An aircraft (100) including a fuselage (102) having a longitudinal axis (20) extending through the fuselage front end (104) and the fuselage rear end (106); a foldable wing (120) located on the fuselage (102) and being movable between a flight position wherein the wing (102) is generally perpendicular to the longitudinal axis (20), and a stowed position wherein the wing (102) is generally parallel to the longitudinal axis (20); and a pair of stabilizing wings (140, 142) having an anhedral orientation disposed on the fuselage (102).
FOLDABLE AIRCRAFT WITH ANHEDRAL STABILIZING WINGS
FALTBARES FLUGZEUG MIT ABWÄRTSGERICHTETEN STABILISIERUNGSFLÜGELN
AÉRONEF PLIABLE COMPORTANT DES AILES DE STABILISATION À DIÈDRE NÉGATIF
2020-08-26
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |