FIELD: aeronautical engineering.
SUBSTANCE: proposed aircraft has two variable-incidence wings which are arranged in nose and tail sections of fuselage. Aircraft is equipped with actuating mechanisms ensuring required lifting force due to change is incidence. Wings are tiltable relative to hinges. Aircraft is also equipped with automatic stabilization system including interceptors or control surfaces; this system may switched off at moment of longitudinal control of aircraft.
EFFECT: reduced mass due to enhanced efficiency of stabilization.
5 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| TWO-DECK AIRCRAFT WITH ROTARY WINGS SPACED APART BY VERTICAL TAIL | 2009 |
|
RU2410289C1 |
| DOUBLE-DECK HORIZONTAL TAKEOFF AND LANDING AIRCRAFT WITH TILTABLE WINGS | 2005 |
|
RU2286287C1 |
| VTOL AIRCRAFT | 2006 |
|
RU2350510C2 |
| METHOD OF COMPLEX IMPROVEMENT OF AERODYNAMIC AND TRANSPORT CHARACTERISTICS, RAM WING MACHINE FOR IMPLEMENTATION OF NAMED METHOD (VERSIONS) AND FLIGHT METHOD | 2010 |
|
RU2539443C2 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| WING-IN-GROUND-EFFECT CRAFT-AMPHIBIA ON AIR CUSHION | 2003 |
|
RU2211773C1 |
| GROUND-EFFECT CRAFT | 2002 |
|
RU2254250C2 |
| BALANCE-TYPE AIRCRAFT WITHOUT HORIZONTAL TAIL AND WITH TILTABLE WING | 2004 |
|
RU2277496C1 |
| VERTICAL OR SHORT TAKEOFF AND LANDING UNIVERSAL UNMANNED AIRCRAFT | 2015 |
|
RU2604755C1 |
| WING-IN-GROUND-EFFECT CRAFT-AMPHIBIA ON AIR CUSHION | 2003 |
|
RU2211772C1 |
