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LY12合金翼片等温模锻的缺陷分析

DEFECTS ANALYSIS OF LY12 ALLOY WING IN ISOTHERMAL FORGING
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摘要 简要叙述了大型薄腹板筋型翼片件,在5×10~4kN液压机上采用等温模锻工艺方案的可行性和等温模锻的变形温度、应变速率等工艺参数。分析了翼片等温模锻时产生穿筋、缩孔、折叠和裂纹等各种缺陷的原因。经试验确定了消除各种缺陷的实用方法,选择合理的模具结构设计和最佳的坯料外形、尺寸制备等。用CAD方法可得到较为理想的等效高度坯料和模具型槽中设计较为实用而又经济的工艺余料孔。 The paper briefly describes the geometric structure characteristics of large wing with thin webs, and the possibility of isothermal forging technology of wing is used in 5 × 104 kN hydraulic press. The technological parameters of isothermal forging such as its deformation temperature, strain rate and so on are introduced. The paper also analyses the causes of defects in detail such as pierce rib, strinkage cavity, lap and crack, and so on. The practical methods to remove these defects by lots of technological tests are given. Meanwhile, it points out that in order to avoid or reduce the defects, it is important to determine the die structure, optimum shapes and size of blank in the small serial production with the help of CAD. The suitable equivalent height blank and the practical and inexpensive holes for excess metal in dies cavity can be obtained.
出处 《航空学报》 EI CAS CSCD 北大核心 1993年第6期B313-B316,共4页 Acta Aeronautica et Astronautica Sinica
关键词 铝合金 翼片 等温模锻 缺陷分析 the wing of aluminium alloy, isothermal forging, defects analysis
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参考文献5

  • 1刘润广,王仲仁,刘海华,马二建,张希宇,邓少平,尚秀田,徐福昌,苗启彬.铝合金Ly12超塑等温变形时力学行为的研究[J].航天工艺,1991(3):6-11. 被引量:1
  • 2刘润广,航天工艺,1988年,3期,27页
  • 3吕炎,锻压工艺学,1983年
  • 4刘润广,导弹技术,1981年,2期,15页
  • 5团体著者,有色金属锻造,1979年

二级参考文献1

  • 1刘玉文,刘文俊,赵庭良,王少林,李延仁,夏晓文,魏德生.供应状态铝合金LY12超塑性的研究[J]吉林工业大学学报,1983(02).

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