Patent application number | Description | Published |
20130227969 | ACCUMULATOR ARRANGEMENT WITH AN INTEGRATED SUBCOOLER - An accumulator arrangement for use in a cooling system suitable for operation with two-phase refrigerant includes a condenser having a refrigerant inlet and a refrigerant outlet. The accumulator arrangement further includes an accumulator for receiving the two-phase refrigerant therein, the accumulator having a refrigerant inlet connected to the refrigerant outlet of the condenser and a refrigerant outlet. Finally, the accumulator arrangement includes a subcooler having a refrigerant inlet and a refrigerant outlet, the refrigerant inlet of the subcooler being connected to the refrigerant outlet of the accumulators, and the subcooler being arranged at least partially within the interior of the accumulator. | 09-05-2013 |
20130227975 | COOLING SYSTEM WITH A PLURALITY OF SUBCOOLERS - A cooling system, in particular for use on board an aircraft, includes a cooling circuit allowing circulation of a two-phase refrigerant therethrough, an evaporator disposed in the cooling circuit, and a condenser disposed in the cooling circuit. A plurality of subcoolers is arranged in series in the cooling circuit downstream of the condenser. | 09-05-2013 |
20130233003 | RELIABLE COOLING SYSTEM FOR OPERATION WITH A TWO-PHASE REFRIGERANT - A cooling system, in particular for use on board an aircraft, includes a first cooling circuit allowing circulation of a two-phase refrigerant therethrough, a first evaporator disposed in the first cooling circuit, a first condenser disposed in the first cooling circuit, and a first heat sink adapted to provide cooling energy to the first condenser. The cooling system further includes a second cooling circuit allowing circulation of a two-phase refrigerant therethrough, a second evaporator disposed in the second cooling circuit, a second condenser disposed in the second cooling circuit, a second heat sink adapted to provide cooling energy to the second condenser, and a cooling energy transfer arrangement which is adapted to transfer cooling energy provided by the first heat sink and/or the first condenser to the second cooling circuit or to transfer cooling energy provided by the second heat sink and/or the second condenser to the first cooling circuit. | 09-12-2013 |
20130233004 | COOLING SYSTEM FOR OPERATION WITH A TWO-PHASE REFRIGERANT - A cooling system particularly suitable for use on board an aircraft includes a cooling circuit allowing circulation of a two-phase refrigerant therethrough. An evaporator in the cooling circuit has a refrigerant inlet and a refrigerant outlet. A condenser in the cooling circuit has a refrigerant inlet and a refrigerant outlet. A detection device is configured to output a signal indicative of the state of aggregation of the refrigerant in a connecting portion of the cooling circuit which connects the refrigerant outlet of the evaporator to the refrigerant inlet of the condenser. A control device is configured to control at least one of the temperature and the pressure of the refrigerant in the connecting portion of the cooling circuit in dependence on the signal output by the detection device such that the refrigerant in the connecting portion of the cooling circuit is maintained in its gaseous state of aggregation. | 09-12-2013 |
20130331019 | AIRCRAFT OUTER SKIN HEAT EXCHANGER, AIRCRAFT COOLING SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT OUTER SKIN HEAT EXCHANGER - An aircraft outer skin heat exchanger includes a first cooling air inlet and a first cooling air duct section, in which a first heat carrier fluid duct section is arranged. A cooling air conveying device is configured to convey a cooling air stream in such a way through the first cooling air inlet and the first cooling air duct section that the cooling air stream is subdivided by a first heat carrier fluid duct section, arranged in the first cooling air duct section, into two partial air streams which flow through the first cooling air duct section substantially parallel to one another and in the same direction. | 12-12-2013 |
20130340470 | AIRCRAFT COMPRISING A COOLING SYSTEM FOR OPERATION WITH A TWO-PHASE REFRIGERANT - An aircraft includes a cooling system having a cooling circuit to circulate a two-phase refrigerant therethrough, an evaporator disposed in a first section of the cooling circuit and having a refrigerant inlet and outlet, a condenser disposed in a second section of the cooling circuit and having a refrigerant inlet and outlet, a first cooling circuit control valve disposed in the cooling circuit between the refrigerant outlet of the evaporator and the refrigerant inlet of the condenser, and a second cooling circuit control valve disposed in the cooling circuit between the refrigerant outlet of the condenser and the refrigerant inlet of the evaporator. The first and the second cooling circuit control valves in their closed state seal the first section of the cooling circuit from the second section of the cooling circuit. The second section of the cooling circuit is installed in an unpressurized region of the aircraft. | 12-26-2013 |
20140060090 | Method of servicing an aircraft cooling system and aircraft cooling system - A method of servicing an aircraft cooling system comprises connecting a refilling container containing a two-phase refrigerant to a refrigerant connection provided in a cooling circuit of the cooling system, supplying refrigerant from the refilling container into the cooling circuit of the cooling system, and operating a condenser disposed in the cooling circuit so as to liquefy gaseous refrigerant flowing through the cooling circuit. | 03-06-2014 |
20140060091 | Method of servicing an aircraft cooling system and aircraft cooling system - A method of servicing an aircraft cooling system comprises connecting a refilling container containing a two-phase refrigerant to a refrigerant connection provided in a cooling circuit of the cooling system, supplying refrigerant from the refilling container into the cooling circuit of the cooling system, and operating a condenser disposed in the cooling circuit so as to liquefy gaseous refrigerant flowing through the cooling circuit. | 03-06-2014 |
20140090407 | Multifunctional refrigerant container and method of operating such a refrigerant container - A refrigerant container, which is in particular suitable for use in a cooling system designed for operation with a two-phase refrigerant, includes a receiving space for receiving a refrigerant that is disposed in an interior of the refrigerant container. Disposed in the receiving space of the refrigerant container is a heat exchanger allowing passage of a further refrigerant therethrough and being configured to remove heat from refrigerant in the liquid and/or gaseous state of aggregation that is received in the receiving space in order to supercool the refrigerant and/or convert the refrigerant to the liquid state of aggregation. | 04-03-2014 |
20140090802 | AIRCRAFT THERMAL CONTROL SYSTEM AND METHOD OF OPERATING AN AIRCRAFT THERMAL CONTROL SYSTEM - An aircraft thermal control system includes a thermal control unit including an internal circuit, an evaporator and a condenser, the evaporator and the condenser being disposed in the internal circuit. The aircraft thermal control system further includes a cooling circuit which is thermally coupled to the evaporator of the thermal control unit, and a heating circuit which is thermally coupled to the condenser of the thermal control unit. | 04-03-2014 |
20140298841 | STORAGE ASSEMBLY WITH A CONVEYING DEVICE INTEGRATED INTO A STORAGE CONTAINER - A storage assembly, which is in particular suitable for use in a cooling system designed for an operation with a two-phase coolant medium, comprising a storage container with a receiving area for receiving a coolant medium and a conveying device for conveying coolant medium from the receiving area of the storage container. The conveying device is formed integral with the storage container of the storage assembly. | 10-09-2014 |
20140345305 | AIRCRAFT COOLING SYSTEM AND METHOD FOR OPERATING AN AIRCRAFT COOLING SYSTEM - An aircraft cooling system comprising a refrigerating device and a heat exchanger thermally coupled to the refrigerating device. A ram air duct of the aircraft cooling system is adapted to supply cooling air to the heat exchanger, in order to remove waste heat generated in the operation of the refrigerating device from the heat exchanger to the aircraft surroundings. A connecting element comprises a first end connected to the ram air duct and a second end connectable to a device for providing conditioned air and is adapted to supply conditioned air to the ram air duct, at least in certain operating phases of the aircraft cooling system. | 11-27-2014 |