Due to its high power-weight ratio and low maintenance cost, the supercritical tail rotor drive shaft has attracted more and more attention in helicopter design. The dry friction damper is specifically designed to suppress the excessive vibration of the supercritical shaft when passing through the critical speed. The stability of the shaft/damper system and the vibration damping efficiency are affected by the nonlinear rub-impact process between the shaft and the damper. In order to reveal the damping mechanism and the stability of the shaft/damper system, and to guide the design of the damper, a nonlinear dynamic model of the system is established. Typical responses for systems with different rub-impact stiffness, clearance, rub-impact friction coefficients and critical dry friction forces are obtained by numerically solving the nonlinear governing Equations. The dynamic characteristics and stability of the system are investigated by drawing the bifurcation diagrams, whirling orbits and time history diagrams. It is demonstrated that there exists three forms of rub-impact between the shaft and the friction damper, namely, the forward full annular rub-impact, forward local annular rub-impact and backward local annular rub-impact. The unstable backward full annular rub-impact is not present. With an increasing critical dry friction force and rub-impact friction coefficient, the rub-impact system will easily evolve into the backward local annular rub-impact region which decreases the system's stability. A decreasing clearance or an increasing rub-impact stiffness will induce a similar effect, but the influence of rub-impact friction coefficient and critical dry friction force is more obvious. Moreover, the effects of these four device parameters on the transcritical vibration amplitude are also derived, which will give a useful guidance for the design of the dry friction damper.
Read full abstract