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航天用铝合金蒙皮拉形工艺研究
英文标题:Study on stretch forming of aluminum alloy skin for aerospace
作者:晋坤 孙秀京 尹苹 付杨 孙震 王存 马超 毛爱群 
单位:中国运载火箭技术研究院 
关键词:2A14铝合金 拉形工艺 蒙皮 力学性能 
分类号:V46
出版年,卷(期):页码:2015,40(8):47-51
摘要:
采用FET-1000T横向蒙皮拉伸成形机设备对2A14铝合金进行了蒙皮拉形工艺的研究。研究结果表明:对于单曲率蒙皮零件的成形,主要采用先预拉伸再弯曲成形后补拉伸的拉形工艺,预拉伸主要是保证成形前坯料的平直,补拉伸是为了减少零件弯曲成形后的回弹;经过预拉伸处理的蒙皮,母线直线度在0.9~1.2 mm之间,厚度在8.03~8.10 mm之间,其成形后的母线直线度大致呈现中间低两边高的现象,而厚度分布则呈现中间厚两边薄的趋势;适当的增加约0.6%的补拉伸量,既可以提高蒙皮的型面贴合度,又可以保证蒙皮的力学性能,从而达到蒙皮零件成形/成性的协同控制。
Skin stretch-forming process of aluminum alloy 2A14 was studied by FET-1000T transverse skin stretch forming equipment. The results show that the main method on forming of the single curvature skin part is first pre-stretched forming, then bending and post-stretched forming. The pre-stretching is to ensure the flat state of the material, and post-stretching can reduce the springback of skin. Through pre-stretching, the straightness of skin is within the range of 0.9 to 1.2 mm, the thickness is within the range of 8.03 to 8.10 mm; the straightness of skin is low on the center of the skin, while high in both ends of the skin; the thickness of skin is thick on the center, while thin in both ends. An appropriate increase of the amount (≈0.6%) in complementary stretching can enhance the skin profile accuracy, ensure the mechanical property, and achieve cooperative control on the skin shape and property.
基金项目:
航天科技集团重大工艺项目子课题(ZDGY2013-03)
作者简介:
晋坤(1987-),男,硕士,助理工程师
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