FIELD: aviation. SUBSTANCE: proposed aircraft has fuselage, delta wing, engine, main and nose supports. Aircraft is provided with two wells located in side surfaces of fuselage having form of triangle in cross section at bend of surfaces at right angle and narrowing from lower tail section. Aircraft is provided with two rudders articulated in fuselage wells. Wing is mounted on said bends of side surfaces of fuselage and consists of root section and two tip sections articulated together; wing is also provided with drive in form of two power cylinders whose rods are connected with tips and housing is connected with root section; size of fuselage cross section is not similar over entire length. EFFECT: improved service properties. 12 dwg
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Authors
Dates
2004-02-10—Published
2002-06-19—Filed