本文選題：復(fù)合材料修補　切入點：電熱損傷　出處：《材料科學(xué)與工程學(xué)報》2017年06期

【摘要】：為了研究碳纖維復(fù)合材料(CFRP)修補結(jié)構(gòu)在電熱載荷環(huán)境下的沖擊性能,采用自制的電熱損傷測試平臺,測試了修補后CFRP層板在不同電流下試樣的表面溫度分布和電阻變化規(guī)律,對修補后CFRP層板進行了低速沖擊和沖擊后剩余壓縮強度(CAI)測試,并對沖擊損傷失效特征進行了對比分析。結(jié)果表明:低電流對修補后CFRP層板的抗沖擊性能影響較小,CAI呈現(xiàn)略微增長的趨勢;隨著電流強度的增加,電熱產(chǎn)生的高溫對修補界面層產(chǎn)生破壞,導(dǎo)致材料抗沖擊性能減弱,CAI明顯降低。
[Abstract]:In order to study the impact property of carbon fiber reinforced plastic (CFRP) repair structure under electrothermal load, the surface temperature distribution and resistance change of the repaired CFRP laminates under different currents were measured by using a self-made electrothermal damage test platform. The low speed impact and residual compressive strength of the repaired CFRP laminates were tested. The failure characteristics of impact damage are compared and analyzed. The results show that the impact of low current on the impact resistance of CFRP laminates is slightly increased with the increase of current intensity. The high temperature produced by electroheat destroys the interface layer, which results in the decrease of the impact resistance of the material and the decrease of CAI.
【作者單位】： 中國民航大學(xué)天津市民用航空器適航與維修重點實驗室;廣州飛機維修工程有限公司;
【基金】：中央高校基本科研業(yè)務(wù)費資助項目(3122013Z009)
【分類號】：TB33

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1 張俊;碳纖維樹脂基復(fù)合材料修補區(qū)域電熱溫度場的研究[D];中國民航大學(xué);2016年

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