AIRCRAFT WITH BALANCE, STABILITY AND CONTROL SERVO-MOTORS

摘要

The invention relates to an aircraft with balance, stability and control servo-motors, meant to be used for atmospheric and extra-atmospheric flights. According to the invention, the aircraft comprises a cylinder-shaped body, resting on a retractable landing gear, onto said body there being attached two turbo-jet engines and a trapezium-shaped wing, operated by means of some electric servo-motors (5, 6 and 7), the central vertical body (2) having a resistant tubular chamber (4) which is provided inside with the servo-motors (5, 6 and 7) arranged in the vertical, transverse and longitudinal plane, supported at one end on the tubular chamber (4) by means of some roller bearings (10), the other end of the shaft (9) of each servo-motor being mounted by means of a coupling (12) on a cross element (11) which is rigidly mounted in the tubular chamber (4), coaxial with the longitudinal axis of the aircraft.