Structural Battery for an Aircraft Vehicle

In one embodiment, systems and methods include using a battery to provide electrical charge to a vehicle. The battery comprises a first half of a housing coupled comprising one or more air vents and an anode disposed at least partially within the first half of the housing. The battery further compri...

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Bibliographische Detailangaben
Hauptverfasser:	Eller, Michael R, Brewer, Roger A
Format:	Patent
Sprache:	eng
Schlagworte:	AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BASIC ELECTRIC ELEMENTS COSMONAUTICS ELECTRIC EQUIPMENT OR PROPULSION OF ELECTRICALLY-PROPELLEDVEHICLES ELECTRICITY ELECTRODYNAMIC BRAKE SYSTEMS FOR VEHICLES, IN GENERAL EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS 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:	In one embodiment, systems and methods include using a battery to provide electrical charge to a vehicle. The battery comprises a first half of a housing coupled comprising one or more air vents and an anode disposed at least partially within the first half of the housing. The battery further comprises a second half of the housing comprising one or more air vents, wherein the anode extends from the first half of the housing and into the second half of the housing. The battery further comprises a pair of cathodes disposed within the second half of the housing, wherein the pair of cathodes extends from the second half of the housing and into the first half of the housing, wherein the anode is disposed between the pair of cathodes, wherein there is a gap between the anode and each one of the pair of cathodes.