FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to the design of unmanned aerial vehicles and anti-ship missile systems using these aircraft. Anti-ship missile system (ASMS) is equipped with at least two unmanned reactive aircrafts-helicopters (UNAH), which are returned to APAL helicopter pad, having both two-rotor coaxial bearing system (TRCBS), which includes in TRCBS-X2 two single-blade rotors (R) with profiled counterweights, providing creation of vertical thrust only at vertical and short take-off/landing (STO and SL) or in transition modes of flight, and two turbojet dual-path engines (TDPE) in common stern nacelle. Air intake inlet device is equipped with controlled different-size flaps arranged under lower or above upper inclined formed air duct channel, so that large of them deflects into channel, and smaller - outside depending on flight speed. TDPE have jet nozzles with thrust vector control (TVC) in the lifting and running system (LRS) and front output of the longitudinal shafts from their turbines for power take-off via the clutch to the coaxial HB reducer mounted at the front on the flight from the centre of mass.
EFFECT: higher payload, flight range, probability of target hitting.
5 cl, 1 dwg, 1 tbl
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Authors
Dates
2019-11-15—Published
2018-03-12—Filed