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Superplastic Properties of γ+α_2 Titanium Aluminide Alloy Ti-43Al-(Nb,Mo,B) in Cast + Post-Solidification Heat Treated Condition

机译:铸造+后凝固耐热处理条件下γ+α_2铝化铝合金铝化铝合金Ti-43Al-(Nb,Mo,B)的超塑性

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A novel approach to fabrication of globularized fine-grained structure in γ+α_2 titaniumaluminide alloys has been proposed. The approach included the use of a specially designed alloyTi-43Al-X(Nb,Mo,B) and heat treatment. It was found that the ingot structure of the alloy might bepartially globularized on a scale of bulk material using only globularization anneal excluding any hotworking procedure. The microstructure and tensile mechanical properties of the alloy in the cast +heat treated condition were investigated. The tensile mechanical tests were performed in air in thetemperature range of T=900-1130°C at an initial strain rate of ε=1.7×10~(-4)s~(-1).High elongation(δ=160-230%) and low flow stresses (σ=36-100 MPa) typical of superplastic behavior were measuredat T=1050-1 130°C. It was demonstrated that the sheet material produced by spark cutting of the cast +heat treated alloy might be successfully hot formed.
机译:已经提出了一种在γ+α_2钛合金IDE合金中制备球状细粒化结构的新方法。该方法包括使用专门设计的合金-43Al-X(Nb,Mo,B)和热处理。发现合金的铸锭结构可能在散装材料的等级上脱落,只使用外球形退火,不包括任何热工程序。研究了铸造+热处理条件下合金的微观结构和拉伸力学性能。以ε= 1.7×10〜(-4)〜(-1)的初始应变速率,在T = 900-1130℃的测量范围内的空气中进行拉伸机械试验。高伸长率(Δ= 160-230 %)和低流量应力(σ= 36-100MPa)的超塑性行为的典型测量为T = 1050-1130℃。证明,通过火花切割生产的铸+热处理合金的片材可以成功形成。

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