FIELD: aviation.
SUBSTANCE: proposed aircraft with lifting fuselage has wing with engines mounted on its outer panels and fuselage whose width exceeds considerably its height. Front section of fuselage smoothly changes in plan from narrow nose section to wide main section. Tail unit has two stabilizers with control surfaces which are separated in fuselage width away from longitudinal vertical plane of symmetry of aircraft and are mounted at angle relative to it. Mounted on each stabilizer is all-moving swept rudder forming T-shaped tail unit.
EFFECT: improved structure of fuselage and tail unit.
4 cl, 3 dwg
| Title | Year | Author | Number |
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