The aircraft (10) comprises a fuselage (11) and a rhombohedral wing structure (12) comprising front wings (13, 14) mounted on a front wing-root support (17) and rear wings (15, 16) mounted on a rear wing-root support (18).At least two wings (13, 14) support an engine (24, 26) provided with a propeller (25, 27).The rear end of the fuselage supports an engine (21) provided with a propeller (22).The aircraft comprises means (28 to 35) for tilting said engines, the rotary shaft of each of the propellers being tilted between an orientation parallel to the main axis of the fuselage and an orientation perpendicular to the main axis of the fuselage and to an axis extending through the ends of the front wings.
AÉRONEF À VOILURE RHOMBOÉDRIQUE À DÉCOLLAGE ET/OU ATTERRISSAGE VERTICAL
RHOMBOHEDRAL-WING AIRCRAFT FOR VERTICAL TAKE-OFF AND/OR LANDING
FLUGZEUG MIT RHOMBOEDRISCHER FLÜGELSTRUKTUR FÜR SENKRECHTES STARTEN UND/ODER LANDEN
2021-05-26
Patent
Electronic Resource
French
IPC: | B64C AEROPLANES , Flugzeuge |
AÉRONEF À VOILURE RHOMBOÉDRIQUE À DÉCOLLAGE ET/OU ATTERRISSAGE VERTICAL
European Patent Office | 2018
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