In one aspect, there is provided a spar member for an aircraft wing including a support beam having an interior surface, an exterior surface, and opposing ends configured for an aircraft wing, the interior surface and exterior surface disposed between the opposing ends; and a first spar flange extending generally laterally from the exterior surface, the first spar flange configured for attachment with a first wing skin. The first spar flange can be an upper or lower spar flange. In some embodiments, the first spar flange is at an acute angle relative to the exterior surface of the support beam. In certain embodiments, the first spar flange is at an angle of from about 50 degrees to about 85 degrees relative to the exterior surface of the support beam.


    Access

    Download


    Export, share and cite



    Title :

    SPAR FOR A COMPOSITE WING STRUCTURE


    Contributors:

    Publication date :

    2017-08-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Spar for a composite wing structure

    WOLFE DOUGLAS K / CARLSON DAVID G / MCCULLOUGH JOHN R et al. | European Patent Office | 2020

    Free access

    COMPOSITE SPAR FOR A WING STRUCTURE

    BARNETT THOMAS / PROUDLER LEE / SCAIFE ANDREW | European Patent Office | 2019

    Free access

    COMPOSITE SPAR FOR A WING STRUCTURE

    BARNETT THOMAS / PROUDLER LEE / SCAIFE ANDREW | European Patent Office | 2021

    Free access

    Composite spar for a wing structure

    European Patent Office | 2018

    Free access

    Composite spar for a wing structure

    THOMAS BARNETT / LEE PROUDLER / ANDREW SCAIFE | European Patent Office | 2019

    Free access