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
2021-08-12
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Airplane Takeoff Trims Utilizing Stabilizers and Elevators
European Patent Office | 2019
|AIRPLANE TAKEOFF TRIMS UTILIZING STABILIZERS AND ELEVATORS
European Patent Office | 2021
|