Methods for making structural shims (220) for the mating assembly of parts, such as for installation between a skin (212) and substructure (214) of an aircraft. The methods include the steps of disposing a hardenable composition (216) into a gap between the first (212) and second parts (214), hardening the hardenable composition to provide a shim pattern (218) that is dimensionally stable, and removing the shim pattern from the gap without damage. The shim pattern can be used to provide a digital model thereof, which can in turn be used to fabricate the structural shim (220).


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    Titel :

    METHODS OF SHIMMING AN ASSEMBLY


    Beteiligte:
    ZOOK JONATHAN D (Autor:in) / HEBERT LARRY S (Autor:in) / PRAGGASTIS CHRIS A (Autor:in) / JONES JACOB P (Autor:in) / DEMOSS SUSAN E (Autor:in)

    Erscheinungsdatum :

    18.08.2022


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B29C Formen oder Verbinden von Kunststoffen , SHAPING OR JOINING OF PLASTICS / B64C AEROPLANES , Flugzeuge



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