A transient derivative scheduling control system

By utilizing compensating parameters required for steady state operation of a gas turbine engine which processed variables of compressor speed, compressor pressure and altitude a derivative of the variable desired is synthesized and compared to the actual value in a closed- loop system for limiting...

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Bibliographic Details
Main Authors KENISON, DAVID FRANCIS, SPOCK, WAYNE R, MCLAUGHLIN, PETER W
Format Patent
LanguageEnglish
French
German
Published 25.06.1986
Edition4
Subjects
AIR INTAKES FOR JET-PROPULSION PLANTS
BLASTING
COMBUSTION ENGINES
CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
GAS-TURBINE PLANTS
HEATING
HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
LIGHTING
MECHANICAL ENGINEERING
WEAPONS
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Summary:By utilizing compensating parameters required for steady state operation of a gas turbine engine which processed variables of compressor speed, compressor pressure and altitude a derivative of the variable desired is synthesized and compared to the actual value in a closed- loop system for limiting the rate of change of fuel flow in an engine treatment condition. In a twin spool engine a function generator responding to speed for the low pressure compressor and altitude generates a signal indicative of rate of change if the speed of the high pressure compressor. The signal is compensated for time constants consistant with the dynamics of the engine and compared with a compensated actual high pressure compressor speed. The error produced with a gain generated from corrected high pressure compressor speed inputs the main electronic digital fuel control. (Fig. 1)
Bibliography:Application Number: EP19850630177