期刊文献+
共找到2篇文章
< 1 >
每页显示 20 50 100
CFRP/Ti叠层构件螺旋铣孔层间孔径偏差研究 被引量:2
1
作者 邱建平 陈金祥 +3 位作者 周莹 孟宪本 杨选宏 郭飞燕 《航空制造技术》 CSCD 北大核心 2023年第9期93-98,111,共7页
螺旋铣孔是航空航天领域装配孔加工的一种新型加工工艺,与传统钻孔工艺相比,具有加工质量好、制孔效率高、刀具成本低等优势。在进行碳纤维复合材料(CFRP)/钛合金(Ti)叠层构件螺旋铣孔时,由于两种材料特性差异巨大,易导致层间出现孔径偏... 螺旋铣孔是航空航天领域装配孔加工的一种新型加工工艺,与传统钻孔工艺相比,具有加工质量好、制孔效率高、刀具成本低等优势。在进行碳纤维复合材料(CFRP)/钛合金(Ti)叠层构件螺旋铣孔时,由于两种材料特性差异巨大,易导致层间出现孔径偏差,影响制孔精度,成为螺旋铣孔技术应用过程中亟须解决的关键问题。基于便携式螺旋铣孔单元搭建了试验装置,开展了CFRP/Ti叠层构件螺旋铣孔工艺试验,分析了CFRP/Ti叠层构件螺旋铣孔层间孔径偏差的形成原因,提出了通过改变螺旋铣孔工艺参数和铣削方式减小CFRP/Ti叠层构件层间孔径偏差的工艺方法,并进行了试验验证。结果表明,变工艺参数加工可使层间孔径偏差有效降低,不超过0.02 mm。 展开更多
关键词 叠层构件 螺旋铣孔 加工精度 孔径偏差 变工艺参数加工
下载PDF
High temperature deformation behavior and optimization of hot compression process parameters in TC11 titanium alloy with coarse lamellar original microstructure 被引量:4
2
作者 鲁世强 李鑫 +2 位作者 王克鲁 董显娟 傅铭旺 《Transactions of Nonferrous Metals Society of China》 SCIE EI CAS CSCD 2013年第2期353-360,共8页
The high temperature deformation behaviors of α+β type titanium alloy TC11 (Ti-6.5Al-3.5Mo-1.5Zr-0.3Si) with coarse lamellar starting microstructure were investigated based on the hot compression tests in the tem... The high temperature deformation behaviors of α+β type titanium alloy TC11 (Ti-6.5Al-3.5Mo-1.5Zr-0.3Si) with coarse lamellar starting microstructure were investigated based on the hot compression tests in the temperature range of 950-1100 ℃ and the strain rate range of 0.001-10 s-1. The processing maps at different strains were then constructed based on the dynamic materials model, and the hot compression process parameters and deformation mechanism were optimized and analyzed, respectively. The results show that the processing maps exhibit two domains with a high efficiency of power dissipation and a flow instability domain with a less efficiency of power dissipation. The types of domains were characterized by convergence and divergence of the efficiency of power dissipation, respectively. The convergent domain in a+fl phase field is at the temperature of 950-990 ℃ and the strain rate of 0.001-0.01 s^-1, which correspond to a better hot compression process window of α+β phase field. The peak of efficiency of power dissipation in α+β phase field is at 950 ℃ and 0.001 s 1, which correspond to the best hot compression process parameters of α+β phase field. The convergent domain in β phase field is at the temperature of 1020-1080 ℃ and the strain rate of 0.001-0.1 s^-l, which correspond to a better hot compression process window of β phase field. The peak of efficiency of power dissipation in ℃ phase field occurs at 1050 ℃ over the strain rates from 0.001 s^-1 to 0.01 s^-1, which correspond to the best hot compression process parameters of ,8 phase field. The divergence domain occurs at the strain rates above 0.5 s^-1 and in all the tested temperature range, which correspond to flow instability that is manifested as flow localization and indicated by the flow softening phenomenon in stress-- strain curves. The deformation mechanisms of the optimized hot compression process windows in a+β and β phase fields are identified to be spheroidizing and dynamic recrystallizing controlled by self-diffusion mechanism, respectively. The microstructure observation of the deformed specimens in different domains matches very well with the optimized results. 展开更多
关键词 titanium alloy coarse lamellar microstructure high temperature deformation behavior processing map hot compression process parameter optimization
下载PDF
上一页 1 下一页 到第
使用帮助 返回顶部