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1. 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。

2. 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。

3. 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。

4. 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。

5. 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。

6. 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。

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. 发明申请

US20100326105A1 REFRIGERATING DEVICE, IN PARTICULAR FOR AIRCRAFT 有权
标题翻译：制冷装置，特别是飞机
公开(公告)号：US20100326105A1
公开(公告)日：2010-12-30
申请号：US12790284
申请日：2010-05-28
申请人： Wilson Willy Casas Noriega , Stefan Wischhusen , Wolfgang Ebigt , Dirk Kastell
发明人： Wilson Willy Casas Noriega , Stefan Wischhusen , Wolfgang Ebigt , Dirk Kastell
IPC分类号： F25B49/02 , F25B1/00
CPC分类号： F25B41/00 , B64D13/08 , B64D2013/0674 , F25B2400/0401 , F25B2400/0411 , F25B2600/0251 , F25B2700/2106 , F25B2700/2116 , Y02T50/56
摘要： The invention relates to a refrigerating device (10), in particular for an aircraft, having a refrigerant circuit, in which a refrigerant container (12), an expansion valve (14), an evaporator (16), a compressor (20) and a condenser (22) are disposed. To save energy during operation and to increase the reliability and availability of the refrigerating device (10), in the refrigerant circuit there is a compressor bypass line (26), in which a bypass valve (18) is disposed, and a refrigerant pump (30) that is disposed downstream of the condenser (22) and upstream of the evaporator (16). It is possible to dispense with the refrigerant pump (30) if the condenser (22) is disposed at a higher level than the evaporator (16) in the refrigerant circuit.
摘要翻译：本发明涉及具有制冷剂回路的制冷装置（10），特别是用于航空器的制冷装置（10），其中制冷剂容器（12），膨胀阀（14），蒸发器（16），压缩机（20）和设置冷凝器（22）。为了节省运转时的能量，提高制冷装置（10）的可靠性和可利用性，在制冷剂回路中设置有配置有旁通阀（18）的压缩机旁通管路（26）和制冷剂泵 30），其设置在冷凝器（22）的下游和蒸发器（16）的上游。如果冷凝器（22）设置在比制冷剂回路中的蒸发器（16）更高的高度，则可以省略制冷剂泵（30）。

9. 发明授权

US08584485B2 Aircraft cooling system evaporator arrangement for two independent coolant circuits 有权
标题翻译：飞机冷却系统蒸发器布置用于两个独立的冷却剂回路
公开(公告)号：US08584485B2
公开(公告)日：2013-11-19
申请号：US12675496
申请日：2008-09-01
申请人： Wolfgang Ebigt , Wilson Willy Casas Noriega
发明人： Wolfgang Ebigt , Wilson Willy Casas Noriega
IPC分类号： F25B7/00
CPC分类号： B64D11/04 , B64D2013/0629 , B64D2013/0674 , F25B5/02 , Y02T50/46
摘要： An aircraft cooling system evaporator arrangement has an evaporation device including four evaporators that are hydraulically separate from each other with respect to coolant flow. Refrigerant flows from a feed line into first and second evaporators, from the first evaporator into and through a third evaporator, and from the second evaporator into and through a fourth evaporator. The first and third evaporators define a first pair of evaporators arranged parallel to a second pair of evaporators defined by the second and fourth evaporators. First and second coolant supply lines of a first coolant circuit supply coolant to one of the evaporators in each of the first and second pair of evaporators respectively, and first and second coolant supply lines of a second, independent coolant circuit supply coolant to the other of the evaporators in each of the first and second pair of evaporators respectively.
摘要翻译：飞机冷却系统蒸发器装置具有蒸发装置，其包括相对于冷却剂流在液压上彼此分离的四个蒸发器。制冷剂从进料管线流入第一和第二蒸发器，从第一蒸发器进入并通过第三蒸发器，并且从第二蒸发器流入并通过第四蒸发器。第一和第三蒸发器限定了平行于由第二和第四蒸发器限定的第二对蒸发器布置的第一对蒸发器。第一冷却剂回路的第一和第二冷却剂供应管线分别向第一和第二对蒸发器中的每个蒸发器中的一个蒸发器供应冷却剂，第二独立冷却剂回路的第一和第二冷却剂供应管路将冷却剂供给到另一个蒸发器分别在第一和第二对蒸发器中。

10. 发明授权

US08584484B2 Aircraft cooling system evaporator arrangement for two mutually independent coolant circuits 有权
标题翻译：飞机冷却系统蒸发器布置用于两个相互独立的冷却剂回路
公开(公告)号：US08584484B2
公开(公告)日：2013-11-19
申请号：US12675278
申请日：2008-09-01
申请人： Wolfgang Ebigt , Wilson Willy Casas Noriega
发明人： Wolfgang Ebigt , Wilson Willy Casas Noriega
IPC分类号： F25B7/00
CPC分类号： F25B5/02 , B64D13/08 , B64D2013/0629 , B64D2013/0674 , F25B2600/2511
摘要： An aircraft cooling system evaporator arrangement has at least two mutually independent coolant circuits, at least two evaporation devices arranged to be hydraulically parallel for enabling an exchange of heat between the coolant and a refrigerant, at least two supply lines for supplying refrigerant to the evaporation devices, and at least two discharge lines for discharging refrigerant from the evaporation devices. A different one of the evaporation devices, a different one of the supply lines and a different one of the discharge lines are assigned to each of the coolant circuits, and the supply lines are hydraulically separate from each other as are the discharge lines. At least one refrigerant sensor monitors a refrigerant state of each of the discharge lines and an expansion valve is driven in accordance with the refrigerant sensors to control streams of refrigerant through the supply lines.
摘要翻译：飞机冷却系统蒸发器装置具有至少两个相互独立的冷却剂回路，至少两个蒸发装置被布置成液压平行，以便能够在冷却剂和制冷剂之间交换热量，至少两条用于向制冷剂供应制冷剂的供应管线和用于从蒸发装置排出制冷剂的至少两个排出管线。不同的一个蒸发装置，不同的一个供应管线和不同的一个排放管线被分配给每个冷却剂回路，并且供应管线与排放管线一样液压地分开。至少一个制冷剂传感器监测每个排出管线的制冷剂状态，并且根据制冷剂传感器驱动膨胀阀以控制通过供应管线的制冷剂流。

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