold carrier fluid circuit to the second cold carrier fluid circuit or thermally uncouple it from the second cold carrier fluid circuit.
摘要翻译：用于冷却飞机上的热负荷的飞行器冷却系统包括冷产生装置，第一冷载体流体回路，其热连接到冷产生装置并连接到第一热负载以便从第一热负荷传送热量，第二冷载体流体回路，连接到第二热负荷以便从第二热负荷传递热量;热交换器，设置在第二冷载体流体回路中并且构造成将第二冷载体流体回路热耦合到环境温度围绕飞行器以及耦合系统，其被配置为选择性地将第一冷载体流体回路耦合到第二冷载体流体回路，或者使其与第二冷载体流体回路热分解。

2. 发明申请

US20090321062A1 COOLING SYSTEM FOR COOLING HEAT LOADS ON BOARD AN AIRCRAFT AND METHOD FOR OPERATING SUCH A COOLING SYSTEM 有权
标题翻译：用于冷却飞机上的热负荷的冷却系统和用于操作这种冷却系统的方法
公开(公告)号：US20090321062A1
公开(公告)日：2009-12-31
申请号：US12438489
申请日：2007-08-17
申请人： Wolfgang Ebigt , Wilson Willy Casas Noriega , Andreas Frey , Dirk Kastell
发明人： Wolfgang Ebigt , Wilson Willy Casas Noriega , Andreas Frey , Dirk Kastell
IPC分类号： F28F27/00
CPC分类号： F25B25/005 , B64D13/06 , B64D2013/0629 , B64D2013/064 , B64D2013/0674 , Y02T50/44 , Y02T50/56
摘要： A cooling system for cooling heat loads on board an aircraft comprises a cold producing device, a first cold carrier fluid circuit, which is thermally coupled to the cold producing device and is connected to a first heat load in order to carry off heat from the first heat load, and a second cold carrier fluid circuit, which is connected to a second heat load in order to carry off heat from the second heat load. A coupling system of the cooling system is adapted to selectively thermally couple the first cold carrier fluid circuit to the second cold carrier fluid circuit or thermally uncouple it from the second cold carrier fluid circuit. In a method for operating such a cooling system for cooling heat loads on board an aircraft, the first cold carrier fluid circuit is selectively thermally coupled to the second cold carrier fluid circuit or thermally uncoupled from the second cold carrier fluid circuit by means of the coupling system.
摘要翻译：用于冷却飞机上的热负荷的冷却系统包括冷产生装置，第一冷载体流体回路，其与冷产生装置热耦合并连接到第一热负荷，以便从第一热负载和第二冷载体流体回路，其连接到第二热负荷以便从第二热负荷传递热量。冷却系统的联接系统适于选择性地将第一冷载体流体回路耦合到第二冷载体流体回路，或者使其与第二冷载体流体回路热分离。在用于操作用于冷却飞机上的热负荷的这种冷却系统的方法中，第一冷载体流体回路选择性地热耦合到第二冷载体流体回路，或者通过耦合与第二冷载体流体回路热分离系统。

3. 发明授权

US09145210B2 Redundant aircraft cooling system for redundant aircraft components 有权
标题翻译：用于冗余飞机部件的冗余飞机冷却系统
公开(公告)号：US09145210B2
公开(公告)日：2015-09-29
申请号：US12518374
申请日：2007-12-03
申请人： Wilson Willy Casas Noriega , Wolfgang Ebigt , Andreas Frey
发明人： Wilson Willy Casas Noriega , Wolfgang Ebigt , Andreas Frey
IPC分类号： F28D15/00 , F28F7/00 , B64D13/00 , B64D13/06 , F25B25/00
CPC分类号： B64D13/00 , B64D13/06 , B64D2013/0614 , B64D2013/0674 , F25B25/005 , F25B2500/06 , Y02T50/56
摘要： An aircraft cooling system includes a first coolant stream which cools at least one first heat load and a second coolant stream which cools at least one second heat load. The aircraft cooling system is formed such that the first heat load and the second heat load are thermally coupled together. The first heat load and the second heat load can be formed by two mutually redundant aircraft components. A third coolant stream thermally couples the first heat load and the second heat load together. The third coolant stream can be cooled by a heat sink, such as the outer skin of the aircraft in a bilge region.
摘要翻译：飞机冷却系统包括冷却至少一个第一热负荷的第一冷却剂流和冷却至少一个第二热负荷的第二冷却剂流。飞机冷却系统形成为使得第一热负荷和第二热负荷热耦合在一起。第一热负荷和第二热负荷可以由两个相互冗余的飞行器部件形成。第三冷却剂流将第一热负荷和第二热负荷热耦合在一起。第三冷却剂流可以由散热器（例如在舱底区域中的飞行器的外皮）来冷却。

4. 发明申请

US20100132920A1 Redundant Aircraft Cooling System For Redundant Aircraft Components 有权
标题翻译：用于冗余飞机部件的冗余飞机冷却系统
公开(公告)号：US20100132920A1
公开(公告)日：2010-06-03
申请号：US12518374
申请日：2007-12-03
申请人： Wilson Willy Casas Noriega , Wolfgang Ebigt , Andreas Frey
发明人： Wilson Willy Casas Noriega , Wolfgang Ebigt , Andreas Frey
IPC分类号： F28D15/00 , F28F7/00
CPC分类号： B64D13/00 , B64D13/06 , B64D2013/0614 , B64D2013/0674 , F25B25/005 , F25B2500/06 , Y02T50/56
摘要： An aircraft cooling system (1) according to the invention comprises a first coolant stream (4a) which cools at least one first heat load (2a), and a second coolant stream (4b) which cools at least one second heat load (2b), wherein the aircraft cooling system (1) is formed such that the first heat load (2a) and the second heat load (2b) are thermally coupled together. The first heat load (2a) and the second heat load (2b) can be formed by two mutually redundant aircraft components. A third coolant stream (12) can thermally couple the first heat load (2a) and the second heat load (2b) together. The third coolant stream (12) can be cooled by a heat sink (16).
摘要翻译：根据本发明的飞机冷却系统（1）包括冷却至少一个第一热负荷（2a）的第一冷却剂流（4a）和冷却至少一个第二热负荷（2b）的第二冷却剂流（4b），其中所述飞行器冷却系统（1）形成为使得所述第一热负荷（2a）和所述第二热负荷（2b）热耦合在一起。第一热负荷（2a）和第二热负荷（2b）可以由两个相互冗余的飞行器部件形成。第三冷却剂流（12）可以将第一热负荷（2a）和第二热负荷（2b）热耦合在一起。第三冷却剂流（12）可以被散热器（16）冷却。

5. 发明申请

US20080047688A1 Cooling System And Cooling Method For Cooling Components Of A Power Electronics 审中-公开
标题翻译：电力电子设备冷却系统及冷却方法
公开(公告)号：US20080047688A1
公开(公告)日：2008-02-28
申请号：US11845195
申请日：2007-08-27
申请人： Wolfgang Ebigt , Wilson Casas Noriega , Andreas Frey
发明人： Wolfgang Ebigt , Wilson Casas Noriega , Andreas Frey
IPC分类号： F28F7/02
CPC分类号： F28F7/02 , F28D7/0025 , F28D7/0033 , F28D15/00 , F28D2021/0029 , H01L2924/0002 , H01L2924/00
摘要： Cooling system and cooling method for cooling components of a power electronics The invention relates to a cooling system for cooling components (10) of power electronics installed on board an aircraft, in particular a passenger aircraft, comprising a cooling device (30) which is to be coupled in a heat-transmitting and planar manner to the components of the power electronics, and which cooling device (30) comprises at least two heat sinks (32, 34, 36, 38, 39, 50) fluidly isolated from one another, the cooling system further comprising at least two cooling circuits each including a cooling fluid source, wherein the at least two heat sinks of the cooling device (30) can be separately supplied with cooling fluids from different cooling fluid sources, and wherein the cooling system is configured such that no phase transition of the cooling fluids within the cooling circuits occurs, during operation of the cooling system. The invention also relates to a method for cooling components of power electronics.
摘要翻译：用于冷却电力电子设备的冷却系统和冷却方法技术领域本发明涉及一种用于冷却安装在飞机上的电力电子部件（10）的冷却系统，特别是客机，包括冷却装置（30）以热传递和平面方式耦合到电力电子设备的部件，并且该冷却装置（30）包括彼此流体隔离的至少两个散热器（32,34,36,38,39,50）所述冷却系统还包括至少两个冷却回路，每个冷却回路各自包括冷却流体源，其中所述冷却装置（30）的所述至少两个散热器可以分别从不同的冷却流体源供应冷却流体，并且其中所述冷却系统被配置为使得在冷却系统的运行期间不会发生冷却回路内的冷却流体的相变。本发明还涉及一种用于冷却电力电子元件的方法。

6. 发明授权

US08539787B2 Aircraft air-conditioning system for the individual air conditioning of regions of an aircraft cabin with a liquid coolant 有权
标题翻译：用于具有液体冷却剂的飞机机舱区域的单独空调的飞机空调系统
公开(公告)号：US08539787B2
公开(公告)日：2013-09-24
申请号：US11848760
申请日：2007-08-31
申请人： Wolfgang Ebigt , Stefan Repp , Andreas Frey
发明人： Wolfgang Ebigt , Stefan Repp , Andreas Frey
IPC分类号： B60H1/32
CPC分类号： B64D13/08 , B60N2/24 , B60N2/5628 , B60N2/5657 , B64D11/0626 , B64D2013/003 , B64D2013/0674 , F24F2221/38
摘要： An aircraft air-conditioning system is disclosed, which includes at least one heat exchanger to which coolant circulating in a cooling circuit of a cooling system and air are fed. The coolant cools the fed air in the heat exchanger, and the air leaving the heat exchanger enters the aircraft cabin. The coolant of the cooling system is always in the liquid state in the cooling circuit. The liquid coolant can also cool an aircraft seat or a sitting area of the aircraft seat.
摘要翻译：公开了一种飞机空调系统，其包括至少一个热交换器，在冷却系统的冷却回路中循环的冷却剂和空气被供给到该热交换器。冷却剂冷却热交换器中的进料空气，并且离开热交换器的空气进入飞机机舱。冷却系统的冷却液在冷却回路中总是处于液态。液体冷却剂还可以冷却飞机座椅或飞机座椅的休息区域。

7. 发明申请

US20080053126A1 Aircraft Air-Conditioning System For The Individual Air Conditioning Of Regions Of An Aircraft Cabin With A Liquid Coolant 有权
标题翻译：飞机空调系统用于具有液体冷却剂的飞机机舱区域的个人空调
公开(公告)号：US20080053126A1
公开(公告)日：2008-03-06
申请号：US11848760
申请日：2007-08-31
申请人： Wolfgang Ebigt , Stefan Repp , Andreas Frey
发明人： Wolfgang Ebigt , Stefan Repp , Andreas Frey
IPC分类号： F25D15/00
CPC分类号： B64D13/08 , B60N2/24 , B60N2/5628 , B60N2/5657 , B64D11/0626 , B64D2013/003 , B64D2013/0674 , F24F2221/38
摘要： An aircraft air-conditioning system is disclosed, which includes at least one heat exchanger (14) to which coolant circulating in a cooling circuit of a cooling system and air are fed. The coolant cools the fed air in the heat exchanger (14), and the air leaving the heat exchanger (14) enters the aircraft cabin. The coolant of the cooling system is always in the liquid state in the cooling circuit. The liquid coolant can also cool an aircraft seat (2) or a sitting area of the aircraft seat (2).
摘要翻译：公开了一种飞机空调系统，其包括至少一个热交换器（14），在冷却系统和空气的冷却回路中循环冷却剂。冷却剂冷却热交换器（14）中的进料空气，并且离开热交换器（14）的空气进入飞机机舱。冷却系统的冷却液在冷却回路中总是处于液态。液体冷却剂还可以冷却飞机座椅（2）或飞机座椅（2）的休息区域。

8. 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。

9. 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。

10. 发明授权

US07431685B2 Method and device for investigating substance libraries 有权
标题翻译：用于调查物质图书馆的方法和装置
公开(公告)号：US07431685B2
公开(公告)日：2008-10-07
申请号：US10239986
申请日：2001-03-28
申请人： Andreas Frey , Juergen Helfman , Marcus Alexander Schmidt , Gerhard Mueller
发明人： Andreas Frey , Juergen Helfman , Marcus Alexander Schmidt , Gerhard Mueller
IPC分类号： C40B50/00
CPC分类号： C07K1/047 , B01J19/0046 , B01J2219/00286 , B01J2219/00306 , B01J2219/00317 , B01J2219/00353 , B01J2219/00378 , B01J2219/00414 , B01J2219/00418 , B01J2219/00486 , B01J2219/00511 , B01J2219/0052 , B01J2219/00522 , B01J2219/00527 , B01J2219/00585 , B01J2219/0059 , B01J2219/00596 , B01J2219/00605 , B01J2219/00612 , B01J2219/00617 , B01J2219/00619 , B01J2219/00621 , B01J2219/00626 , B01J2219/00637 , B01J2219/00659 , B01J2219/00707 , B01J2219/00722 , B01J2219/00725 , C07B2200/11 , C07K1/045 , C40B40/06 , C40B40/10 , C40B60/14
摘要： The aim of the invention is to investigate the bonding of substances to target molecules. This is achieved by means of a densely packed device wherein various target molecules are bonded in a large number of sample areas. Cross-contamination and evaporation need to be minimized. The active surface of the sample areas have to be maximized. The inventive solution resides in the use of carrier plates, containing densely packed capillary structures and having a very large inner surface despite small outer dimensions. 1000 times more molecules can be bonded than on a flat outer surface of a comparable size. Cross contamination is avoided by the lack of cross links between the capillaries. Evaporation is minimized by a small outer surface. After the inner surface of the capillaries has been silanized, peptides and peptidomimetics are synthesized in a locally targeted manner. The molecular interactions of components of the substance library with active substances in a solution or a suspension are investigated by means of a local resolution optical detection method. Handling, especially cleaning and covering with substances, is carried out in a simple manner by rinsing liquids through the capillary plate.
摘要翻译：本发明的目的是研究物质与目标分子的结合。这是通过密集包装的装置实现的，其中各种目标分子结合在大量的样品区域中。交叉污染和蒸发需要最小化。样品区域的活性表面必须最大化。本发明的解决方案在于使用载体板，其包含密集填充的毛细结构，并且尽管具有小的外部尺寸，但具有非常大的内表面。与可比尺寸的平坦外表面相比，可以结合1000倍的分子。由于毛细管之间缺少交叉连接来避免交叉污染。蒸发通过小的外表面最小化。在毛细血管的内表面已被硅烷化之后，肽和肽模拟物以局部靶向的方式合成。通过局部分辨光学检测方法研究物质文库的成分与溶液或悬浮液中活性物质的分子相互作用。通过用毛细管冲洗液体，以简单的方式进行处理，特别是清洁和物质的覆盖。

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