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飞机铝合金管材拉杆收口工艺
英文标题:Closing process on pull rod for aircraft aluminum alloy pipe
作者:王强 
单位:成都飞机工业(集团)有限责任公司 
关键词:铝合金管材 拉杆 管端收口工艺 旋锻模具 轴向进给量 
分类号:TG316
出版年,卷(期):页码:2024,49(3):60-65
摘要:

针对飞机铝合金管材拉杆零件,进行管端收口工艺研究,分析工艺方案、旋锻模具设计、旋锻工艺参数设计并进行试验验证。研究结果表明:拉杆收口旋锻成形工艺相对冷挤压、热挤压成形更高效;旋锻成形过程中,实际操作的工艺参数中轴向进给量的影响起主要作用;为保证拉杆内外表面质量,避免加工缺陷,随着收口外径尺寸的减小,轴向进给量也要相应地减小。轴向进给量与模具锥角和单组径向压缩量相关,对于过渡区锥角为19°的拉杆,外圆直径为Φ35~Φ40 mm时,每组初锻轴向进给量应小于3.0 mm;当外圆直径为Φ30~Φ35 mm时,轴向进给量应小于1.8 mm;当外圆直径小于Φ30 mm时,轴向进给量应小于1.2 mm。

For the pull rod parts of aircraft aluminum alloy pipe, the pipe end closing technology was studied, and the process scheme, die design and process parameter design of rotary forging were analyzed and verified by experiments. The research shows that the rotary forging process used for pull rod is more efficient than cold extrusion and hot extrusion forming. In the process of rotary forging, the influence of axial feeding amount plays a major role in the actual operation process. In order to ensure the quality of inner and outer surfaces of pull rod and avoid the processing defect, the axial feeding amount should be reduced accordingly with the reduction of outer diameter of closing part. The axial feeding amount is related to the mold cone angle and the radial compression amount of a single group. For the pull rod with the transition zone taper of 19°, when the outside diameter of each group of initial forging is Φ35-Φ40 mm, the appropriate selection of axial feeding amount should be less than 3.0 mm; when the outside diameter is Φ30-Φ35 mm, the appropriate selection of axial feeding amount should be less than 1.8 mm; when the outside diameter is less than Φ30 mm, the appropriate selection of axial feeding amount should be less than 1.2 mm.

基金项目:
作者简介:
作者简介:王强(1972-),男,工程硕士,高级工程师,E-mail:sur.f@163.com
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