FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering. Proposed aircraft consists of "carrier" aircraft with elongated main wing that can be mounted both under and below fuselage, and modular fuselages to be jointed thereto. Said modules with central and front wings are rigidly interjointed by detachable power assemblies. Air channels are formed between wings, pylons and fuselages, configured so that part of airflow adjoining the main wing becomes a confuser flow with main wing flaps deflected to increase pressure under said wing, thus increasing the lift, while flow part adjoining central wing becomes a diffuser flow with flaps deflected, thus, generating rarefaction under said wing. Control jets are arranged on the main wing tails.
EFFECT: improved bank and course controllability.
3 dwg
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