An aircraft (1) having a wing (3) and a wing tip device (4) at the tip of the wing (3), the wing tip device (4) having front and rear spars (14, 13), wherein the wing tip device (4) has a cross-brace spar (18) that links the front and rear spars and is oriented such that it is oblique to the front and rear spars (14, 13). A wing assembly (2) of the aircraft (1). A wing tip device (4) of the aircraft (1). A method of manufacture of the aircraft (1), wing assembly (2) and wing tip device (4).


    Access

    Download


    Export, share and cite



    Title :

    A SPAR ARRANGEMENT IN A WING TIP DEVICE


    Additional title:

    HOLMANORDNUNG IN EINER FLÜGELSPITZE
    AGENCEMENT DE LONGERONS DANS UNE EXTRÉMITÉ D'AILE


    Contributors:

    Publication date :

    2021-06-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Spar arrangement in a wing tip device

    BHATIA SARABPAL-SINGH / PHILLIPS SAMUEL | European Patent Office | 2023

    Free access

    SPAR ARRANGEMENT IN A WING TIP DEVICE

    BHATIA SARABPAL-SINGH / PHILLIPS SAMUEL | European Patent Office | 2018

    Free access

    Spar arrangement in a wing tip device

    BHATIA SARABPAL-SINGH / PHILLIPS SAMUEL | European Patent Office | 2024

    Free access

    SPAR ARRANGEMENT IN A WING TIP DEVICE

    BHATIA SARABPAL-SINGH / PHILLIPS SAMUEL | European Patent Office | 2023

    Free access

    A spar arrangement in a wing tip device

    SAMUEL PHILLIPS / SARABPAL-SINGH BHATIA | European Patent Office | 2018

    Free access