A multirotor aircraft that includes a chassis, three or more vertical rotors, one or more free wings and one or more fixed horizontal rotors. The free wing is attached to the chassis by an axial connection so that the angle of the free wing is changed relative to the chassis according the flow of air over the free wing. The fixed horizontal rotor enables the multirotor aircraft to lower and climb while flying forward at a stable horizontal pitch of the chassis.
A FREE WING MULTIROTOR WITH VERTICAL AND HORIZONTAL ROTORS
FREIFLÜGEL-MULTIROTOR MIT VERTIKALEN UND HORIZONTALEN ROTOREN
ROTOR MULTIPLE À AILES LIBRES À ROTORS VERTICAUX ET HORIZONTAUX
2024-07-31
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge / B64U / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / G05G CONTROL DEVICES OR SYSTEMS INSOFAR AS CHARACTERISED BY MECHANICAL FEATURES ONLY , Steuer- oder Regelvorrichtungen oder Steuer- oder Regelsysteme gekennzeichnet ausschließlich durch mechanische Einzelheiten |
Free wing multirotor with vertical and horizontal rotors
European Patent Office | 2023
|Free Wing Multirotor with Vertical and Horizontal Rotors
European Patent Office | 2023
|Free wing multirotor with vertical and horizontal rotors
European Patent Office | 2024
|A FREE WING MULTIROTOR WITH VERTICAL AND HORIZONTAL ROTORS
European Patent Office | 2018
|A Free Wing Multirotor with Vertical and Horizontal Rotors
European Patent Office | 2020
|