An aircraft includes a central wing accommodating passengers and/or freight and two lateral wings that pivot on the central wing about respective axes of rotation. The various wings obey the following geometric characteristics: 0.3×Long1.4×Long, wherein Larg being the distance between the two axes, Long being the length of the central wing, Haut being the height of the central wing, Env being the wingspan of the aircraft. The axes of rotation are inclined by an angle relative to the vertical axis of the aircraft such that the lateral pivot from rear to front and vice versa so as to come closer to, or deploy on either side from, the fuselage.
AÉRONEF À PROPULSION ÉLECTRIQUE COMPORTANT UNE AILE CENTRALE ET DEUX AILES LATÉRALES MOBILES EN ROTATION
AIRCRAFT WITH ONE CENTRAL WING AND TWO MOBILE ROTATING SIDE WINGS AND ELECTRICAL PROPULSION
ELEKTRISCH ANGETRIEBENES FLUGZEUG MIT ZENTRALEM FLÜGEL UND ZWEI MOBILEN DREHSEITIGEN FLÜGELN
2024-05-01
Patent
Electronic Resource
French
European Patent Office | 2021
|European Patent Office | 2021
|European Patent Office | 2021
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