A wing for an aircraft includes a first end (32), a second end (34), and a skin (44) extending longitudinally from the first end to the second end. The wing also includes at least one channel (60,62) positioned within the skin and extending longitudinally between the first and second ends. The at least one channel (60,62) defines a longitudinal translation path for translating at least one electrical power source (30) longitudinally between the first and second ends.
WING DESIGN FOR REMOVABLE BATTERY
FLÜGELKONZEPT FÜR HERAUSNEHMBARE BATTERIE
CONCEPTION D'AILE POUR BATTERIE AMOVIBLE
2024-02-21
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |