FIELD: aviation. SUBSTANCE: proposed aircraft has fuselage with replaceable nose compartment, wing, tail unit, landing gear, engines, air intakes and auxiliary power plant which is located in tail section of fuselage across its longitudinal axis. Air intake has passage bounded by wing on which door is rotatably secured+ADs- said door is flush with upper surface of wing. Construction of air intake makes it possible to deliver air either through axial inlet or through inlet in wing. Nose fuselage is provided with replaceable compartment for different types of equipment. EFFECT: enhanced reliability and safety of flights. 15 cl, 6 dwg
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Authors
Dates
2003-08-20—Published
2002-10-02—Filed