BATTERY COOLING SYSTEM FOR AN AIRCRAFT

Battery cooling system (1) for an aircraft, comprisinga cooling source means (10) with a cooling medium (11),a multiplicity of battery cells (20) with a cooling line means (31-34) supporting the cooling of the multiplicity of battery cells (20),a valve (41-44) for controlling the flow of the cooling...

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Bibliographische Detailangaben
Hauptverfasser:	Handler, Balazs, Dudás, Péter, Lorincz, Daniel, Debreceni, Tibor, Balazs, Gergely György
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	BASIC ELECTRIC ELEMENTS ELECTRICITY PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY
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Beschreibung
Zusammenfassung:	Battery cooling system (1) for an aircraft, comprisinga cooling source means (10) with a cooling medium (11),a multiplicity of battery cells (20) with a cooling line means (31-34) supporting the cooling of the multiplicity of battery cells (20),a valve (41-44) for controlling the flow of the cooling medium (11) from the cooling source means (10) into the cooling line means (31-34), anda battery management device (50), which is configured to control the valve (41-44),wherein the cooling medium (11) at the cooling source means (10) is a pressurized gas.