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.
AN AIRPLANE WITH TANDEM ROTO-STABILIZERS
AVION A ROTO-STABILISATEURS EN TANDEM
2021-08-06
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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