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EFFECTS OF INTERLAYER RESIN BONDING ON FATIGUE CRACK INITIATION/PROPAGATION IN LAMINATE MATERIALS WITH A SURFACE LAYER OF COPPER FILM

机译:中间层树脂粘合对铜膜表面层层压材料疲劳裂纹萌生/繁殖的影响

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As model specimens to examine the effects of interlayer resin bonding on fatigue properties in laminate materials with a surface film, pure copper films with a thickness of 100μm and 50μm were bonded with epoxy resin to steel base plates. The fatigue crack propagation from the notch root of the specimen was slower for the epoxy-bonded film than for the base specimen, because the epoxy bonding interlayer restricted crack propagation from the surface film to the inner base plate. On the epoxy-bonded film, however, many fatigue cracks initiated at multiple sites sufficiently away from the notch root, and propagated only on the surface copper film. In addition, the number of these multiple fatigue cracks, caused mostly at the site of the annealing twin boundaries, was larger on the surface copper film with a thickness of 100μm than 50μm.
机译:作为模型试样,以检查层间树脂键合对具有表面膜的层压材料中疲劳性能的影响,厚度为100μm和50μm的纯铜膜与环氧树脂键合到钢基板上。来自试样的缺口根的疲劳裂纹裂缝繁殖对于环氧键合薄膜比对于基本样本较慢,因为环氧键合层间层间隔从表面膜被限制到内部基板的裂纹传播。然而,在环氧键合膜上,在多个位点引发的许多疲劳裂缝足以远离凹口根,并仅在表面铜膜上传播。另外,这些多次疲劳裂缝的数量大多在退火双界的位点上引起的,在表面铜膜上较大,厚度为100μm小于50μm。

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