FIELD: aircraft engineering.
SUBSTANCE: gyroplane comprises aircraft airframe, rotor arranged on airframe with its blade rigidly fixed with rotor hub and aircraft internal combustion engine. Gyroplane airframe accommodates a pair of high-speed rotors comprising set of blades fitted at sweepback angle «
» with respect to blade section peripheral speed vector «
», where «» is the angle between blade front edge and plane perpendicular to vector «
». Ends of adjacent swept-back blades are linked up and furnished with jet nozzles. Gyroplane additionally incorporates compressor coupled with aircraft internal combustion engine.
EFFECT: increased horizontal flight speed, simpler system of rotor start prior to take-off and easier control in take-off and landing.
2 dwg
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