<p>VTOL aircraft comprising a first and a second ducted rotor (1, 2) positioned at the ends (8, 9) of a vertical fuselage (3) and whose propellers (4, 6) are driven to rotate in mutually opposite directions. Control flaps (13) for orientation and transverse flight are operatively associated at least to the lower ducted rotor (2). <IMAGE></p>
申请公布号
EP1396423(A1)
申请公布日期
2004.03.10
申请号
EP20030016319
申请日期
2003.07.18
申请人
C.R.F. SOCIETA CONSORTILE PER AZIONI
发明人
PERLO, PIERO;BOLLEA, DENIS;ALACQUA, STEFANO;FINIZIO, ROBERTO;CARVIGNESE, COSIMO;BALOCCO, ELENA
