RECONFIGURABLE HYBRID VTOL SYSTEM
Number of patents in Portfolio can not be more than 2000
United States of America
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Issued Date -
Apr 15, 2021
app pub date -
Oct 14, 2020
filing date -
Oct 14, 2020
priority date (Note) -
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status (Latency Note)
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Abstract
A reconfigurable hybrid Vertical Takeoff and Landing (VTOL) vehicle includes a turntable bearing coupling a conventional wing to a fuselage. The fuselage, designed to couple to and release a cargo pod from its undercarriage, is configured to accept a high wing juncture such that the wing can rotate from a flight configuration to a transport configuration. The transport configuration aligns the wing with the fuselage sufficient to enable the hybrid VTOL vehicle to fit within a standard intermodal container or transport aircraft.
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