FIELD: aviation.
SUBSTANCE: supersonic convertiplane with X-shaped wing has airframe according to the scheme of an integral unstable longitudinal triplane with a high-positioned forward-swept wing, front horizontal tail, the all-moving panels of which are mounted on top of the side air intakes, two augmented bypass turbofan engines located in the nacelles between tailbooms, which have vertical fin with small tailplane halves on their outer sides. The aircraft is equipped with a system of wings, representing a combination of two, with X-shaped in the layout of wing panels, wings, the front of which is gull wing equipped with beams in the bends of its panels. The all-moving sweep rear wing panels are rotatable in a transverse plane around the longitudinal axis of the corresponding central part of spaced beam with formation of a three-fin airframe scheme in flight.
EFFECT: increasing aerodynamic efficiency of flight due to doubled interference of inverted shock waves.
6 cl, 3 dwg, 1 tbl
Title | Year | Author | Number |
---|---|---|---|
SUPERSONIC CONVERTIBLE AIRPLANE WITH X-SHAPED WING | 2016 |
|
RU2632782C1 |
SUPERSONIC CONVERTIBLE AIRCRAFT | 2015 |
|
RU2605587C1 |
SUPERSONIC CONVERTIBLE LOW-NOISE AIRCRAFT | 2015 |
|
RU2614438C1 |
SUPERSONIC LOW-NOISE AIRCRAFT WITH TANDEM WINGS | 2015 |
|
RU2605585C1 |
SUPERSONIC AIRCRAFT WITH CLOSED STRUCTURE WINGS | 2015 |
|
RU2591102C1 |
SUPERSONIC CONVERTIBLE AIRCRAFT | 2009 |
|
RU2432299C2 |
UNMANNED AERIAL MISSILE SYSTEM AND METHOD OF ITS APPLICATION | 2018 |
|
RU2690142C1 |
STEALTH SHORT TAKE-OFF AND LANDING AIRCRAFT | 2018 |
|
RU2705416C2 |
HIGH-SPEED HYBRID DRONE COPTER-PLANE | 2010 |
|
RU2464203C2 |
CRYOGENIC TURBO-ELECTRIC STOL AIRCRAFT | 2013 |
|
RU2534676C1 |
Authors
Dates
2017-06-07—Published
2015-11-30—Filed