Method and system for controlling a turbomachine with control saturations management
AssigneeSafran Aircraft Engines
InventorsTyphaine Raslain, Christophe Marc Alexandre Le Brun, Sylvain Clermonte
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AssigneeSafran Aircraft Engines
InventorsTyphaine Raslain, Christophe Marc Alexandre Le Brun, Sylvain Clermonte
Estimating the term…
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.
A 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 each saturates depending on the operating parameters of the turbomachine, the control method comprising:
A system 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 each saturates depending on the operating parameters of the turbomachine, the control system comprising:
Dependencies are inferred from the claim text.