FIELD: transport.
SUBSTANCE: invention relates to rotorcraft, namely, to VTOL aircraft. VTOL aircraft comprises airframe composed of bearing shaped disc-like center wing section with nose fuselage-type compartment on the side of front center section front semicircle and lift blower inscribed in geometrically mid part of center section, outer wings, vertical and horizontal fins and screw propellers. Aircraft is mounted at jump landing gear. Lift blower represents a two-stage design that allows the thrust reversal. On the side of tail center section front semicircle engine nacelle with all-moving horizontal fins and screw propeller to be operated in push mid-flight screw and equalizer screw modes.
EFFECT: aircraft for transfer of cargoes and passengers over large distances.
12 cl, 11 dwg
Title | Year | Author | Number |
---|---|---|---|
MUKHAMEDOV'S CONFIGURATION AIRCRAFT OPERATING ON CRYOGENIC FUEL | 2011 |
|
RU2469915C1 |
MANEUVERABLE AEROPLANE AND METHOD OF ITS TAKEOFF | 1997 |
|
RU2115593C1 |
MULTI-PURPOSE FIGHTER | 2000 |
|
RU2166462C1 |
LARGE PASSENGER-CAPACITY AIRCRAFT OF INTEGRATED SYSTEM | 1992 |
|
RU2040435C1 |
MUKHAMEDOV'S WING | 2009 |
|
RU2412861C1 |
HEAVY-DUTY MULTI-PROPELLER CONVERTER PLATE | 2012 |
|
RU2492112C1 |
HYBRID SHORT TAKEOFF AND LANDING ELECTRIC AIRCRAFT | 2014 |
|
RU2558168C1 |
UNMANNED COMBINED HELICOPTER | 2016 |
|
RU2629482C1 |
VERTICAL SHORT TAKE-OFF AND LANDING AIRCRAFT | 0 |
|
SU1839152A1 |
VERTICAL AND ULTRA-SHORT TAKE-OFF AND LANDING AIRCRAFT | 0 |
|
SU1766781A1 |
Authors
Dates
2013-11-10—Published
2011-11-01—Filed