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Fatigue Crack Propagation Behavior in Surface Film-Bonded Materials with Resin Bonding layer

机译:具有树脂粘结层的表面膜粘结材料的疲劳裂纹扩展行为

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摘要

Surface film-bonded materials with resin interlayer are often used in electronic parts, fatigue properties of which have to be discussed in order to maintain the expected electronic function without fracture during operating. In this study, pure copper and commercial grade iron films with the thickness of 100 mum were bonded to the surface of carbon steel base plate by epoxy resin adhesive or by diffusion. As a result of fatigue testing, there was a tendency for the epoxy-bonding layer to restrict fatigue crack propagation from the surface film to inner base plate. In addition, the epoxy-bonded iron film had a compressive residual stress and also caused smaller stress amplitude in the inner base plate between films, so that the fatigue life of the epoxy-bonded plate was longer for the iron film than for the copper film. The fatigue crack propagation rate, da/dN, for all the film-bonded plates was expressed by a power law of the measured crack opening displacement range, DELTA PHI_(250), as well as for several metal base plates, although the fatigue crack on the epoxy-bonded film propagated at the low value of DELTA PHI_(250) in which the fatigue crack did not propagate for the diffusion-bonded plate and the base plates.
机译:具有树脂夹层的表面膜粘结材料通常用于电子零件,必须讨论其疲劳特性,以保持预期的电子功能而不会在操作过程中破裂。在这项研究中,通过环氧树脂粘合剂或扩散法将厚度为100微米的纯铜和商品级铁膜粘合到碳钢基板的表面。作为疲劳试验的结果,环氧粘合层存在限制疲劳裂纹从表面膜向内部基板的扩展的趋势。另外,环氧粘结铁膜具有压缩残余应力,并且在膜之间的内部基板中引起较小的应力振幅,因此铁膜的环氧粘结板的疲劳寿命比铜膜的疲劳寿命长。 。尽管疲劳裂纹是通过疲劳裂纹扩展速率,但对于所有薄膜粘合板,其疲劳裂纹扩展速率da / dN均由所测裂纹开口位移范围DELTA PHI_(250)以及多个金属基板的幂定律表示。在以ΔPHI_(250)的低值传播的环氧粘合膜上,在扩散粘合板和基板上疲劳裂纹没有传播。

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