FIELD: aeronautical engineering. SUBSTANCE: method of testing the helicopter rotor members for "ground resonance" consists in subsequent loading first at frequency of rotation of rotor and then at frequency of "ground resonance" and rotation of rotor and determination of frequency of natural oscillations of blades, moments in lag hinge of hose of helicopter rotor hub and stiffness of composite bearing from relationship given in formulae of invention. Loading the blade is effected on stand which makes it possible to model loads acting on real blade fitted on helicopter. EFFECT: determination of stiffness of composite bearing of lag hinge of helicopter rotor hub. 3 cl, 3 dwg
Authors
Dates
1995-04-30—Published
1991-06-24—Filed