Patent attributes
A battery-structure that may be located at least partially in the wings of an aircraft. The battery-structure forms a portion of the structural support of the wings and includes a plurality of battery receiving compartments; and a plurality of batteries located in the battery-structure. The batteries are configured to fit snugly within the battery receiving compartments, thereby increasing the rigidity of the battery-structure and the wings. The structural constituent of the battery-structure may be made from a carbon or graphite reinforced composite material or from a fiberglass composite material. The battery-structure may include a top panel, a bottom panel, a pair of side panels, and a plurality of web members. The panels and the web members may define the battery receiving compartments. The batteries can be received snugly between the web members to reinforce the rigidity and/or strength of the battery-structure.
