Aircraft battery cooling and fire suppression
AssigneeLockheed Martin Corporation
InventorsErez Eller, Timothy F. Lauder
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AssigneeLockheed Martin Corporation
InventorsErez Eller, Timothy F. Lauder
Estimating the term…
Systems and methods for providing cooling and fire suppression for battery modules of an aircraft. One embodiment described herein provides an aircraft including a plurality of battery modules and a battery thermal management system. Each battery of the plurality of battery modules includes a housing. The battery thermal management system includes a storage vessel containing a cooling propellant, a conduit fluidly coupling the storage vessel to an interior of the housing of each of the plurality of battery modules, a vessel valve controlling a flow rate of the cooling propellant from the storage vessel to the conduit, and a venting system. The venting system includes one or more nozzles extending to an exterior of the aircraft and in fluid communication with the interior of the housing of each of the plurality of battery modules. The one or more nozzles direct the cooling propellant to the exterior of the aircraft.
An aircraft comprising:
A battery thermal management system for a plurality of battery modules within an aircraft, the battery thermal management system including:
A method of managing a plurality of battery modules aboard an aircraft, the method comprising:
Dependencies are inferred from the claim text.