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
2022-08-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
AIRPLANE TAKEOFF TRIMS UTILIZING STABILIZERS AND ELEVATORS
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