A mounting structure 300 for mounting a plinth fairing (400,fig.5) to a fuselage (100,fig.1) of an aircraft, the mounting structure comprising a plurality of lateral frames 310 comprising at least one pair of adjacent frames comprising a first lateral frame 311, and a second lateral frame 312; a plurality of intercostal ribs 320 comprising at least a first intercostal rib 321; wherein the at least one pair of adjacent lateral frames is configured to be attachable to the fuselage of the aircraft; and wherein the first intercostal rib is configured to be selectively removably attachable to the first lateral frame and the second lateral frame. Also disclosed is a kit including the mounting structure and plinth fairing as well as a method off attachment and reconfiguration.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Customisable plinth for an aircraft


    Erscheinungsdatum :

    13.12.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    Customisable plinth for an aircraft

    KEVAN ELLIS WHITTAKER / PAUL KEITH WHITTLE / ROBERT HENRY SNEDDON et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    CUSTOMISABLE PLINTH FOR AN AIRCRAFT

    WHITTAKER KEVAN ELLIS / WHITTLE PAUL KEITH / SNEDDON ROBERT HENRY et al. | Europäisches Patentamt | 2025

    Freier Zugriff

    INTERLINKED PLINTH ATTACHMENT SYSTEM FOR AIRCRAFT SEATS

    OLESON MICHAEL L | Europäisches Patentamt | 2020

    Freier Zugriff

    INTERLINKED PLINTH ATTACHEMNT SYSTEM FOR AIRCRAFT SEATS

    OLESON MICHAEL L | Europäisches Patentamt | 2020

    Freier Zugriff

    Interlinked plinth attachment system for aircraft seats

    OLESON MICHAEL L | Europäisches Patentamt | 2023

    Freier Zugriff