An aircraft landing gear bay roof for forming a pressurization barrier between an upper pressurized compartment and a landing gear bay for the housing of a landing gear. The roof comprises a main bulkhead extending in a longitudinal direction, an inclined forward bulkhead, rigidly connected to a forward edge of the main wall, and an inclined aft bulkhead, rigidly connected to an aft edge of the main bulkhead. The forward bulkhead and the aft bulkhead each form an obtuse angle with the main bulkhead. This configuration enables a better absorption of loads by the landing gear bay roof and a shorter and optimized path for transmission of the mechanical loads, in particular to the fuselage member to which the aft bulkhead is configured to be connected.


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    Titel :

    AIRCRAFT LANDING GEAR BAY ROOF COMPRISING AN INCLINED AFT BULKHEAD


    Beteiligte:
    BELLET DANIEL (Autor:in) / LOYANT FRANCOIS (Autor:in) / LEGARDEZ ALEXANDRE (Autor:in) / ROUX SIMON (Autor:in) / CROUZET SEBASTIEN (Autor:in) / DUBREUIL LAURENT (Autor:in) / PRUDENT ALAIN (Autor:in)

    Erscheinungsdatum :

    18.04.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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