US Patent 6854686 VTOL aircraft
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Patent 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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Patent Inventor Names
Cosimo Carvignese0
Denis Bollea0
Elena Balocco0
Piero Perlo0
Roberto Finizio0
Stefano Alacqua0
Date of Patent
February 15, 2005
0Patent Application Number
106267040
Date Filed
July 25, 2003
0Patent Primary Examiner
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US Patent 6854686 VTOL aircraft
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