AIRCRAFT Russian patent published in 2004 - IPC

FIELD: flying vehicles.

SUBSTANCE: proposed aircraft includes fuselage with bearing platform, wing with transversal rib in the center, tail unit made in form of fin and provided with rudder and stabilizer with elevator, wing motion mechanism and drive. Lower portion of fuselage is provided with bearing platform having longitudinal slit and two ribs for mounting the wing. In the center of inner lower surface of wing there is a transversal rib and two shaped slots with shoulder according to shape of slit. Wing motion mechanism is mounted above bearing platform and consists of propeller located along fuselage axis and provided with struts at the ends which are attached to bearing platform. This mechanism is also provided with suspended guide rod located under propeller; its ends are embedded in propeller struts; mechanism is provided with two slide blocks whose nuts are fitted on propeller and bush is fitted on suspended rod. Width of slit and ribs of bearing platform ensures motion of ribs and shoulder of wing. Drive consists of electric motor, reduction gear and two connecting members in form of universal joints.

EFFECT: extended functional capabilities.

8 dwg