网站首页期刊简介编委会过刊目录投稿指南广告合作征订与发行联系我们English
WSTi3515S阻燃钛合金热暴露性能
英文标题:Heat exposure property of burn-resistant titanium alloy WSTi3515S
作者:马凡蛟 赖运金 辛社伟 王晓亮 张平祥 王标 钟燕 
单位:西部超导材料科技股份有限公司 西北有色金属研究院 中国燃气涡轮研究院 
关键词:WSTi3515S钛合金 阻燃钛合金 热暴露性能 热稳定性能 高温拉伸性能 
分类号:TG146.2+3
出版年,卷(期):页码:2017,42(5):147-151
摘要:
对WSTi3515S合金板坯试样进行550 ℃/100 h/AC热暴露试验后,分别在室温和100 ℃下测试其拉伸性能;未经过热暴露的试样,分别在从室温到550 ℃的不同温度点测试了其拉伸性能。结果表明:经过热暴露后的试样,受到析出相强化的作用,强度略有提高,但塑性指标均存在明显下降,其中,100 ℃时的拉伸强度低于室温拉伸性能,塑性有所提高,但仍比未经过热暴露的试样测试结果低;热暴露时,晶界处析出第二相是WSTi3515S合金的关键特征,也是WSTi3515S合金热稳定性能降低的原因;在试验温度提高的情况下,光滑拉伸试样强度不断降低,塑性先上升后降低;缺口拉伸试样强度持续下降,塑性没有明显变化,弹性模量持续下降。
The tensile properties of alloy WSTi3515S slab samples were tested at room temperature and 100 ℃ after 550 ℃/100 h/AC heat exposure test. The tensile properties were tested at different temperatures from room temperature to 550 ℃ without heat exposure test. The results show that by the precipitation strengthening effect, the tensile strength of sample after heat exposure is slightly improved, but the plasticity is obviously decreased. However, the tensile strength at 100 ℃ is lower than that at room temperature, and the plasticity is higher. But it is still lower than the sample without heat exposure test. Furthermore, during heat exposure test, the second phase precipitated at grain boundary is the key feature of alloy WSTi3515S. It is also the reason for the decrease of the thermal stability of alloy WSTi3515S. Under improving the test temperature, the strength of the smooth tensile specimen decreases and the plasticity increases first and then decreases, while the strength of the notched tensile specimen decreases continually, the plasticity does not change obviously, and the elastic modulus decreases continually.
基金项目:
陕西省科技统筹创新工程计划(2016KTCQ01-100);陕西省科技统筹创新工程计划(2016KTCQ01-81)
作者简介:
马凡蛟(1985-),男,硕士,工程师
参考文献:


[1]赖运金, 张平祥, 王凯旋,等. Ti-V-Cr系阻燃钛合金厚板组织与力学性能对比研究[J]. 材料导报,2016, 30 (10): 57-61.Lai Y J, Zhang P X, Wang K X, et al. A comparative study about microstructure and mechanical properties of Ti-V-Cr type burn-resistant titanium alloy slabs [J]. Materials Review, 2016, 30 (10): 57-61.
[2]刘全明,张朝晖,刘世锋, 等. 钛合金在航空航天及武器装备领域的应用与发展[J]. 钢铁研究学报,2015, 27(3):1-4.Liu Q M, Zhang Z H, Liu S F, et al. Application and development of titanium alloy in aerospace and military hardware[J]. Journal of Iron and Steel Research, 2015, 27(3):1-4.
[3]赖运金,张平祥,辛社伟, 等. 国内阻燃钛合金工程化技术研究进展[J]. 稀有金属材料与工程, 2015, 44(8): 2067-2073.Lai Y J, Zhang P X, Xin S W, et al. Research progress on engineered technology of burn-resistant titanium alloys in China[J]. Rare Metal Materials and Engineering, 2015, 44(8): 2067-2073.
[4]张鹏,朱强,秦鹤勇, 等. 航空发动机用耐高温材料的研究进展[J]. 材料导报,2014,28(11):27-31,37.Zhang P, Zhu Q, Qin H Y, et al. Research progress of high temperature materials for aero-engines [J]. Materials Review,2014,28(11):27-31, 37.
[5]Lai Y J, Zhang P X, Zhang X M, et al. Physical properties of WSTi3515S burn-resistant titanium alloy[J]. Rare Metals,2016, 35(5):361-366.
[6]赖运金,张维,王晓亮, 等. WSTi3515S阻燃钛合金的工程化制备及力学性能研究[J]. 钛工业进展,2015, 32(6):13-18.Lai Y J, Zhang W, Wang X L, et al. Industrial manufacturing and mechanical properties of WSTi3515S burn-resistant titanium alloy [J]. Titanium Industry Progress, 2015, 32(6):13-18.
[7]赵红霞,黄旭,王宝, 等. 热处理对Ti-35V-15Cr-0.15Si-0.05C合金热稳定性能的影响[J]. 材料工程,2013,(7):73-77.Zhao H X, Huang X, Wang B, et al. Effect of heat-treatment on the microstructure and thermal stability properties of Ti-35V-15Cr-0.15Si-0.05C titanium alloy [J]. Journal of Materials Engineering, 2013, (7):73-77.
[8]赖运金,张平祥,辛社伟, 等. 热处理对WSTi3515S合金组织和性能的影响[J]. 稀有金属材料与工程,2015,44(6):1469-1473.Lai Y J, Zhang P X, Xin S W, et al. Effect of heat treatment on microstructure and mechanical properties of WSTi3515S alloy[J]. Rare Metal Materials and Engineering, 2015, 44(6):1469-1473.
[9]舒滢,黄张洪,彭雯雯,等. 铸态Ti40阻燃钛合金高温拉伸力学性能及断裂行为研究[J]. 材料导报,2014, 28(20):84-87.Shu Y, Huang Z H, Peng W W, et al. High temperature tensile mechanical properties and fracture behavior of as-cast Ti40 burn resistant titanium alloy[J]. Materials Review,2014, 28(20):84-87.
[10]张文泉,王俊英,张学昆. 金属材料拉伸试验的缺口效应[J]. 理化检验:物理分册,2008, 44(10):533-535.Zhang W Q, Wang J Y, Zhang X K. Notch effect of metallic material during tensile testing [J]. Physical Testing and Chemical Analysis Part A:Physical Testing,2008, 44(10):533-535.
[11]宋迎东,胡绪腾,刘华翔. 钛合金缺口试样拉伸破坏载荷预测[J]. 南京航空航天大学学报,2014, 46(4):487-493.Song Y D, Hu X T, Liu H X. Prediction of broken load for notched specimen of titanium alloy [J]. Journal of Nanjing University of Aeronautics & Astronautics, 2014, 46(4):487-493.
[12]刘海军,曹睿,何洪, 等. K418合金缺口敏感性研究[J]. 稀有金属,2010, 34(5):69-74.Liu H J, Cao R, He H, et al. Notch sensitivity of K418 alloy [J]. Chinese Journal of Rare Metals, 2010, 34(5):69-74.

服务与反馈:
文章下载】【加入收藏
《锻压技术》编辑部版权所有

中国机械工业联合会主管  中国机械总院集团北京机电研究所有限公司 中国机械工程学会主办
联系地址:北京市海淀区学清路18号 邮编:100083
电话:+86-010-82415085 传真:+86-010-62920652
E-mail: fst@263.net(稿件) dyjsjournal@163.com(广告)
京ICP备07007000号-9