FIELD: transport.
SUBSTANCE: invention relates to production of helicopters. Helicopter landing gear (4) comprises suspended structure (10), one wheel (8) fastened to said structure (10) to run about its axle (9), suspended structure drive means and wheels (8) arranged between retracted position to reduce drag and released position of helicopter takeoff landing. Skid (40) arranged between axle (9) and periphery of wheel (8) is located diametrically opposite said suspended structure (10) relative to said axle (9). Connector (42) comprises connecting hinges (43, 68) connecting said skid (40) with structure (10) to turn about axle (9). Resilient mounts (43, 81) serve to support said skid (40) in initial angular position. Said means (42, 81) comprises torsion roller (43) extending along axle (9).
EFFECT: landing gear adapted to various relief and landing conditions.
10 cl, 7 dwg
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