COOLING AN ELECTRONIC DEVICE IN AN AIRCRAFT BY CASE-BY-CASE SINGLE-PHASE OR TWO-PHASE COOLING

Cooling of an electronic device in an aircraft by case-by-case single-phase or two-phase cooling There is proposed a method for cooling an electronic device in an aircraft (11), comprising the following steps: circulating a coolant in a cooling circuit, cooling the electronic device (2) by means of...

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Bibliographische Detailangaben
Hauptverfasser:	REISS, Matthias, CASAS NORIEGA, Wilson Willy, ROERING, Sebastian
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BLASTING CASINGS OR CONSTRUCTIONAL DETAILS OF ELECTRIC APPARATUS ELECTRIC TECHNIQUES NOT OTHERWISE PROVIDED FOR ELECTRICITY HEAT EXCHANGE IN GENERAL HEAT-EXCHANGE APPARATUS, NOT PROVIDED FOR IN ANOTHER SUBCLASS,IN WHICH THE HEAT-EXCHANGE MEDIA DO NOT COME INTO DIRECT CONTACT HEATING LIGHTING MANUFACTURE OF ASSEMBLAGES OF ELECTRICAL COMPONENTS MECHANICAL ENGINEERING PRINTED CIRCUITS WEAPONS
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Beschreibung
Zusammenfassung:	Cooling of an electronic device in an aircraft by case-by-case single-phase or two-phase cooling There is proposed a method for cooling an electronic device in an aircraft (11), comprising the following steps: circulating a coolant in a cooling circuit, cooling the electronic device (2) by means of the coolant, and in an aircraft outer-shell heat exchanger, emitting the heat taken up by the coolant. The coolant evaporates, at least partially, during the cooling of the electronic device (2), and condenses in the aircraft outer-shell heat exchanger (7). The coolant circulates in the coolant circuit by natural convection.