Friction Damping in Compressor Blade Dovetail Attachments
An empirical model is presented for predicting the fundamental mode resonant response of friction damped, free standing compressor blades from the cyclic slip that can occur in its dovetail attachment. The model is an extension of the conventional approach in that it includes the microslip regime of slip by assuming that the tangential force coefficient (tangential force to normal force ratio when slip occurs) depends on the magnitude of slip but, like friction coefficient, is independent of normal force. Experimental data obtained from bench damping tests are presented relating these quantities for plain and coated [copper-nickel indium (Cu-Ni-In) plus molydisulphide (MoS2)] dovetail attachments. The results demonstrate that substantial friction damping can be obtained at low compressor speeds, where aerodynamic excitation is often most severe, and that such damping is dominated by the microslip properties of the dovetail interface. The dovetail coating significantly increased friction damping and proved to be durable in an endurance test, as it has in service.