航空学报 > 1993, Vol. 14 Issue (6): 313-316

LY12合金翼片等温模锻的缺陷分析

刘润广1, 王仲仁1, 张希宁2, 邓少平2   

  1. 1. 哈尔滨工业大学锻压教研室,哈尔滨 150006;2. 北京航星机器制造公司冶金工艺所,北京 100013
  • 收稿日期:1991-06-07 修回日期:1991-12-24 出版日期:1993-06-25 发布日期:1993-06-25

DEFECTS ANALYSIS OF LY12 ALLOY WING IN ISOTHERMAL FORGING

Liu Run-guang1, Wang Zhong-ren Zhang Xi-ning1, Deng Shao-ping2   

  1. 1. Harbin Institute of Technology Forging and Stamping Faculty Harbin, 150006;2. Beijing Hang Xing machine manufacturing Company metallurgy Technology Institute, Beijing, 100013
  • Received:1991-06-07 Revised:1991-12-24 Online:1993-06-25 Published:1993-06-25

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。

关键词: 铝合金翼片, 等温模锻, 缺陷分析

Abstract: 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.

Key words: the wing of aluminium alloy, isothermal forging, defects analysis