VTOL aircraft
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United States of America Patent
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-
Feb 15, 2005
Grant Date -
Jul 8, 2004
app pub date -
Jul 25, 2003
filing date -
Jul 26, 2002
priority date (Note) -
Expired
status (Latency Note)
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Abstract
VTOL aircraft comprising a first and a second ducted rotor positioned at the ends of a vertical fuselage and whose propellers are driven to rotate in mutually opposite directions. Control flaps for orientation and transverse flight are operatively associated at least to the lower ducted rotor.
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