There is provided a leading edge system (10) for an aerospace vehicle. The leading edge system has at least one structural member. The leading edge system further has a plurality of removable modules removably attached to the at least one structural member. Each removable module has a hollow box substructure (42) and at least one flange portion disposed along a first end (52) of the hollow box substructure. The leading edge system further has a plurality of first attachment elements (70) configured for attaching the at least one flange portion (54) of the removable module to a first end portion of the at least one structural member. The leading edge system further has a plurality of second attachment elements (74) configured for attaching a second end of the hollow box substructure opposite the flange portion, to a second end portion of the at least one structural member opposite the first end portion.


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    Titel :

    LEADING EDGE SYSTEMS AND METHODS FOR AEROSPACE VEHICLES


    Weitere Titelangaben:

    VORDERKANTENSYSTEME UND VERFAHREN FÜR RAUMFAHRZEUGE
    SYSTÈMES ET PROCÉDÉS DE BORD D'ATTAQUE POUR LES VÉHICULES AÉROSPATIAUX


    Beteiligte:
    STANLEY DANIEL C (Autor:in) / KRUSE JOHN S (Autor:in) / EMBLER JONATHAN D (Autor:in) / O'HARA JEREMY N (Autor:in)

    Erscheinungsdatum :

    26.10.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64G Raumfahrt , COSMONAUTICS



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