An aircraft is disclosed having a structure at least part of which is capable of generating aerodynamic lift. A body having a mass is movably mounted to a portion of the structure by an active support. The active support includes an actuator to move the body relative to the portion of the structure, and a controller for controlling movement of the actuator in response to a dynamic input. The active support provides a range of movement for the body in at least one degree of freedom. The actuator moves the body across the entire range of movement in that one degree of freedom in a time period of less than 3 seconds. The actuator moves the body sufficiently rapidly to generate an inertial force that is equal to or greater than any aerodynamic force generated by the body during that movement of the body. The active support may be used to reduce loads on the aircraft structure.


    Access

    Download


    Export, share and cite



    Title :

    AIRCRAFT WITH ACTIVE SUPPORT


    Contributors:

    Publication date :

    2019-06-13


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F15D FLUID DYNAMICS, i.e. METHODS OR MEANS FOR INFLUENCING THE FLOW OF GASES OR LIQUIDS , Strömungsdynamik, d.h. Verfahren oder Vorrichtungen zum Beeinflussen der Strömung von Gasen oder Flüssigkeiten / B64C AEROPLANES , Flugzeuge



    Aircraft with active support

    FRANCESCO GAMBIOLI / HENRY EDWARDS | European Patent Office | 2019

    Free access

    Aircraft with active support

    GAMBIOLI FRANCESCO / EDWARDS HENRY | European Patent Office | 2021

    Free access

    AIRCRAFT WITH ACTIVE SUPPORT

    GAMBIOLI FRANCESCO / EDWARDS HENRY | European Patent Office | 2019

    Free access

    AIRCRAFT WITH ACTIVE SUPPORT

    GAMBIOLI FRANCESCO / EDWARDS HENRY | European Patent Office | 2019

    Free access

    Aircraft with active support

    European Patent Office | 2018

    Free access