VERTICAL TAKEOFF AND LANDING FLYING VEHICLE Russian patent published in 2005 - IPC

FIELD: aeronautical engineering.

SUBSTANCE: proposed flying vehicle has fuselage, wings, air flow generators and control system including vertical rudders which are symmetric in profile and are mounted behind wings in way of air flows. Fuselage is provided with two aerodynamic boxes which are longitudinal extensible and have rectangular apertures in outer side face; arranged in each said box are wing and air flow generator. Aerodynamic boxes are provided with reducer mechanism for synchronous transmission of torque from high-speed engines of tubular shafts of aeroturbines. Control system includes vertical and horizontal rudders located in aperture of each aerodynamic box. Wing is provided with slat and flap. Air flow reflector is mounted above wing over entire length at varying angle of attack. Fuselage is provided with vertical tail and horizontal tail and may be provided with landing skis. Each high-speed engine is made in form of shaft-turbine engine. Air flow generators are provided with axial-flow compressors; each compressor is located in rectilinear tube of tubular air ducts near intake unit on shaft secured in bearings. Boxes may be provided with reducer mechanism for synchronous transmission of torque from aeroturbine shafts to shafts of axial-flow compressors. Vertical rudders may be provided with flaps.

EFFECT: improved operational parameters.

14 cl, 12 dwg