2005
DOI: 10.1111/j.1460-2695.2005.00938.x
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Fatigue of single‐ and double‐rivet self‐piercing riveted lap joints

Abstract: A B S T R A C T The fatigue behaviour of single-and double-rivet aluminum alloy 5754-O self-piercing riveted (SPR) lap joints has been investigated experimentally and analytically. With the single rivet, the experimental program involves a set of 27 cyclic tension tests on joints with 1-, 2-or 3-mm-thick sheet coupons. In most cases (85%), fatigue cracks are found to initiate in the gross section on the faying surface of the upper sheet. With two rivets (installed in two rows), the experimental program consist… Show more

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Cited by 61 publications
(38 citation statements)
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“…They concluded that the rate of increase of the static and fatigue strength differed as the prestraining levels varied. Iyer et al [39] found both the fatigue and static strength of double-rivet SPR joints to be strongly dependent on the "orientation combination" of the rivets.…”
Section: Self-piercing Rivetingmentioning
confidence: 99%
“…They concluded that the rate of increase of the static and fatigue strength differed as the prestraining levels varied. Iyer et al [39] found both the fatigue and static strength of double-rivet SPR joints to be strongly dependent on the "orientation combination" of the rivets.…”
Section: Self-piercing Rivetingmentioning
confidence: 99%
“…SPR is widely used by several automotive manufacturers as an economical and effective technique to join aluminum vehicle bodies [6][7][8][9]. SPR joints of aluminum to aluminum [6,[10][11][12][13][14], magnesium to magnesium [15], and aluminum to steel [16][17][18] alloys have shown superior peel and fatigue strength compared to RSW joints. Unlike welding, SPR does not involve any heating or melting of material, nor does it require additional manufacturing processes, like pre-drilling holes, which could add additional manufacturing time and cost [5].…”
Section: Introductionmentioning
confidence: 99%
“…The fatigue behavior of single and double riveted joints made from aluminum alloy 5754-O has been studied by Iyer et al (Iyer et al, 2005). A 3D elastic FEA showed that crack initiation occurred at the region of maximum tensile stress.…”
Section: Finite Element Analysis -From Biomedical Applications To Indmentioning
confidence: 99%