A blade including a structure with aerodynamic profile including two opposite skins obtained by three-dimensional weaving of a fibrous reinforcement densified by a matrix, and a longeron including a fibrous reinforcement obtained by three-dimensional weaving and densified by a matrix, the longeron including a first part extending outside the structure with aerodynamic profile and designed to be connected to a drive hub in rotation of the blade and a second part arranged inside the structure with aerodynamic profile between the two skins. The second part of the longeron has a thickness substantially similar to that of the skins of the structure with aerodynamic profile. In addition, the fibrous reinforcement of the second part of the longeron has the same weaving armor as that of the reinforcement of the skins of the structure with aerodynamic profile.


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    Titel :

    AUBE A LONGERON COMPOSITE INTÉGRÉ


    Weitere Titelangaben:

    BLADE HAVING AN INTEGRATED COMPOSITE SPAR
    PROPELLERBLATT MIT INTEGRIERTEM VERBUNDHOLM


    Beteiligte:
    FABRE ADRIEN (Autor:in) / HORN NICOLAS (Autor:in) / MARSAL DAVID (Autor:in) / PERROLLAZ JEAN-MARC (Autor:in)

    Erscheinungsdatum :

    13.04.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Französisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / F01D Strömungsmaschinen [Kraft- und Arbeitsmaschinen oder Kraftmaschinen], z.B. Dampfturbinen , NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS



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