The present disclosure provides methods and system for managing gust loading in an aircraft. A deflection angle of one or more spoilers of the aircraft is monitored. When the spoiler deflection angle is above a first threshold value, one or more aileron control signals are sent to the ailerons. The aileron control signals cause the ailerons to deflect based on the spoiler deflection angle.


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    Title :

    Gust loading management


    Contributors:

    Publication date :

    2020-12-29


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    GUST LOADING MANAGEMENT

    MCCLEMENTS ARTHUR / KROESE PAUL | European Patent Office | 2019

    Free access

    GUST LOADING MANAGEMENT

    MCCLEMENTS ARTHUR / KROESE PAUL | European Patent Office | 2021

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    GUST LOADING MANAGEMENT

    MCCLEMENTS ARTHUR / KROESE PAUL | European Patent Office | 2017

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    Gust and counter gust

    Pritchard, D. | Engineering Index Backfile | 1966


    Gust loading and response of flexible aircraft

    Traillnash, R.W. / Chandivert, M.G. | Engineering Index Backfile | 1967