An apparatus including one or more panels including an outer face sheet comprising a plurality of first composite materials; an inner face sheet comprising a plurality of second composite materials; and a plurality of foam pieces disposed between the outer face sheet and the inner face sheet, wherein the foam pieces reduce warping of the panels.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    COMPOSITE THIN WINGBOX ARCHITECTURE FOR SUPERSONIC BUSINESS JETS


    Beteiligte:

    Erscheinungsdatum :

    21.04.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS



    Composite thin wingbox architecture for supersonic business jets

    BEHZADPOUR FOROUZAN / STICKLER PATRICK B | Europäisches Patentamt | 2022

    Freier Zugriff

    COMPOSITE THIN WINGBOX ARCHITECTURE FOR SUPERSONIC BUSINESS JETS

    BEHZADPOUR FOROUZAN / STICKLER PATRICK B | Europäisches Patentamt | 2022

    Freier Zugriff

    COMPOSITE THIN WINGBOX ARCHITECTURE FOR SUPERSONIC BUSINESS JETS

    FOROUZAN BEHZADPOUR / PATRICK B STICKLER | Europäisches Patentamt | 2022

    Freier Zugriff

    AIRCRAFT COMPOSITE WINGBOX INTEGRATION

    KISMARTON MAX U / MUNK CLAYTON L | Europäisches Patentamt | 2018

    Freier Zugriff

    Aircraft composite wingbox integration

    KISMARTON MAX U / MUNK CLAYTON L | Europäisches Patentamt | 2019

    Freier Zugriff