A composite structure forming a load bearing composite shell for a helicopter, with a shell which defines the exterior of a fuselage and includes a central fuselage section and tail boom, a fuselage which is adapted house an engine or drive train, a layered composite crashworthy seat and support structure and a fastening and a method of fastening by providing an adhesive between two layers which is allowed to flow through opposing holes in the layers to provide a chemical and mechanical attachment between the layers.


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    Titel :

    Monocoque helicopter fuselage with integral tail boom


    Beteiligte:
    MALONEY PETER (Autor:in) / HEATLEY NINA (Autor:in)

    Erscheinungsdatum :

    03.04.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B60N SEATS SPECIALLY ADAPTED FOR VEHICLES , Sitze besonders für Fahrzeuge ausgebildet / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    HELICOPTER WITH FUSELAGE AND COMPOSITE TAIL BOOM

    FINK AXEL | Europäisches Patentamt | 2018

    Freier Zugriff

    Monocoque fuselage

    Nelson, W. | Engineering Index Backfile | 1932


    The monocoque fuselage

    Seymour, Lester D. | Engineering Index Backfile | 1921


    A HELICOPTER WITH A FUSELAGE AND COMPOSITE TAIL BOOM

    FINK AXEL | Europäisches Patentamt | 2019

    Freier Zugriff

    HELICOPTER WITH A FUSELAGE AND A COMPOSITE TAIL BOOM

    FINK AXEL | Europäisches Patentamt | 2017

    Freier Zugriff