Abstract
Clearances between bearing outer ring and sleeve can generally be maintained to provide a margin for the thermal expansion of the bearings. However, temperature variation, improper assembly and long-term vibration can enlarge the clearances and accelerate mechanical wear, leading to what is known as the fit looseness fault. Therefore, it is important to study a fit looseness fault model and investigate how to control the vibration coming from the fit looseness fault. In this paper, a Jeffcott rotor system with three disks was modeled as a single unit. A fit looseness model was applied in the whole rotor model to study the contact problems and response characteristics using a numerical integration method. Then, a squeeze film damper model was applied to assess the vibration reduction effects on the whole rotor system with the fit looseness fault. By comparing the results of the fit looseness fault without squeeze film damper and with squeeze film damper, it is found that the squeeze film damper can reduce nonlinear vibration responses effectively generated by the fit looseness fault for the nonlinear contact. This research work contributes to understanding the mechanism of fit looseness fault and controlling strong nonlinear vibration responses due to the fit clearances.
Highlights
Looseness fault is a typical fault in the rotating machinery including gas turbine, compressor and aero-engine
Applying the numerical methods for the rotor system with fit looseness fault and Squeeze film damper (SFD) models, this kind of piecewise nonlinear behaviors resulting from the interaction between the bearing outer ring and the sleeve were investigated to illustrate the fit looseness fault mechanism, and vibration reduction effects of SFD are assessed
In order to assess the passive vibration reduction effects of SFD, the fit looseness fault model without SFD was applied to simulate piecewise phenomenon caused by the fit clearance (50 mm)
Summary
Looseness fault is a typical fault in the rotating machinery including gas turbine, compressor and aero-engine. Applying the numerical methods for the rotor system with fit looseness fault and SFD models, this kind of piecewise nonlinear behaviors resulting from the interaction between the bearing outer ring and the sleeve were investigated to illustrate the fit looseness fault mechanism, and vibration reduction effects of SFD are assessed.
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