The present invention relates to an airplane capable of hyper-short/vertical takeoff and landing (hyper-STOL/VTOL) and having non-rotatable vertical propulsions. It attempts to overcome a limitation of QuadPlane design by making efficient use of both horizontal and vertical propulsions during hovering and vertical flight.
Airplane with tandem roto-stabilizers
09.08.2022
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
Airplane Takeoff Trims Utilizing Stabilizers and Elevators
Europäisches Patentamt | 2023
AIRPLANE TAKEOFF TRIMS UTILIZING STABILIZERS AND ELEVATORS
Europäisches Patentamt | 2021
|