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). One end of each front wing is articulated to one end of a rear wing and at least one of the wing-root supports is able to move along the fuselage. The wing-root supports (17, 18) are positioned respectively underneath and on top of the fuselage (11).The length (41) of the rear wings (15, 16) is strictly less than the length (48) of the front wings (13, 14).The aircraft (10) comprises an adaptor for adapting the position of each wing root (17, 18) to suit the flight conditions.
Aircraft with variable-geometry rhombohedral wing structure
23.11.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
AIRCRAFT WITH VARIABLE-GEOMETRY RHOMBOHEDRAL WING STRUCTURE
Europäisches Patentamt | 2019
|RHOMBOHEDRAL-WING AIRCRAFT FOR VERTICAL TAKE-OFF AND/OR LANDING
Europäisches Patentamt | 2020
|Rhombohedral-wing aircraft for vertical take-off and/or landing
Europäisches Patentamt | 2023
|