摘要 |
The winged air or water craft has a wing surface for an aerodynamic lift with a quiet and low-energy drive to set the wing surface (18). The wing surface is in one piece, which is positioned by pref. electromotor actuators to give the lifting action and/or the wing pitch angle. The control movements are through a control cable system (22,25,26) and/or struts acting on the wing surface directly or indirectly. The movements can be effected by hydraulics. The fuselage can be fitted with an additional wing (39) for an aerodynamic lift, and an elevator (54) at the tail end. The control system works with one or more acceleration sensors to act on the auxiliary wing (39) and/or elevator (54) according to the rhythm to minimize fuselage movement.
|