Potential weight savings due to the use of composite materials for highly loaded primary structures are being demonstrated through the design, fabrication, and test of an all composite wing carrythrough bulkhead for the F/A-18 fighter aircraft. A one piece composite design which results in a 24 percent weight savings, relative to the existing aluminum bulkhead, was developed. Critical details of this design were evaluated through element tests, and a full scale prototype component was fabricated. The structural integrity of this design will be demonstrated in a comprehensive full scale test program.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Development of composite wing carrythrough bulkheads for fighter aircraft


    Beteiligte:
    Goering, J. C. (Autor:in) / Behrens, R. S. (Autor:in) / Libeskind, Mark (Autor:in)


    Erscheinungsdatum :

    01.09.1990


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Development of Composite Wing Carrythrough Bulkheads for Fighter Aircraft

    J. C. Goering / R. S. Behrens / M. Libeskind | NTIS | 1990


    Probabilistic analysis of an advanced fighter/attack aircraft composite wing structure

    Millwater, H. / Griffin, K. / Wieland, D. et al. | AIAA | 2000


    INLET BULKHEADS FOR LARGE DIAMETER AIRCRAFT ENGINES

    WIJESINGHE JANAKA / ROCHA ANDREW G / ZIMNEY ERIC J | Europäisches Patentamt | 2022

    Freier Zugriff

    INLET BULKHEADS FOR LARGE DIAMETER AIRCRAFT ENGINES

    WIJESINGHE JANAKA / ROCHA ANDREW G / ZIMNEY ERIC J | Europäisches Patentamt | 2021

    Freier Zugriff

    Inlet bulkheads for large diameter aircraft engines

    WIJESINGHE JANAKA / ROCHA ANDREW G / ZIMNEY ERIC J | Europäisches Patentamt | 2024

    Freier Zugriff