FLYING VEHICLE MAIN ROTOR Russian patent published in 1995 - IPC

Abstract RU 2033943 C1

FIELD: aeronautical engineering. SUBSTANCE: axis of hose bush 1 is shifted relative to axis of rotation of main rotor at displacement α. Distance between axis of lag hinge 4 and axis of rotation of main rotor is equal to l_r. Hub has torsion bar 5, casing 6 and flexible member 7 mounted in guides at clearance Δ. EFFECT: enhanced reliability of main rotor due to reduction of loads in plane of rotation. 2 dwg

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RU 2 033 943 C1

Authors

Voronkov A.Z.

Sobol' S.B.

Dates

1995-04-30—Published

1991-06-04—Filed