Study on Group Technologyof T-section Aluminum Alloy Profile Parts and Application
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摘要: 针对目前飞机T型材零件单件弯曲成形效率低成形精确差的问题,提出了T型材弯曲件成组拉弯成形的成组加工方法。基于截面尺寸、引导线的曲率半径等信息建立了成组分析算法,对T型材进行分组,使用长型材拉弯成形后切割分段得到符合精确外形要求的T型材零件。通过理论计算、模拟分析和拉弯试验,验证了T型材拉弯成形成组加工技术的可行性,该方法提高了零件的制造效率和成形精度,可以大幅度降低人工矫正的工作量和加工成本。Abstract: A group processing method was proposed for the problem of low forming efficiency and poor forming accuracy in single-piece stretch bending forming with T-section in this paper.Based on the section size and radius of curvature of guide line, the analysis algorithm of group technology was established. T-section profile was grouped, and the long profile was formed and cut into sections to obtain T-section parts that meet the requirements of precise shape. Through the calculation, simulation analysis, and stretch bending tests, the feasibility of the group technology of forming T-section profile by stretch bending was verified. This method can improve the manufacturing efficiency and forming accuracy of parts, and greatly reduced the workload and processing cost of manual correction.
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Key words:
- T-section profile /
- group technology /
- finite element method /
- stretch bending forming
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表 1 T型材成组化编码分类要素
Table 1. Group coding and classification elements of T profiles
Ⅰ Ⅱ Ⅲ Ⅳ Ⅴ Ⅵ 弦板
宽度弦板
厚度腹板
高度腹板
厚度长度 半径 表 2 零件编码含义
Table 2. Meaning of part coding
mm 代号 0 1 2 3 4 5 6 7 8 9 Ⅰ 50~60 60~70 70~80 80~90 90~100 100~110 110~120 120~130 130~140 140~150 Ⅱ 0~2 2~4 4~6 6~8 8~10 Ⅲ 80~140 Ⅳ 0~2 2~4 4~6 6~8 8~10 10~12 12~14 14~16 16~18 Ⅴ 1900~2000 2000~2100 2100~2200 2200~2300 2300~2400 2400~2500 2500~2600 2600~2700 2700~2800 2800~2900 Ⅵ ≤200 >200 表 3 某项目某部件T型材成组加工工装统计
Table 3. Statistics of T profile group processing tooling for a certain part of B767-300
序号 材料规格 工艺方案 成形零件项数 一次拉弯件数 1 TMS60-9399 成组加工 56 21 2 TMS60-27356 成组加工 5 22 3 TMS60-27316 成组加工 1 20 4 TMS60-25891 成组加工 2 20 表 4 某项目某部件T型材零件截面几何尺寸统计
Table 4. Statistics on the section geometrical sizes of T section of the certain part of the B767-300
规格 项数 A/ in B/ in T/ in r/ in 腹板高度/mm TMS60-27356 4 4.4 3.7 0.08 0.12 ≤125.5 TMS60-9399 16 2.2 5.15 0.1 0.13 ≤104 TMS60-27814 14 2.5 5.3 0.1 0.13 ≤105 TMS60-21666 1 2 4.1 0.08 0.125 73.5 TMS60-30966 23 3.1 4.5 0.1 0.125 ≤102 TMS60-10074 3 2.4 3.15 0.1 0.16 ≤105 TMS60-27316 1 4 5.1 0.09 0.1 86.5 表 5 某项目某部件T型材引导线几何尺寸统计
Table 5. Statistics on the section geometrical sizes of T profile guide line of the certain part of B767-300
规格 项数 长度L/mm 弯曲半径R/mm TMS60-27356 4 ≤200 1项R2450、
3项R2100TMS60-9399 16 ≤200 R2450 TMS60-27814 14 ≤200 R2450 TMS60-21666 1 ≤200 R2100 TMS60-30966 23 ≤200 R2100 TMS60-10074 3 ≤200 R2100 TMS60-27316 1 ≤200 R2450 表 6 引导线几何参数
Table 6. Geometric parameters of guide line
引导线类别 弯曲半径/mm 弯曲角度/(°) 弦长/mm R2100 2100 5.457 199.924 R2450 2450 4.677 199.945 表 7 满足成形精度引导线半径和弦长的误差、数值范围
Table 7. Error and value range of guide line radius and chord length to meet forming accuracy
引导线类别 弯曲半径误差极值/mm 弯曲半径范围/mm 弦长误差极值/mm 弦长范围/mm R2100 440.583 1659.417~2540.583 20.984 178.940~220.909 R2450 599.8332 1850.167~3049.833 24.486 175.458~224.431 表 8 引导线半径回弹前后变化
Table 8. Changes of the radius of the guide line before and after springback
试件
编号理论半径/
mm回弹后半
径/mm回弹量/
mm回弹率/
%R2000 2000 2055.24 110.47 2.7 表 9 拉弯试验回弹前后弯曲半径变化
Table 9. Change of bending radius before and after springback in stretch-bending test
试件
编号回弹前
半径/mm回弹后
半径/mm回弹量/
mm回弹率/
%半径
变化率/%R2000 2023.81 2065.56 41.75 2.1 3.3 -
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