An actuator assembly comprising an output member rotatable about a center axis relative to a structure, a first actuator having a first stator fixed to the structure and a first rotor rotatable about the center axis relative to the first stator, a second actuator having a second stator coupled to the first rotor such that the second stator rotates about the center axis relative to the first stator with rotation of the first rotor about the center axis and having a second rotor rotationally coupled to the output member, a controller configured in a failure mode to drive one of the first actuator or the second actuator to selectively control the rotation of the output member about the center axis with an operational failure of the other of the first actuator or the second actuator.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    FAULT TOLERANT MULTIPLE ROTARY ACTUATOR ASSEMBLY


    Beteiligte:

    Erscheinungsdatum :

    23.03.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / H02P CONTROL OR REGULATION OF ELECTRIC MOTORS, ELECTRIC GENERATORS OR DYNAMO-ELECTRIC CONVERTERS , Steuern oder Regeln von elektrischen Motoren, elektrischen Generatoren, dynamoelektrischen Umformern



    Fault tolerant multiple rotary actuator assembly

    STOELTING PAUL A | Europäisches Patentamt | 2023

    Freier Zugriff

    SUMMING AND FAULT TOLERANT ROTARY ACTUATOR ASSEMBLY

    KOPP JOHN | Europäisches Patentamt | 2022

    Freier Zugriff

    Summing and fault tolerant rotary actuator assembly

    KOPP JOHN | Europäisches Patentamt | 2020

    Freier Zugriff

    SUMMING AND FAULT TOLERANT ROTARY ACTUATOR ASSEMBLY

    KOPP JOHN | Europäisches Patentamt | 2019

    Freier Zugriff

    SUMMING AND FAULT TOLERANT ROTARY ACTUATOR ASSEMBLY

    KOPP JOHN | Europäisches Patentamt | 2017

    Freier Zugriff