FIELD: transport.
SUBSTANCE: proposed convertiplane comprises helicopter fuselage (1), rigid propeller (4) with fixed blades (5, 6, 7) that make integral Y-like symmetric wing-rotor. Blades (9, 10, 11) are arranged on the wing outer ends to move axially thereon, coupled with airflow swashplate via horizontal rods (13) and sector levers in wing-rotor lengthwise spaces. Two rigid propellers (3) are arranged on tail unit (2) with axles coupled behind tail beam. Aforesaid axles support reversing motor drives connected, via sustainer power distribution circuit, to starter-generator.
EFFECT: simpler design, higher reliability and maneuverability.
4 cl, 7 dwg
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