FIELD: aircraft engineering.
SUBSTANCE: this plane features canard configuration and comprises fuselage, forplane, main tail wing, tail unit with rudder and engine with propulsor. Forplane is composed by front and rear bearing surfaces connected by central pylon. Front bearing surface is composed of the wing with sweep of 30-75 degrees in leading edge and zero sweep in trailing edge. Rear bearing surface is composed by the wing with zero sweep in leading edge and arc-shape trailing edge of negative sweep at zero pitch that has equal spacing from horizontal plane over its entire length. Front bearing surface in lengthwise direction is located ahead of rear bearing surface leading edge while in height rear bearing surface trailing edge is located under rear bearing surface leading edge.
EFFECT: better longitudinal stability at wind-wave effects.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SELF-STABILISING HOVERCRAFT | 2008 |
|
RU2424137C2 |
| AERODYNAMIC CANARD CONFIGURATION MISSILE AND METHODS OF APPLICATION | 2005 |
|
RU2327101C2 |
| SELF-STABILISING WINGED SURFACE EFFECT VEHICLE | 2007 |
|
RU2368522C2 |
| SELF-STABILISING WING-IN-GROUND EFFECT CRAFT | 2007 |
|
RU2362693C2 |
| SELF-STABILIZING WINS-IN-GROUND-EFFECT CRAFT | 2003 |
|
RU2224671C1 |
| WINGED SURFACE EFFECT VEHICLE OF "AIRPLANE" PATTERN | 2007 |
|
RU2368521C2 |
| MULTI-PURPOSE SUPER-HEAVY TRANSPORT TECHNOLOGICAL AIRCRAFT PLATFORM OF SHORT TAKE-OFF AND LANDING | 2019 |
|
RU2714176C1 |
| METHOD OF COMPLEX IMPROVEMENT OF AERODYNAMIC AND TRANSPORT CHARACTERISTICS, RAM WING MACHINE FOR IMPLEMENTATION OF NAMED METHOD (VERSIONS) AND FLIGHT METHOD | 2010 |
|
RU2539443C2 |
| WING-IN-GROUND EFFECT CRAFT | 1999 |
|
RU2232690C2 |
| GROUND-EFFECT CRAFT | 2005 |
|
RU2314219C2 |
