A winglet is disclosed having a tubular main spar with forward and aft main spar webs joined by upper and lower main spar caps; a front spar with a front spar web, an upper front spar cap, and a lower front spar cap; an upper skin joined to the upper main spar cap and the upper front spar cap; and a lower skin joined to the lower main spar cap and the lower front spar cap. The winglet is manufactured by co-curing the upper skin to the upper main spar cap and the upper front spar cap; and co-curing the lower skin to the lower main spar cap and the lower front spar cap.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    BRAIDED COMPOSITE SPAR


    Weitere Titelangaben:

    UMFLOCHTENER HOLM AUS VERBUNDWERKSTOFF
    LONGERON COMPOSITE TRESSÉ


    Beteiligte:
    FONG TONY (Autor:in) / AXFORD TIMOTHY (Autor:in)

    Erscheinungsdatum :

    22.02.2017


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



    BRAIDED COMPOSITE SPAR

    FONG TONY / AXFORD TIMOTHY | Europäisches Patentamt | 2019

    Freier Zugriff

    BRAIDED COMPOSITE SPAR

    FONG TONY / AXFORD TIMOTHY | Europäisches Patentamt | 2019

    Freier Zugriff

    BRAIDED COMPOSITE SPAR

    FONG TONY / AXFORD TIMOTHY | Europäisches Patentamt | 2015

    Freier Zugriff

    BRAIDED COMPOSITE SPAR

    FONG TONY / AXFORD TIMOTHY | Europäisches Patentamt | 2016

    Freier Zugriff

    Braided composite spar

    FONG TONY / AXFORD TIMOTHY | Europäisches Patentamt | 2018

    Freier Zugriff