Battery module configured for use in an electric aircraft

A system including a battery module configured for use in an electric aircraft includes at least a battery cell and a battery module casing. The at least a battery cell includes at least a pair of cell tabs and at least a conductor. The battery module casing includes at least a lithiophobic surface...

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Bibliographische Detailangaben
Hauptverfasser:	Meyjes, Sam, Lawes, Stephen, Schreiber, Stuart, Bannon, Seamus
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS COSMONAUTICS DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ELECTRICITY ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR HELICOPTERS MAGNETIC SUSPENSION OR LEVITATION FOR VEHICLES PARACHUTES PERFORMING OPERATIONS PROCESSES OR MEANS, e.g. BATTERIES, FOR THE DIRECT CONVERSIONOF CHEMICAL INTO ELECTRICAL ENERGY TRANSPORTING VEHICLES IN GENERAL
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Beschreibung
Zusammenfassung:	A system including a battery module configured for use in an electric aircraft includes at least a battery cell and a battery module casing. The at least a battery cell includes at least a pair of cell tabs and at least a conductor. The battery module casing includes at least a lithiophobic surface with an ejecta barrier and at least a nonlithiphobic surface that is configured to vent the cell ejecta. The battery module casing closely matches the dimensions of the battery cell.