共查询到19条相似文献,搜索用时 62 毫秒
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分析了铝合金锥形筒锻件的自由锻造生产工艺的弊端,研究和确定模锻生产工艺参数,使产品的各项技术指标均达到用户的要求。 相似文献
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介绍了2A14铝合金U型模锻件的生产工艺,针对该模锻件的材料特性、锻件的结构特点和技术要求,确定了锻造工艺。经过生产验证,制定的锻造工艺是合理的,成功地生产出了外形尺寸、组织和性能均合格的2A14铝合金U型模锻件。 相似文献
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为了揭示叶轮件模锻成形过程中金属的变形流动规律,采用有限元模拟对不同形状坯料成形过程的塑性变形流动行为进行对比分析.结果表明:叶片处是较难以充填成形的部位,且随着截面位置的下移,金属向该处型腔充填流动的趋势更为显著;与圆柱形坯料相比,阶梯形坯料成形过程中叶片部位更易于被充填成形,金属流动的均匀性也较好;通过工艺实验验证了利用阶梯形坯料可一次性成形出尺寸精度和性能均符合设计要求的叶轮锻件. 相似文献
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铝合金薄壁壳体件是航空航天及兵器工业上广泛采用的零件,但其制造工艺却长期得不到有效解决。文章采用Anycasting和DEFORM-3D软件,分别对充型阶段的凝固和塑性变形阶段进行了计算,并通过复合加载保证了零件使用性能上的要求。结果表明,模具和浇注温度越高,则凝固时间越长,且模具温度的影响要大于浇注温度的影响;在保证铝液完全充填型腔的前提下,充分考虑了模具的使用寿命和铝合金熔化温度的要求,进行了模具温度和浇注温度的优化;采用复合加载来代替简单加载可以有效地提高制件密度,使零件性能趋于均匀化。 相似文献
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将Al-1.8Cu-0.4Mg-0.4Mn合金进行50%、60%、70%、80%不同压下量的一次冷轧,随后分别将一次冷轧压下率为50%和70%的样品进行等温中间退火并进行80%压下率的二次冷轧,对其织构演变过程进行研究。研究结果表明,当压下量大于60%时,一次冷轧的样品呈现“铜式”织构特征,即在α、β取向线上分布G、B、C及S组分,C、B和S组分强度随变形量的增加而增大,G组分则先增大后减小,在70%变形量时达最大。中间退火再结晶织构较弥散,但中间退火对二次冷轧织构有较大影响。初次冷轧变形量50%的样品形成弱的{001}<110>旋转立方织构,初次冷轧变形量70%的样品形成“铜式”织构。 相似文献
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Defect analysis of complex-shape aluminum alloy forging 总被引:1,自引:0,他引:1
The isothermal precision forging was applied for the purpose of forming aluminum alloy with complex shape. The complexity of forging is easy to lead to the occurrence of the defects, such as underfilling, folding, metal flow lines disturbance and fibre breaking. The reasons for the defects were analyzed on the basis of experiments and finite element method(FEM). The results show that the size of flash gutter bridge, the lubricating condition and the deformation process are the main factors influencing the filling qualities of complex-shape aluminum alloy forging. The folding defect is mainly caused by different velocities of filling cavities, fast flow of much metal in one direction and confluence of two or multi metal strands. Improper metal distribution in different regions can cause the flow lines "disturbance and fast metal flow in one direction is also a cause of the flow lines disturbance According to the reasons, some measures were taken to improve the quality of the forged parts.These studies can contribute to offering some experiences in making process project and optimizing the process parameters for forging complex-shape aviation products. 相似文献