Control systems and methods for an aircraft propulsion system are disclosed in which the propulsion control system (140) is integrated to intelligently control aircraft propulsion and minimize transient effects from the power demands of other aircraft subsystems (120, 130, 152)

    La présente invention se rapporte à des systèmes et à des procédés de commande destinés à un système de propulsion d'aéronef dans lesquels le système de commande de propulsion (140) est intégré pour commander intelligemment la propulsion de l'aéronef et pour réduire au minimum les effets de transition issues des demandes d'énergie d'autres sous-systèmes d'aéronef (120, 130, 152).


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    Title :

    INTELLIGENT INTEGRATED CONTROL SYSTEM AND METHOD


    Additional title:

    SYSTEME DE COMMANDE INTELLIGENT INTEGRE ET PROCEDE


    Contributors:

    Publication date :

    2022-04-26


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern



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