FIELD: aeronautical engineering.
SUBSTANCE: proposed aircraft complex includes carrier aircraft (1) with separable unmanned flying vehicles (5) mounted in its cargo compartment (4) on revolving drum (2) of multi-position launcher (3); each flying vehicle is provided with cruising engine (8) in transportation position which may be extended to working position beyond body lines (7). Fuel system of each unmanned flying vehicle is provided with additional elastic fuel tank (14) located in cavity (6) of body for laying-out near position of engine being extended; fuel system is also provided with system indicating utilization of fuel from elastic tank. Aircraft complex includes also fuel supply source which may be brought into communication with elastic fuel tanks of unmanned flying vehicles through detachable connectors (27) fitted with shut-off valves (28). Fuel supply source is made in form of fuel tank (24) located on revolving drum of multi-position launcher and provided with fuel supply unit (29).
EFFECT: reduction of filling lines mass and length; reduction of hydraulic resistance of these lines; simplified construction.
2 cl, 7 dwg
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