Device and method for reducing gust loads acting on control surfaces of an aircraft. Each control surface is movable by at least one actuator, and a flight control system provides reference variables Xsoll and {dot over (X)}soll to actuate the actuator of each control surface. Xsoll indicates a target position, force, or moment of the actuator, and {dot over (X)}soll indicates a time derivative of Xsoll. The device includes: a first sensor system identifying a position, force, or moment, indicated by variable Fext,Boe, as produced by gusts acting from outside on the control surface; and a regulator regulating the actuator of the control surface based on Fext,Boe, Xsoll and {dot over (X)}soll, and XA and {dot over (X)}A, resulting from the actuator acting on the control surface and detected by a second sensor system, wherein regulation of the actuator by the regulator enables compensation of the position, force, or moment produced by gusts acting on the control surface.


    Access

    Download


    Export, share and cite



    Title :

    VERMINDERUNG VON AN EINEM LUFTFAHRZEUG AUFTRETENDEN BÖENLASTEN


    Additional title:

    REDUCING GUST LOADS ACTING ON AN AIRCRAFT
    RÉDUCTION DES CHARGES DE RAFALES SE PRODUISANT SUR UN AÉRONEF


    Contributors:

    Publication date :

    2021-06-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    German


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    VERMINDERUNG VON AN EINEM LUFTFAHRZEUG AUFTRETENDEN BÖENLASTEN

    VAN DER LINDEN FRANCISCUS | European Patent Office | 2018

    Free access

    Verminderung von an einem Luftfahrzeug auftretenden Böenlasten

    LINDEN FRANCISCUS VAN DER | European Patent Office | 2018

    Free access

    LUFTFAHRZEUG MIT EINEM BATTERIEKÜHLSYSTEM

    WETZEL WOLFGANG | European Patent Office | 2016

    Free access

    Luftfahrzeug mit einem Brennstoffzellenantriebssystem

    LELLEK STEPHAN / LAW BARNABY / HÄGERT JAN et al. | European Patent Office | 2024

    Free access

    Luftfahrzeug mit einem Fluidleitungssystem

    MEISIEK JÜRGEN / MAULITZ TORSTEN | European Patent Office | 2019

    Free access