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.


    Access

    Download


    Export, share and cite



    Title :

    Monocoque helicopter fuselage with integral tail boom


    Contributors:

    Publication date :

    2018-04-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    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 | European Patent Office | 2018

    Free access

    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 | European Patent Office | 2019

    Free access

    HELICOPTER WITH A FUSELAGE AND A COMPOSITE TAIL BOOM

    FINK AXEL | European Patent Office | 2017

    Free access