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Texture studies of hot compressed near alpha titanium alloy (IMI 834) at 1000°C with different strain rates

机译:不同应变速率下在1000°C下热压近α钛合金(IMI 834)的织构研究

摘要

IMI 834 Titanium alloy is a near alpha (hcp) titanium alloy used for high temperature applications with the service temperature up to 600°C. Generally, this alloy is widely used in gas turbine engine applications such as low pressure compressor discs. For these applications, good fatigue and creep properties are required, which have been noticed better in a bimodal microstructure, containing 15-20% volume fraction of primary alpha grains (αp) and remaining bcc beta (β) grains transformed secondary alpha laths (αs). The bimodal microstructure is achieved during processing of IMI 834 in the high temperature α+β region. The major issue of bimodal IMI 834 during utilization is its poor dwell fatigue life time caused by textured macrozones. Textured macrozone is the spatial accumulation of similar oriented grains in the microstructure generated during hot processing in the high temperature α+β region. Textured macrozone can be mitigated by controlling the hot deformation with certain strain rate under stable plastic conditions having β grains undergoing dynamic recrystallization. Hence, a comprehensive study is required to understand the deformation behavior of α and β grains at different strain rates in that region. Hot compression tests up to 5°% strain of the samples are performed with five different strain rates i.e. 10-3 s-1, 10-2 s-1, 10-1 s-1, 1 s-1 and 10 s-1 at 1000°C using Gleeble 3800. The resultant bimodal microstructure and the texture studies of primary alpha grains (αp) and secondary alpha laths (αs) are carried out using scanning electron microscopy (SEM)-electron back scattered diffraction (EBSD) method.
机译:IMI 834钛合金是一种近α(hcp)钛合金,用于高温应用,工作温度高达600°C。通常,这种合金广泛用于燃气涡轮发动机应用中,例如低压压缩机盘。对于这些应用,要求具有良好的疲劳和蠕变性能,这在双峰微结构中表现得更好,双峰微结构包含体积分数为15-20%的初生α晶粒(αp)和剩余的bcc beta(β)晶粒转变为次生alpha条带)。在IMI 834的高温α+β区加工过程中实现了双峰微观结构。使用过程中,双峰IMI 834的主要问题是由织构大区引起的较差的保压疲劳寿命。纹理大区是在高温α+β区热加工过程中产生的微观结构中类似取向晶粒的空间累积。在稳定的,具有β晶粒动态再结晶的塑性条件下,通过以一定的应变率控制热变形,可以减轻织构的大区。因此,需要进行全面的研究以了解该区域不同应变速率下α和β晶粒的变形行为。使用五个不同的应变率(即10-3 s-1、10-2 s-1、10-1 s-1、1 s-1和10 s-1)执行高达5%应变的热压缩测试使用Gleeble 3800在1000°C下进行。使用扫描电子显微镜(SEM)-电子背散射衍射(EBSD)方法进行了初生α晶粒(αp)和次生α板条(αs)的双峰微观结构和织构研究。

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