An aerodynamic structure incorporated in an aircraft control surface provides a spar extending along at least a portion of the control surface in a direction and the spar includes a plurality of bends along the direction of extension along the control surface to provide space to accommodate actuator fittings or other structural or operational requirements.


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    Title :

    KICKED SPARS FOR RUDDER AND ELEVATOR APPLICATIONS


    Additional title:

    GEKNICKTE HOLME FÜR SEITEN- UND HÖHENRUDERANWENDUNGEN
    LONGERONS COUDÉS POUR GOUVERNAILS DE DIRECTION ET DE PROFONDEUR


    Contributors:

    Publication date :

    2019-03-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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