AIRCRAFT COOLING SYSTEM

An aircraft cooling system (10) comprises a cooler (12) which is adapted to supply cooling energy to an aircraft device to be cooled, and a heat transfer arrangement (18) which is adapted to transfer waste heat generated by the cooler (12) to a cabin air extraction system (20). The heat transfer arr...

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Bibliographische Detailangaben
Hauptverfasser:	TRÜMPER, TORSTEN, REISS, MATTHIAS
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO BUILDINGS,e.g. HOUSING, HOUSE APPLIANCES OR RELATED END-USERAPPLICATIONS CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TOTRANSPORTATION COMBINED HEATING AND REFRIGERATION SYSTEMS COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS HEAT PUMP SYSTEMS HEATING LIGHTING LIQUEFACTION SOLIDIFICATION OF GASES MANUFACTURE OR STORAGE OF ICE MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS REFRIGERATION MACHINES, PLANTS OR SYSTEMS REFRIGERATION OR COOLING TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINSTCLIMATE CHANGE TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	An aircraft cooling system (10) comprises a cooler (12) which is adapted to supply cooling energy to an aircraft device to be cooled, and a heat transfer arrangement (18) which is adapted to transfer waste heat generated by the cooler (12) to a cabin air extraction system (20). The heat transfer arrangement (18) comprises a heat transfer circuit (26), in which a liquid heat transfer medium heated by the waste heat of the cooler (12) circulates.