Research on the Dynamic Characteristics of High-Speed Rotors Supported by a Double Layer Squeeze Film Damper-Bearing Composite Structure

This paper develops a dynamic model for a damper-bearing-rotor system featuring a novel double layer squeeze film damper-bearing composite structure, addressing the limitations of conventional single layer dampers in providing sufficient vibration damping for high-speed advanced mechanical equipment, such as aircraft and rocket engines. A 12-degree-of-freedom Timoshenko beam element was employed to construct a finite element model of the rotor system subjected to unbalanced and nonlinear oil film force excitation. An approach for decreasing the iterative dimension of high-dimensional local nonlinear systems has been devised, which considerably improves the efficiency of transient solutions for dynamic equations. The transient excitation process of an unbalanced rotor with multilayer oil film bearings was analyzed, with the Reynolds equations for dampers and bearings solved using the finite element method. Results indicate that the double layer squeeze oil film damper-bearing composite structure exhibits high stability, excellent impact resistance, and significantly reduces rotor amplitude at high and critical speeds. Double layer squeeze film dampers provide a more obvious vibration suppression benefit and can reduce vibrations more effectively at high speeds than single layer squeeze film dampers. Within the range of 1‰ to 2‰ of the journal radius, increasing the radial clearance of the oil film bearings as well as double layer squeeze film dampers can further reduce the rotor vibration amplitude under high-speed conditions. Additionally, experimental equipment was used to verify all three of these phenomena, and the results of the experiments demonstrated a high degree of agreement with the results of the numerical simulation.