A method for joining two aircraft structural parts by a bolted or riveted joint and for preventing cracks at said joint includes a step of providing a first metallic aircraft structural part and a second aircraft structural part, wherein the first aircraft structural part includes a first joint region and a second aircraft structural part includes a second joint region. Furthermore, the method includes a step of inducing compressive residual stresses in a first area of the first joint region for preventing cracks. Finally, the method includes a step of fastening together the first and second aircraft structural parts at the first and second joint regions by a bolted or riveted joint. An aircraft including first and second aircraft structural parts is also described.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    PREVENTING CRACKS AT BOLTED OR RIVETED JOINTS OF AIRCRAFT STRUCTURAL PARTS


    Beteiligte:

    Erscheinungsdatum :

    10.03.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64C AEROPLANES , Flugzeuge



    Preventing cracks at bolted or riveted joints of aircraft structural parts

    FURFARI DOMENICO / OHRLOFF NIKOLAUS | Europäisches Patentamt | 2020

    Freier Zugriff

    Preventing cracks at bolted or riveted joints of aircraft structural parts

    FURFARI DOMENICO / OHRLOFF NIKOLAUS | Europäisches Patentamt | 2019

    Freier Zugriff


    Contact Analysis for Riveted and Bolted Joints of Composite Laminates

    Ye, T. Q. / Li, W. / Shen, G. Q. | British Library Online Contents | 1992