The invention refers to an aircraft, in particular to a vertical take-off and landing aircraft, and to a wing of such aircraft comprising a plurality of actuated flaps (2) each having at least one propulsion unit (4) included, the flaps BEING arranged next to each other along the wing span and independently actuated to pivot and further comprising an elastic seal in a gap between at least two of the flaps.
AIRCRAFT FLAP-TO-FLAP SEAL
DICHTUNG ZWISCHEN LUFTFAHRZEUGKLAPPEN
JOINT VOLET À VOLET D'UN AÉRONEF
2022-05-18
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |