Reinforcing component (11), and its manufacturing method, for a structure of an aircraft or spacecraft (1) which comprises a first component region (13), which is in particular elongate, for reinforcing at least one other element (19), and at least one second component region (17), which is permanently connected to the first component region (13). The reinforcing component (11) is formed using a thermoplastic plastics material in each of the first component region (13) and the second component region (17). In the first component region (13), the thermoplastic plastics material forms a matrix in which continuous reinforcing fibres (31) are embedded, and, in the second component region (17), the reinforcing component (11) comprises discontinuous reinforcing fibres (37) or is free of reinforcing fibres.


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    Titel :

    REINFORCING COMPONENT FOR A STRUCTURE OF AN AIRCRAFT OR SPACECRAFT, AIRCRAFT OR SPACECRAFT, AND METHOD


    Weitere Titelangaben:

    VERSTÄRKUNGSKOMPONENTE FÜR EINE STRUKTUR EINES LUFT- ODER RAUMFAHRZEUGS, LUFT- ODER RAUMFAHRZEUG UND VERFAHREN
    COMPOSANT DE RENFORCEMENT DESTINÉ À UNE STRUCTURE D'UN AÉRONEF OU D'UN ENGIN SPATIAL, AÉRONEF OU ENGIN SPATIAL ET PROCÉDÉ


    Beteiligte:
    SCHWING BERND (Autor:in) / TROULIS MANOS (Autor:in) / WERNER SVEN (Autor:in)

    Erscheinungsdatum :

    07.04.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B29L INDEXING SCHEME ASSOCIATED WITH SUBCLASS B29C, RELATING TO PARTICULAR ARTICLES , Index-Schema für besondere Gegenstände in Verbindung mit Unterklasse B29C / B64G Raumfahrt , COSMONAUTICS / B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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