THERMAL MANAGEMENT SYSTEM

A thermal management system (120) enables fluid coupling of the cooling circuits (122, 126, 128) for the battery (112) and the propeller arrangements (108). More than one propeller arrangement (108)can be serviced by the same cooling circuit, but distribution of the coolant may be finessed. Optional...

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Bibliographische Detailangaben
Hauptverfasser:	JAIN, Rishabh Kumar, JADHAV, Priyanka Dnyaneshwar, SACHDEVA, Aniket Devendra, SHINDE, Nikhlil, CANTRELL, Christopher Thomas, GUMASTE, Parag Ashok, GOKHALE, Manoj Prakash
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	A thermal management system (120) enables fluid coupling of the cooling circuits (122, 126, 128) for the battery (112) and the propeller arrangements (108). More than one propeller arrangement (108)can be serviced by the same cooling circuit, but distribution of the coolant may be finessed. Optional pathways are provided to use heated coolant for heating (e.g., de-icing, cabin heating, etc.) before cooling the coolant. Fluid coupling of conduits between and/or within the cooling circuits provide redundancy to accommodate various faults and equipment malfunctions.