公开(公告)号：US20040129833A1

公开(公告)日：2004-07-08

申请号：US10626697

申请日：2003-07-25

Applicant: C.R.F. SOCIETA CONSORTILE PER AZIONI

Inventor： Piero Perlo ,  Denis Bollea ,  Roberto Finizio ,  Cosimo Carvignese ,  Elena Balocco

IPC: B64C039/00

CPC classification number: B64C29/02 ,  B64C27/20 ,  B64C39/024 ,  B64C39/028 ,  B64C2201/027 ,  B64C2201/042 ,  B64C2201/044 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/108 ,  B64C2201/123 ,  B64C2201/127 ,  B64C2201/146 ,  B64C2201/162 ,  B64C2201/165

Abstract: VTOL micro-aircraft comprising a first and a second ducted rotor mutually aligned and distanced according to a common axis and whose propellers are driven in rotation in mutually opposite directions. Between the two ducted rotors are positioned a fuselage and a wing system formed by wing profiles forming an X or an H configuration and provided with control flaps.

Abstract translation: VTOL微型飞机包括第一和第二导管转子，该第一和第二导管转子根据公共轴相互对准和间隔，并且其螺旋桨沿彼此相反的方向旋转驱动。 在两个管状转子之间设置有由机翼轮廓形成的机身和机翼系统，所述机翼轮廓形成X或H构造并设置有控制翼片。

公开(公告)号：US20040129827A1

公开(公告)日：2004-07-08

申请号：US10626704

申请日：2003-07-25

Applicant: C.R.F. SOCIETA CONSORTILE PER AZIONI

Inventor： Piero Perlo ,  Denis Bollea ,  Stefano Alacqua ,  Roberto Finizio ,  Cosimo Carvignese ,  Elena Balocco

IPC: B64C027/22

CPC classification number: B64C39/026 ,  B64C29/02

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.

Abstract translation: VTOL飞机包括位于垂直机身的端部的第一和第二导管转子，并且其螺旋桨被驱动以沿彼此相反的方向旋转。 用于定向和横向飞行的控制翼片至少可操作地连接到下部管道转子。