Abstract

This paper examines experimentally and analytically the lateral vibrations of a Jeffcott rotor running at various unbalance states. Using a Bently Nevada RK-4 rotor kit, three states of eccentric mass unbalance were assumed in this study: 0.4g, 0.8g and 1.2g. Measurements of the startup data and the steady state data at rigid and flexible rotor condition were collected using a setup that mimics the vibration monitoring industrial practices. Lagrange method was assumed to construct a linear mathematical model of the investigated rotor, based on rigid rotor assumptions, that can predict analytically the lateral vibrations. The dynamic characteristics of the system, including the linearized bearing induced stiffness, were solely extracted from startup data. It was concluded that the developed twodegrees- of-freedom model was able to predict the lateral vibration at the rigid condition with an error around 5%. Whereas it failed to predict the response at flexible condition with matching accuracy. Unlike the majority of the work done in this field where complex, nonlinear mathematical model were used to model real systems, this work validates the applicability of using simple mathematical models in predicting the response of a real rotorsystem with an acceptable accuracy.

Highlights

  • VWDUWXS WHVW WR HYDOXDWH WKH V\VWHP HTXLYDOHQW VWLIIQHVV DQG GDPSLQJ DQG D WLPHZDYH UHVSRQVH WHVW DW FRQVWDQW VSHHGV 530 DQG 530 WR FKHFN WKH YDOLGLW\ RI WKH PDWKHPDWLFDO PRGHO DW D SUDFWLFDO RSHUDWLRQ UDQJH 7KUHH GLIIHUHQW XQEDODQFH VWDWHV ZHUH VLPXODWHG XVLQJ DQG JUDPV HFFHQWULF PDVVHV

  • $EVWUDFW This paper examines experimentally and analytically the lateral vibrations of a Jeffcott rotor running at various unbalance states

  • It was concluded that the developed twodegrees-of-freedom model was able to predict the lateral vibration at the rigid condition with an error around 5%

Read more

Summary

Introduction

VWDUWXS WHVW WR HYDOXDWH WKH V\VWHP HTXLYDOHQW VWLIIQHVV DQG GDPSLQJ DQG D WLPHZDYH UHVSRQVH WHVW DW FRQVWDQW VSHHGV 530 DQG 530 WR FKHFN WKH YDOLGLW\ RI WKH PDWKHPDWLFDO PRGHO DW D SUDFWLFDO RSHUDWLRQ UDQJH 7KUHH GLIIHUHQW XQEDODQFH VWDWHV ZHUH VLPXODWHG XVLQJ DQG JUDPV HFFHQWULF PDVVHV.

Results
Conclusion
Full Text
Paper version not known

Talk to us

Join us for a 30 min session where you can share your feedback and ask us any queries you have

Schedule a call