A VTOL-CAPABLE AIRPLANE HAVING ANGLED PROPULSORS The present invention relates to an airplane capable of hyper-short / vertical takeoff and landing (hyper-STOL / VTOL) and having a positive tilt angle applied to the 5 horizontal propulsors (104A, 104B). A positive tilt angle may also be applied to the vertical propulsors (106A, 106B, 106A1, 106A2, 106B1, 106B2). This invention attempts to reduce pitch angle during hovering and vertical flight. Most Illustrative Diagram: FIG. 3
A VTOL-CAPABLE AIRPLANE HAVING ANGLED PROPULSORS
24.12.2020
Patent
Elektronische Ressource
Englisch
IPC: | B64C AEROPLANES , Flugzeuge |
FORWARD SWEPT WING VTOL AIRCRAFT WITH EMBEDDED LIFT PROPULSORS
Europäisches Patentamt | 2025
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