FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to aircraft missile systems. Adaptive aviation-missile system is equipped with a group of optional and remotely piloted aircraft-helicopters having front or rear horizontal fins, a double-blade bearing screw (DBS) mounted on the fuselage pylon, and combined engine with free power turbines feeding aft steering jet nozzles, leading DBS. In annular fairing there is remote fan creating at vertical and short take-off/landing of propulsive thrust with DBS or its fixed wings-blades of asymmetrically variable sweep (WBAVS) during horizontal flight in configuration of jet rotorcraft/gyroplane or transonic aircraft of weft and triplane. Helicopters can be transformed after landing on deck by stopping WBAVS, which have their fixation units when they are installed along fuselage axis in field-charging configuration for transportation in hangar, refuelling and charging with ammunition.
EFFECT: higher probability of destruction of surface, underwater targets located at long range.
5 cl, 3 dwg, 1 tbl
Title | Year | Author | Number |
---|---|---|---|
ADAPTIVE AIRBORNE MISSILE SYSTEM | 2019 |
|
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Authors
Dates
2020-05-12—Published
2019-04-03—Filed