(燕山大學(xué) 先進(jìn)鍛壓成形技術(shù)與科學(xué)教育部重點(diǎn)實(shí)驗(yàn)室,秦皇島 066004)
摘 要: 輕質(zhì)薄壁件越來(lái)越多地應(yīng)用于航空、航天和汽車(chē)等高新技術(shù)工程領(lǐng)域,但起皺失穩(wěn)一直是薄壁件成形過(guò)程中主要的缺陷之一。因此,輕質(zhì)薄壁件成形過(guò)程中的塑性失穩(wěn)起皺預(yù)測(cè)研究就顯得尤為重要。本文針對(duì)塑性成形中薄壁管件結(jié)構(gòu)由于存在多種初始缺陷(如厚度不均,尺寸偏差等)從而導(dǎo)致失穩(wěn)模擬預(yù)測(cè)與實(shí)際情況不符的現(xiàn)象,以AA6061固體顆粒介質(zhì)管材縮徑工藝為算例,結(jié)合ABAQUS中最適合復(fù)雜接觸工況的DYNAMIC算法以及Draker-Pager顆粒介質(zhì)成形數(shù)值模擬模型,對(duì)無(wú)初始缺陷圓柱殼體、引入屈曲模態(tài)初始缺陷圓柱殼體、引入厚度不均初始缺陷圓柱殼體以及同時(shí)引入屈曲模態(tài)和厚度不均缺陷的圓柱殼體進(jìn)行了縮徑成形模擬,將四種條件下的管件失穩(wěn)波形模擬結(jié)果與試驗(yàn)結(jié)果進(jìn)行了比較。結(jié)果表明:同時(shí)引入屈曲模態(tài)和厚度不均缺陷的動(dòng)態(tài)顯示有限元法可以準(zhǔn)確預(yù)測(cè)出管材縮徑失穩(wěn)后的形貌,并將模擬仿真與實(shí)驗(yàn)的應(yīng)力-位移曲線進(jìn)行對(duì)比,驗(yàn)證了此模擬方法的可靠性。
關(guān)鍵字: 管材縮徑;起皺失穩(wěn)數(shù)值模擬;屈曲模態(tài);厚度缺陷
(Key Laboratory of Advanced Forging & Stamping Technology and Science of Ministry of Education, Yanshan University, Qinhuangdao 066004, China)
Abstract:The lightweight thin-walled parts are increasingly used in high-tech engineering fields such as aviation, aerospace and automobile. Wrinkling instability has always been one of the major defects in thin-walled parts forming processes. Therefore, the study on prediction of plastic wrinkling instability becomes particularly important in the process of forming lightweight thin-walled parts. Based on the inconsistent between the instability simulation prediction of thin-walled tube structures and the actual situation which are due to various initial defects (such as uneven thickness, dimensional deviations, etc.), this paper takes the example of the AA6061 diameter-reduced tubes by solid granule medium forming technology and combines the DYNAMIC algorithm which is the most suitable for complex contact conditions in ABAQUS, simulates the tube outer pressure compression forming with no initial imperfections, buckling modes initial imperfections, uneven thickness initial imperfections and the last one which contains buckling modes initial imperfections and uneven thickness initial imperfections. The dynamic finite element method with simultaneous introduced buckling modes and thickness unevenness imperfections can accurately predict the instability waveforms of the tube through the comparison between the simulations and the tests. The reliability of the simulation method is verified through the comparison between the simulative and experimental force-displacement curves.
Key words: tube outer pressure compression forming; numerical simulation of wrinkling instability; buckling mode; thickness imperfection


