METHOD AND SYSTEM FOR CONTROLLING TURBOMACHINE WITH CONTROL SATURATIONS MANAGEMENT

A method for controlling the first, second and third variables of a turbine engine according to the first, second and third control variables of the turbine engine, each of which may be saturated according to an operating parameter of the turbine engine. The method comprises delivering a first multi...

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Bibliographische Detailangaben
Hauptverfasser:	CLERMONTE SYLVAIN, LE BRUN CHRISTOPHE MARC ALEXANDRE, RASLAIN TYPHAINE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	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 JET-PROPULSION PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	A method for controlling the first, second and third variables of a turbine engine according to the first, second and third control variables of the turbine engine, each of which may be saturated according to an operating parameter of the turbine engine. The method comprises delivering a first multivariable correction (120) of a first value for the three control variables; selecting (130) a first control variable to be delivered as a function of the minimum value, the maximum value and a value determined by the first correction; delivering a second multivariate correction (140) of a second value for the second and third control variables; and selecting (150) the values of the second and third control variables to be delivered among the values determined during the first correction and the values determined during the second correction. 一种用于根据涡轮发动机的第一、第二和第三控制量来控制涡轮发动机的第一、第二和第三变量的方法，所述第一、第二和第三控制量各自可以根据所述涡轮发动机的运行参数而饱和。该方法包括为三个控制量传递第一值的第一多变量校正(120)；根据最小值、最大值和由第一校正确定的值选择(130)要传递的第一控制量；为第二和第三控制量传递第二值的第二多变量校正(140)；以