Active control of unsteady motion phenomena in turbomachinery

Rotary kinetic fluid motors or pumps – With sound or vibratory wave absorbing or preventing means...

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F02C 700

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active

051413914

ABSTRACT:
A control system actively controls at least one troublesome mode of an unsteady motion phenomenon in turbomachinery in order to enable an increase in the operating range of the turbomachinery. For example, rotor blade flutter or rotating stall may be controlled in a turbocompressor. The control system has a control bandwidth which is at least partly coextensive with the bandwidth of the unsteady motion phenomenon and operates by passing sensor signals related to the unsteady motion phenomenon from a sensor array in the turbomachine to a mode filter which produces a signal or signals which are related to the troublesome mode or modes. The selected mode signals are amplified and phase-shifted by time-variable amounts so as to produce control signals having controlled amplitude and phase relationship to the troublesome mode. Actuators in an actuator array continuously driven by the control signals and produce physical effects in the turbomachine which act counter to the troublesome mode without exciting others.

REFERENCES:
patent: 2926524 (1960-03-01), Sanders
patent: 3245219 (1966-04-01), Warden et al.
patent: 3936606 (1976-02-01), Wanke
patent: 4255083 (1981-03-01), Andre et al.
patent: 4557106 (1985-12-01), Williams et al.

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