Rotorcraft flight control with a power hold function comprising monitoring one or more operational parameters (613, 621, 631) of the rotorcraft during flight, determining whether operational parameters (613, 621, 631) need adjustment according to a relationship between the operational parameters (613, 621, 631) and operating limits (615, 623, 635) associated with a particular power setting, and determining a flight parameter for one or more flight control devices of the rotorcraft in response to determining that the operational parameters (613, 621, 631) need adjustment. Providing the power hold further includes sending a position set signal to a trim assembly of the rotorcraft to set a first position of a pilot control connected to the trim assembly according to a pilot control setting (603) generated according to the flight parameter, and controlling a flight control device control according to the position of the pilot control.


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    Titel :

    SYSTEM AND METHOD FOR ROTORCRAFT COLLECTIVE POWER HOLD


    Weitere Titelangaben:

    SYSTEM UND VERFAHREN ZUR KOLLEKTIVEN LEISTUNGSSPERRE FÜR DREHFLÜGLER
    SYSTÈME ET PROCÉDÉ DE MAINTIEN DE PUISSANCE COLLECTIVE DE GIRAVION


    Beteiligte:

    Erscheinungsdatum :

    2019-11-27


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen



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