Method for controlling a first, a second and a third variable of a turbomachine as a function of a first, a second and a third control quantity of a turbomachine which can each be saturated as a function of the operating parameters of the turbomachine.The method comprises a first multivariable correction (120) delivering a first value for the three control quantities, a selection (130) of the first control quantity to be delivered as a function of a minimum value, of a maximum value and of the value determined by the first correction, a second multivariable correction (140) delivering a second value for the second and third control quantities, and a selection (150) of the values of the second and third control quantities to be delivered in the values determined during the first correction and those determined during the second correction.
PROCÉDÉ ET SYSTÈME DE COMMANDE D'UNE TURBOMACHINE AVEC GESTION DES SATURATIONS DE COMMANDE
METHOD AND SYSTEM FOR CONTROLLING A TURBOMACHINE WITH CONTROL SATURATIONS MANAGEMENT
VERFAHREN UND SYSTEM ZUR STEUERUNG EINER TURBOMASCHINE MIT STEUERUNGSSÄTTIGUNGSVERWALTUNG
2024-04-24
Patent
Electronic Resource
French
IPC: | F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F02K JET-PROPULSION PLANTS , Strahltriebwerke / G05B Steuer- oder Regelsysteme allgemein , CONTROL OR REGULATING SYSTEMS IN GENERAL |
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