An aircraft fuel tank arrangement for the relief of a pressure differential between the interior of the aircraft fuel tank and the ambient atmosphere is provided. The aircraft fuel tank arrangement comprises a removable cartridge received within a cartridge-receiving body located at least partially in the fuel tank, said cartridge comprising a first burstable member operable to rupture in the presence of a pressure differential between the interior of the aircraft fuel tank and the ambient atmosphere which is greater than a predetermined pressure differential.


    Access

    Download


    Export, share and cite



    Title :

    Aircraft fuel tank arrangement


    Contributors:

    Publication date :

    2018-05-15


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Aircraft fuel tank inerting arrangement

    JONES JOHN ALAN / HASKINS RICHARD | European Patent Office | 2015

    Free access

    FUEL TANK ARRANGEMENT AND VEHICLE WITH FUEL TANK ARRANGEMENT

    ALEXANDER REINDL | European Patent Office | 2023

    Free access

    FUEL TANK ARRANGEMENT STRUCTURE

    KASUYA YUSUKE / SOMA SATOSHI / IMAMURA SHOGO et al. | European Patent Office | 2017

    Free access

    AIRCRAFT FUEL TANK

    IRWIN ANDREW JAMES | European Patent Office | 2015

    Free access

    Aircraft fuel tank access cover and an aircraft fuel tank

    KORYA CHETAN / SANDERSON TIMOTHY J | European Patent Office | 2015

    Free access