Fuel control for a multi-engine gas turbine installation

Power plants – Combustion products used as motive fluid – Multiple fluid-operated motors

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60 3928R, F02C 902, F02C 908

Patent

active

041007310

ABSTRACT:
An electronic control for a multi-engine gas turbine installation includes two channels each containing a low wins gate with a signal error input and an acceleration limit input, the output of the low wins gate being applied via a high wins gate to an electronic integrator the output of which is compared with a speed signal to provide fuel control for speed governing. For balancing the two channels a difference amplifier provides an output containing information related to the output of one or other low wins gate and the difference between the values of a given parameter of each engine. This acts to control this difference both during steady running and acceleration.

REFERENCES:
patent: 3174284 (1965-03-01), McCarthy
patent: 3520133 (1970-07-01), Loft et al.
patent: 3600888 (1971-08-01), Nethken et al.
patent: 3839860 (1974-10-01), Martin

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