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鈾表面Al/Ti復(fù)合鍍層熱應(yīng)力的有限元分析
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Finite Element Analysis on Thermal Stress for Al/Ti Composite Coatings on Uranium Substrate
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    摘要:

    對鈾表面Al/Ti復(fù)合鍍層的熱應(yīng)力進(jìn)行了熱彈塑性有限元分析,表明Ti鍍層內(nèi)為壓應(yīng)力,Al鍍層內(nèi)為拉應(yīng)力,并達(dá)到鋁的屈服強(qiáng)度,靠近試樣側(cè)邊,存在邊緣效應(yīng)引起的應(yīng)力分布不均勻性,離試樣側(cè)邊2倍鍍層厚度處,不均勻性逐漸消失,試樣側(cè)邊U-Al界面剪切應(yīng)力大于中部區(qū)域.對沉積溫度、鍍層厚度及鍍層力學(xué)性能對鍍層熱應(yīng)力和塑性應(yīng)變的研究表明,隨著沉積溫度升高,鍍層內(nèi)熱應(yīng)力和塑性應(yīng)變明顯增大,減薄Al鍍層和增厚Ti鍍層可降低鍍層內(nèi)熱應(yīng)力和塑性應(yīng)變,Al鍍層屈服強(qiáng)度及Ti鍍層彈性模量對鍍層熱應(yīng)力和塑性應(yīng)變有重要影響.

    Abstract:

    The thermal stress for Al/Ti coatings on uranium substrate was analyzed by using a thermal elastic plastic finite element method (FEM). The results indicate that the thermal stress is compressive inside the Ti coating and tensile inside the Al coating, which reaches the yield strength of Al. There is an uneven thermal stress distribution at the free side of specimen due to the end effect, which is vanished gradually at about 2h (where h is the coating thickness) from the free side of specimen. The shear stress of U-Al at the free side is larger than that in the middle of specimen. The effect of deposition temperature, coating thickness and mechanical properties on the thermal stress and plastic strain in coatings were also investigated. The results show that the thermal stress and plastic strain increase remarkably with the deposition temperature increasing. It is helpful to decrease the thermal stress and plastic strain by decreasing the thickness of Al coating and increasing the thickness of Ti coating. The yield strength of Al coating and the elastic modulus of Ti coating have large effects on the thermal stress and plastic strain of the coatings.

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董平 李瑞文 江帆 陳丕恒.鈾表面Al/Ti復(fù)合鍍層熱應(yīng)力的有限元分析[J].稀有金屬材料與工程,2006,35(6):885~889.[Dong Ping, Li Ruiwen, Jiang Fan, Chen Piheng. Finite Element Analysis on Thermal Stress for Al/Ti Composite Coatings on Uranium Substrate[J]. Rare Metal Materials and Engineering,2006,35(6):885~889.]
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  • 收稿日期:2005-04-08
  • 最后修改日期:2006-02-22
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