A servocontrol for controlling the position of a moving part of an aircraft includes a piloting device configured to control a power device according to a displacement control, the piloting device including a piloting unit further including a set of electronic, mechanical and/or hydraulic accessories in fluidic communication with the hydraulic cylinder and a body delimiting a network of tubular cavities fluidically connecting the electronic, mechanical and/or hydraulic accessories. The body includes an external surface, at least a first coupling portion between the network and a hydraulic cylinder and at least a second coupling portion between the network and the hydraulic cylinder and a neutral axis being defined for each tubular cavity. The neutral axis of at least one tubular cavity is curved.


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    Titel :

    SERVOCONTROL FOR CONTROLLING THE POSITION OF A MOVING PART OF AN AIRCRAFT


    Beteiligte:
    LE ROUX XAVIER (Autor:in)

    Erscheinungsdatum :

    18.07.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



    SERVOCONTROL FOR CONTROLLING THE POSITION OF A MOVING PART OF AN AIRCRAFT MADE IN TWO DISTINCT MATERIALS

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    Improved servocontrol system

    Buchanan, E. C. | NTRS | 1978


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