Embodiments for hybrid pressure deck (200) of an aircraft. One embodiment is a pressure deck disposed over a main gear wheel well of an aircraft. The pressure deck includes longitudinal beams (204) extending in a forward and aft direction between an aft wheel well bulkhead (128) and a rear spar (126) of the aircraft. The pressure deck (200) also includes a web (220) attached to an underside of the longitudinal beams. The web includes a flat web portion (221) supported by transverse stiffeners extending in an inboard and outboard direction, and a curved web portion (222) including arches configured to flex laterally from load in the inboard and outboard direction. A transition between the flat web portion and the curved web portion extends at least partially in the forward and aft direction of the aircraft.


    Access

    Download


    Export, share and cite



    Title :

    HYBRID PRESSURE DECK FOR AIRCRAFT


    Additional title:

    HYBRIDES DRUCKDECK FÜR FLUGZEUGE
    PONT DE PRESSION HYBRIDE POUR AÉRONEF


    Contributors:

    Publication date :

    2022-09-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Hybrid pressure deck for aircraft

    MCLAUGHLIN MARK R / LEIBOV DAVID H | European Patent Office | 2024

    Free access

    HYBRID PRESSURE DECK FOR AIRCRAFT

    VUKOSAV DANILO / MCLAUGHLIN MARK R / LEIBOV DAVID H | European Patent Office | 2022

    Free access

    HYBRID PRESSURE DECK FOR AIRCRAFT

    VUKOSAV DANILO / MCLAUGHLIN MARK R / LEIBOV DAVID H | European Patent Office | 2022

    Free access

    AIRCRAFT PRESSURE DECK

    LEIBOV DAVID H / INGHAM STEVEN D / COX DANIEL et al. | European Patent Office | 2021

    Free access

    AIRCRAFT PRESSURE DECK

    LEIBOV DAVID H / INGHAM STEVEN D / COX DANIEL et al. | European Patent Office | 2024

    Free access