首页> 外文期刊>JSME International Journal. Series C, Mechanical Systems, Machine Elements and Manufacturing >Fatigue Crack Propagation in Surface Film-Bonded Materials Using Pure Copper and Commercial Grade Iron Films
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Fatigue Crack Propagation in Surface Film-Bonded Materials Using Pure Copper and Commercial Grade Iron Films

机译:使用纯铜和工业级铁膜的表面结合材料中的疲劳裂纹扩展

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摘要

As model specimens of surface film-bonded materials with or without resin interlayer, pure copper or commercial grade iron films were bonded to the surface of steel base plates by epoxy resin bonding or by diffusion bonding. The film thickness was 100 and 50 μm for the copper and 100 μm for the iron, respectively. In the fatigue testing results using these specimens, very few slips were observed around the crack initiated relatively early during fatigue on the film bonded with epoxy resin, while many slips were observed during fatigue on the film bonded by diffusion. As for the fatigue life, the epoxy bonding layer restrains the fatigue crack propagation from the surface film to the inner base plate, thus increasing the fatigue crack propagation life of the film-bonded plates with epoxy resin. In this connection, both the compressive residual stress on the iron film and the smaller tensile residual stress on the thinner copper film increased the fatigue crack propagation life significantly as compared with the larger tensile residual stress on the thicker copper film. Finally, the effect of the epoxy bonding layer on the fatigue crack propagation rate of the surface film was discussed in terms of the measured crack opening displacement range at 250 μm from behind the crack tip, Δφ_(250).
机译:作为具有或不具有树脂夹层的表面膜结合材料的模型样品,通过环氧树脂结合或通过扩散结合将纯铜或工业级铁膜结合至钢板基板的表面。铜的膜厚度为100μm,铁的膜厚度为100μm。在使用这些样品的疲劳测试结果中,观察到在与环氧树脂粘合的膜上的疲劳期间相对较早开始的裂纹周围的滑移很少,而在通过扩散粘合的膜上的疲劳期间观察到许多滑移。关于疲劳寿命,环氧树脂接合层抑制了疲劳裂纹从表面膜向内部基板的传播,从而延长了具有环氧树脂的膜接合板的疲劳裂纹传播的寿命。就此而言,与较厚的铜膜上的较大的残余拉伸应力相比,铁膜上的压缩残余应力和较薄的铜膜上的较小拉伸残余应力均显着提高了疲劳裂纹扩展寿命。最后,从裂纹尖端后方在250μm处测得的裂纹开口位移范围Δφ_(250),讨论了环氧粘结层对表面膜疲劳裂纹扩展速率的影响。

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