Publication Date:
2016-06-07
Description:
Experimental findings of a three mass rotor with four channels of feedback control are reported. The channels are independently controllable with force being proportional to the velocity and/or instantaneous displacement from equilibrium of the shaft at the noncontacting probe locations (arranged in the vertical and horizontal attitudes near the support bearings). The findings suggest that automatic feedback control of rotors is feasible for limiting certain vibration levels. Control of one end of a rotor does afford some predictable vibration limiting of the rotor at the other end.
Keywords:
MECHANICAL ENGINEERING
Type:
NASA. Lewis Research Center Rotordyn. Instability Probl. in High-Performance Turbomachinery; p 434-439
Format:
application/pdf
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