Hybrid VTOL vehicle
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United States of America Patent
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Jan 2, 2018
Issued Date -
N/A
app pub date -
Jun 26, 2014
filing date -
Jun 27, 2013
priority date (Note) -
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Abstract
A hybrid VTOL vehicle having an envelope configured to provide hydrostatic buoyancy, a fuselage attached to the envelope and having at least one pair of wings extending from opposing sides thereof to produce dynamic lift through movement, and a thrust generation device on each wing and configured to rotate with each wing about an axis that is lateral to a longitudinal axis of the envelope to provide vertical takeoff or landing capabilities. Ideally, the envelope provides negative hydrostatic lift to enhance low-speed and on-the-ground stability.
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