FIELD: transport.
SUBSTANCE: invention relates to helicopter landing gear. Landing gear comprises the bracket with the first end section connected to mounting means and second end section opposite the first one whereto the wheel is attached. First end section comprises mounting section arranged to turn about the rod coupled with said mounting section across connected said support bracket. Electrically-driven actuator is arranged at mounting section and selectively driven for turning of support bracket about said rod. Said actuator extends coaxially with said rod from said mounting section. Besides, support bracket can incorporates a mounting section arranged about said rod with cover for fixed landing gear.
EFFECT: simplified design, higher reliability and safety.
14 cl, 10 dwg
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