A modular subfloor system 3 comprises first longitudinal structural frames 6, lateral regions 14, and a modular tank system 5 that is connected to the first longitudinal structural frames 6. The modular tank system 5 comprises a bottom shell 8, an upper panel 9, second longitudinal -structural frames 7 arranged between the bottom shell 8 and the upper panel 9 and transversal structural frames 10 that are arranged between the bottom shell 8 and the upper panel 9. The transversal structural frames 10 and the second longitudinal structural frames 7 form compartments 11. The modular tank system 5 further comprises tank bladders 12 arranged in at least some of the compartments 11 and sealing elements that seal the upper panel 9, the bottom shell 8, and the at least some of the compartments 11 of the modular tank system 5.


    Access

    Download


    Export, share and cite



    Title :

    A MODULAR SUBFLOOR ARRANGEMENT FOR AN AIRCRAFT



    Type of media :

    Patent


    Type of material :

    Electronic Resource



    MODULAR SUBFLOOR ARRANGEMENT FOR AN AIRCRAFT

    HUEBNER GOTTFRIED / PROBST STEFAN / LOESER FRANK et al. | European Patent Office | 2019

    Free access

    Modular subfloor arrangement for an aircraft

    HUEBNER GOTTFRIED / PROBST STEFAN / LOESER FRANK et al. | European Patent Office | 2022

    Free access

    Aircraft cabin pressure regulating subfloor

    KOREIS ROCKE R | European Patent Office | 2018

    Free access

    Aircraft Subfloor Response to Crash Loadings

    Carden, Huey D. / Hayduk, Robert J. | SAE | 1981


    AIRCRAFT CABIN PRESSURE REGULATING SUBFLOOR

    KOREIS ROCKE R | European Patent Office | 2016

    Free access