首页|Ti2AlNb合金在不同温度下的热盐腐蚀行为

Ti2AlNb合金在不同温度下的热盐腐蚀行为

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为提高Ti2AlNb合金作为航空发动机部件在海洋环境下服役的可靠性,研究名义成分为Ti-22Al-23Nb-1Mo-1Zr(原子分数/%)的Ti2AlNb合金在550,650,750℃时涂盐Na2SO4/NaCl(95/5,质量比)的热腐蚀行为,绘制不同温度下合金的腐蚀增重曲线,通过X射线衍射(XRD)、扫描电子显微镜(SEM)、能谱仪(EDS)对热盐腐蚀后合金的表面形貌、截面结构以及腐蚀产物进行观察分析.结果表明:550℃时合金腐蚀速率较低,表面氧化层平直、致密且完整,表现出优异的抗热盐腐蚀能力;650℃时合金腐蚀增重曲线符合抛物线规律,氧化层表面发生小范围的剥落,内部出现裂缝且有轻微的分层现象,合金整体上表现出良好的抗热盐腐蚀能力;750℃时合金腐蚀过程中出现明显减重,氧化层表面严重开裂剥落,内部出现明显的层状结构,由两种腐蚀产物层交替叠加:其中主要腐蚀产物层以TiO2为主并含有NbAlO4等多种腐蚀产物,另一层以NaNbO3为主,合金的抗热盐腐蚀能力严重下降.
Hot salt corrosion behavior of Ti2AlNb alloys at different temperatures
To enhance the reliability of Ti2AlNb alloys as an aerospace engine component in marine environments,the hot salt corrosion behavior of Ti2AlNb alloy with nominal compositions of Ti-22Al-23Nb-1Mo-1Zr(atom fraction/%) coated with Na2SO4/NaCl(95/5,mass ratio)at temperatures of 550,650 ℃ and 750 ℃ was investigated. The corrosion mass gain curves of alloys at different temperatures were drawn. The surface morphologies,cross-section structures,and corrosion products of the alloy after hot salt corrosion were examined and analyzed by X-ray diffraction(XRD),scanning electron microscopy(SEM),and energy dispersive X-ray spectroscopy(EDS). The results show that the corrosion rate at 550 ℃ is lower and the oxide scales are straight,dense and intact,exhibiting excellent resistance to hot salt corrosion. The corrosion mass gain curves of the alloy follow a parabolic law at 650℃ and the oxide scales exhibit small-scale peeling and internal cracks,with a slightly layered structure. The alloy exhibits good resistance to hot salt corrosion at 650 ℃ in general. A significant mass loss is observed during the corrosion process at 750 ℃,with the oxide scales cracking and peeling severely. Furthermore,within the oxide scales emerges a distinct layered structure where two layers of corrosion products alternately exist:the main layer is mainly composed of TiO2 and contains various corrosion products including NbAlO4,while the other layer is mainly composed of NaNbO3. The resistance to hot salt corrosion of the alloy decreases seriously at 750 ℃.

Ti2AlNb alloyhot salt corrosionmix salttemperature-dependent

孙光耀、刘石双、周毅、曹京霞、黄旭

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中国航发北京航空材料研究院,北京 100095

中国航发先进钛合金重点实验室,北京 100095

Ti2AlNb合金 热盐腐蚀 混合盐 温度相关

2024

材料工程
中国航发北京航空材料研究院

材料工程

CSTPCD北大核心
影响因子:0.78
ISSN:1001-4381
年,卷(期):2024.52(8)
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