COOLING SYSTEM AND METHOD FOR AN ELECTRICAL AIRCRAFT PROPULSION SYSTEM

The cooling system includes an energy source, one or more heat exchangers for cooling a coolant, the one or more heat exchangers being connected to the energy source by a coolant circuit, one or more air channels inside which the one or more heat exchangers are placed, wherein the coolant circuit in...

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Bibliographische Detailangaben
Hauptverfasser: Bueno Vazquez, Carlos, Xu Xu, Ji, Molano Rembiasz, Jorge
Format: Patent
Sprache:eng
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