FIELD: transport.
SUBSTANCE: invention relates to aircraft, more specifically to the plane which (1) contains fuselage (2) of oblong form along longitudinal axis X of the plane and at least one wing (3) fixed on the fuselage between front end rear end (25) of fuselage. The fuselage (2) actually includes cylindrical central part (21) and rear variable part (23) on which vertical fins (4) and rear power plant (50) are mounted. Between the section (231) of rear part (23) with central part (21) coupling of fuselage and the rear end (25), maximum width of each fuselage section is constant or increases towards the rear to maximum fuselage width L, height of each fuselage section decreases towards the rear in such a manner that fuselage rear end (25) forms rear edge of small thickness, actually horizontal in coordinates system of the plane and actually straightline. Jet engine (51) of power plant is installed in fuselage in so called half-integrated configuration.
EFFECT: technical result consists in simplification of aircraft engine mounting.
10 cl, 16 dwg
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Authors
Dates
2014-07-20—Published
2010-03-12—Filed