METHOD OF DISTRIBUTION OF VIBRATIONAL FORCES ARISING ON HELICOPTER ROTOR SHAFT IN FLIGHT Russian patent published in 1995 - IPC

Abstract RU 2034258 C1

FIELD: aeronautical engineering. SUBSTANCE: method of determination of vibrational forces on helicopter rotor in flight consists in subsequent application of vibrational forces during ground tests in directions along shaft axis and perpendicularly to this axis, measurements of vibrational displacements in these directions and determination of vibrational forces by relationships indicated in formula of innovation. EFFECT: enhanced accuracy of determination of vibrational forces arising in flight. 2 dwg

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RU 2 034 258 C1

Authors

Voronkov A.Z.

Derbin A.N.

Dates

1995-04-30—Published

1991-06-27—Filed