Inhibiting plastic tensile instability of non-symmetric thin-walled shell component via increasing regional metal inflow based on heterogeneous pressure-carrying medium

IF 5.3 1区 工程技术 Q1 ENGINEERING, AEROSPACE Chinese Journal of Aeronautics Pub Date : 2024-01-01 DOI:10.1016/j.cja.2023.05.014
Nan XIANG , Yiquan SHU , Pengyi WANG , Menghan YANG , Haoran WANG , Tao HUANG , Junqing GUO , Fuxiao CHEN
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Abstract

Heterogeneous pressure-carrying medium was employed to establish a differentiated pressure field on sheet metal in flexible die forming process in this work, which aimed at matching the non-symmetric shape of target component and improving metal inflow to avoid local tensile instability. Specifically, metal inflow corresponding to the differentiated pressure field was analytically evaluated. Forming of a typical non-symmetric shell component was experimentally and numerically studied based on the proposed method. Compared with forming processes based on the uniform pressure, difference of metal inflow in two sides of the non-symmetric component increased from 2.16 mm to 3.36 mm and metal inflow in critical region increased by 11.9% when differentiated pressure field (taking heterogeneous elastomer #4–3 for example) was employed. The resultant maximum thinning ratio decreased by 4.2% and the uniformity of shell thickness increased by 16.9%. With the decrease of Shore hardness of elastomer in the formed region, stress path in the ready-to-form region transferred towards the bi-axial tension stress state, i.e., stress ratio (α) increased. And, stress triaxiality (η) in characteristic regions were regulated appropriately, which decreased the risk of tensile instability. It was attributed to the decreased normal pressure and frictional resistance at sheet/elastomer interface in the formed region.

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基于非均质载压介质增加区域金属流入抑制非对称薄壁壳构件塑性拉伸失稳
本研究采用异质载压介质,在柔性模塑成型工艺中对金属板材建立差异化压力场,旨在匹配目标部件的非对称形状,改善金属流入量,避免局部拉伸不稳定性。具体而言,我们对与分化压力场相对应的金属流入量进行了分析评估。根据所提出的方法,对典型非对称壳体部件的成形进行了实验和数值研究。与基于均匀压力的成形过程相比,采用分压场(以异质弹性体 #4-3 为例)时,非对称部件两侧的金属流入量差值从 2.16 mm 增加到 3.36 mm,临界区的金属流入量增加了 11.9%。因此,最大减薄率降低了 4.2%,壳体厚度的均匀性提高了 16.9%。随着成型区域弹性体邵氏硬度的降低,准备成型区域的应力路径向双轴拉伸应力状态转移,即应力比 (α)增加。特征区域的应力三轴性(η)得到了适当的调节,从而降低了拉伸不稳定性的风险。这归因于成型区域板材/弹性体界面的法向压力和摩擦阻力减小。
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来源期刊
Chinese Journal of Aeronautics
Chinese Journal of Aeronautics 工程技术-工程:宇航
CiteScore
10.00
自引率
17.50%
发文量
3080
审稿时长
55 days
期刊介绍: Chinese Journal of Aeronautics (CJA) is an open access, peer-reviewed international journal covering all aspects of aerospace engineering. The Journal reports the scientific and technological achievements and frontiers in aeronautic engineering and astronautic engineering, in both theory and practice, such as theoretical research articles, experiment ones, research notes, comprehensive reviews, technological briefs and other reports on the latest developments and everything related to the fields of aeronautics and astronautics, as well as those ground equipment concerned.
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Editorial Board - Inside Front Cover Table of Content Inhibiting plastic tensile instability of non-symmetric thin-walled shell component via increasing regional metal inflow based on heterogeneous pressure-carrying medium Technologies and studies of gas exchange in two-stroke aircraft piston engine: A review Mechanism of capture section affecting an intake for atmosphere-breathing electric propulsion
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