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 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
2021-05-12
Patent
Electronic Resource
English
FORWARD SWEPT WING VTOL AIRCRAFT WITH EMBEDDED LIFT PROPULSORS
European Patent Office | 2025
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