A New Restraint for High-Load-Transfer Fastener Fatigue Test

    Volume 22, Issue 1 (January 1994)

    ISSN: 0090-3973

    CODEN: JTEOAD

    Page Count: 3


    Yigang, Z
    Research engineer and senior research engineers, Beijing Institute of Aeronautical Materials, Beijing,

    Xueren, W
    Research engineer and senior research engineers, Beijing Institute of Aeronautical Materials, Beijing,

    Yongan, Y
    Research engineer and senior research engineers, Beijing Institute of Aeronautical Materials, Beijing,

    (Received 8 April 1992; accepted 4 June 1993)

    Abstract

    A test somewhat different from the MIL-STD-1312 test 21 (Shear Joint Fatigue-Constant Amplitude) was explored by using a new type of restraint. Rivet fasteners of two kinds of materials were tested under constant amplitude fatigue loading. The new restraint facilitated the test program and reduced the bending load more efficiently than the current method. Fatigue behavior of aluminum alloy and high-strength steel with single-lap rivet fastener specimens was investigated under different load levels.


    Paper ID: JTE12636J

    DOI: 10.1520/JTE12636J

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    Author
    Title A New Restraint for High-Load-Transfer Fastener Fatigue Test
    Symposium , 0000-00-00
    Committee A01D20D30E08E17E28F08