FIELD: aviation.
SUBSTANCE: invention relates to design of aircraft missile systems. Multipurpose missile aircraft system comprises optional and remotely piloted two-body helicopters, including variable-sweep oblique wing (VSOW) and on its arms two single-blade bearing rotors (SBBR), mounted on underwing fuselages-nacelles (UFN). UFN are equipped with combined engines, having free power turbines, driving SBBR and remote fans, creating at the vertical and short take-off/landing (VTL and STL) propulsive and lifting tie-rod with operating/autorotating SBBR or fixed SBBR along the UFN axis during horizontal flight in configuration of jet rotorcraft/gyroplane or aircraft. Aviation guided missiles are arranged in bomb compartments. SBBR have units for fixation of blades and counterweights in position backward and forward on flight and over VSOW in field-charging configuration of aircraft-helicopter for its transportation and maintenance in hangar of aircraft carrier.
EFFECT: higher probability of destruction of surface, underwater targets located at long range, and possibility of its attack after prolonged flight in hovering mode.
5 cl, 1 dwg, 1 tbl
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Authors
Dates
2020-12-09—Published
2019-03-22—Filed