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The research of technological properties titanium alloy Ti-6Al-4V. Part 1. The microstructure and mechanical properties

机译:钛合金Ti-6Al-4V的工艺性能研究。第1部分。显微组织和力学性能

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The paper describes the results of comprehensive studies of the microstructure, mechanical and technological properties (formability and weldability in the solid state) of the titanium sheet alloy VT6 (Ti-6Al-4V) with improved superplastic properties produced by PSC «VSMPO?AVISMA». The first part is investigated the initial microstructure of the alloy and its mechanical properties over a wide temperature range from 650 to 900ºC at strain rates of 4×10-4, 4×10-3 4×10-2 s-1. It is found that the initial microstructure of a sheet is uniform, ultrafine grains have an average size of 1.2 microns. The initial grain size of the microstructure is found to be from 0.1 to 4 microns. Most of the grains have a size of 0.5 to 1.5 microns. Mechanical tensile tests revealed that the ultrafine grained titanium alloy has higher superplasticity characteristics as compared with the standard VT6 sheet. The microstructure of deformed samples and data on changes in the grain size depending on the temperature and strain rate are investigated. Comparing the superplastic characteristics of the samples cut along and across to the direction of rolling indicates the absence of anisotropy. The studied alloy exhibits the best superplastic properties at temperatures from 700 to 850ºC and strain rates of 4×10-4 ? 4×10-3 s-1, which corresponds to the manifestation of the low temperature superplasticity. Relative elongation at that is from 650 to 1075%, which allow recommending the development of the studied alloy for low temperature processes of superplastic forming and diffusion welding for aerospace products.
机译:本文描述了由PSC«VSMPO?AVISMA»生产的具有改善的超塑性的钛板合金VT6(Ti-6Al-4V)的组织,力学性能和技术性能(固态成形性和焊接性)的综合研究结果。 。第一部分研究了合金的初始微观结构及其在650至900ºC的宽温度范围内,应变率为4×10-4、4×10-3 4×10-2 s-1的力学性能。发现片材的初始微观结构是均匀的,超细晶粒的平均尺寸为1.2微米。发现微结构的初始晶粒尺寸为0.1至4微米。大多数晶粒的尺寸为0.5到1.5微米。机械拉伸试验表明,与标准VT6板材相比,超细晶粒钛合金具有更高的超塑性特征。研究了变形样品的微观结构以及取决于温度和应变率的晶粒尺寸变化数据。比较沿轧制方向切开的样品的超塑性特征,表明不存在各向异性。所研究的合金在700至850ºC的温度下具有最佳的超塑性,应变速率为4×10-4?。 4×10-3 s-1,对应于低温超塑性的表现。相对伸长率为650至1075%,这可以推荐开发用于低温工艺的航空航天产品超塑性成形和扩散焊接的合金。

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