AN AIRPLANE WITH TANDEM ROTO-STABILIZERS 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 5 attempts to overcome a limitation of QuadPlane design by making efficient use of both horizontal and vertical propulsions during hovering and vertical flight. Most Illustrative Diagram: FIG. 2 co <~ C) C)
AN AIRPLANE WITH TANDEM ROTO-STABILIZERS
26.08.2021
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
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