A tooling assembly (30) for manufacturing a porous composite structure (300). The tooling assembly (30) includes a first tooling member (10) and a second tooling member (20). The first tooling member (10) includes a first body (11) that defines a first internal volume (12) and a first inlet (13). The first inlet (13) is fluidly coupled with the first internal volume (12). The first tooling member (10) also includes a first tooling surface (14) that defines a plurality of first perforations (15) that are fluidly coupled with the first internal volume (12). The second tooling member (20) includes a second body (21) that defines a second internal volume (22) and a second inlet (23). The second inlet (23) is fluidly coupled with the second internal volume (22). The second tooling member (20) also includes a second tooling surface (24) that defines a plurality of second perforations (25) that are fluidly coupled with the second internal volume (22).


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    Title :

    УЗЕЛ ОСНАСТКИ И СООТВЕТСТВУЮЩИЕ СИСТЕМА И СПОСОБ ИЗГОТОВЛЕНИЯ ПОРИСТОЙ КОМПОЗИТНОЙ КОНСТРУКЦИИ


    Publication date :

    2021-06-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Russian


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT