TG6钛合金的热稳定性及其在高温下的部分恢复

Thermal Stability of TG6 Titanium Alloy and Its Partial Resumption at High Temperature     

Effects of precipitates on fatigue crack growth rate of AA 7055 aluminum alloy

The effects of precipitates on the fatigue crack growth rate of AA 7055 Al alloy subjected to different ageing treatments were investigated using transmission electron microscope and fatigue crack growth testing.The results show that the T77 treated samples exhibit the lowest crack growth rate,while the crack growth rate of over-aged samples is the highest.In terms of the model based on the reversibility of dislocation motion within the plastic zone close to the crack tip,the improved crack growth resistance is attributed to many precipitates that are coherent with Al matrix in the under-aged and T77 treated samples.When the precipitate is coherent with the Al matrix,the larger the precipitate is,the slower the fatigue crack grows.The effects of grain boundary precipitates and precipitate free zone on the fatigue crack growth resistance are less significant than those of precipitates within grains of the alloy.     

搅拌铸造SiC_p/2024铝基复合材料的显微组织与力学性能

利用搅拌铸造?热挤压工艺制备SiCp/2024铝基复合材料板材,研究该复合材料铸态、热挤压态和热处理态的显微组织及力学性能。结果表明:SiC颗粒较均匀地分布于铸锭中,大部分SiC颗粒沿晶界分布,少数颗粒分布于晶内,晶界粗大的第二相呈非连续状分布;复合材料经热挤压变形后,显微孔洞等铸造缺陷明显消除,破碎的晶界第二相及SiC颗粒沿热挤压方向呈流线分布,复合材料的强度和塑性显著提高;对热挤压板材进行(495℃,1h)固溶处理+(177℃,8h)时效处理后,其抗拉强度达430MPa,此时的主要析出强化相为S′(Al2CuMg);热挤压变形有利于改善SiC颗粒与基体合金的界面结合,热处理SiCp/2024铝基复合材料的主要断裂方式为基体合金的延性断裂、SiC颗粒断裂和SiC/Al的界面脱粘。     

Rejuvenation Heat Treatment of the Second-Generation Single-Crystal Superalloy DD6

The second-generation single-crystal superalloy DD6 with [001] orientation was prepared by screw selecting method in the directionally solidified furnace. The long-term aging of the alloy after full heat treatment was performed at1100 °C for 400 h. Then the rejuvenation heat treatment 1300 °C/4 h/AC ? 1120 °C/4 h/AC ? 870 °C/24 h/AC was carried out. The stress rupture properties were investigated at 760 °C/800 MPa, 850 °C/550 MPa, 980 °C/250 MPa and1100 °C/140 MPa after different heat treatments. The microstructures of the alloy at different conditions were studied by SEM. The results show that c0 phase of the alloy became very irregular and larger after long-term aging at 1100 °C for 400 h. A very small amount of needle-shaped TCP phase precipitated in the dendrite core. The coarsened c0 phase and TCP phase dissolved entirely after rejuvenation heat treatment. The microstructure was restored and almost same with the original microstructure. The stress rupture life of the alloy decreased in different degrees at various test conditions after long-term aging. The stress rupture life of the alloy after rejuvenation heat treatment all restores to the original specimen more than 80%at different conditions. The microstructure degradation of the alloy during long-term aging includes coarsening of the c0 phase,P-type raft and precipitation of TCP phase, which results in the degeneration of stress rupture property. The rejuvenation heat treatment succeeds in restoring the original microstructure and stress rupture properties of the alloy.     

轻质密胺泡沫制备工艺优化

基于红外光谱分析和反应过程树脂黏度及泡孔结构的变化, 说明了三聚氰胺和甲醛为主要原料制备热固性泡沫的机理, 物理发泡过程还发生交联固化, 不同条件下制备不同泡孔大小和长径比的泡沫。为获得轻质、降噪和回弹好的发泡材料, 设计了正交实验优化工艺, 得到最佳工艺为:发泡液黏度1500 mPa·s, 树脂液、表面活性乳化剂、正戊烷发泡剂、固化剂质量配比为50:2:16:4, 微波加热60 s, 制得密度5 kg·m^-3的密胺泡沫。     

预处理对NiTiNb合金充氢行为的影响

利用DSC等研究手段,探讨了电解充氢环境下预应变和热处理制度对NiTiNb合金的相变行为及性能特征的影响。结果发现,相同充氢条件下随着预变形量的增大,充氢层体积增加,而心部具有可逆马氏体相变的体积减小。热处理温度的升高,会导致样品中充氢层的体积减小,能发生可逆相变的马氏体的体积增大,样品中的低温峰有向低温移动的趋势。热处理保温时间的延长,使得样品中的氢不断地向样品外部扩散,原来在电解充氢过程中不能可逆马氏体相变的部分得到恢复,而NbH化合物的体积则出现减小。     

虫胶清理技术国内外研究进展及在直升机上的应用

虫胶在人类生活中无处不在,易附着在直升机、汽车等表面,难以清除,并带来腐蚀等问题,为此研究者开展了相关研究工作,并得到了诸多行之有效的虫胶清理方法,例如有机溶剂法、水基清洗法、激光脉冲法、机械法、生物酶解法以及主动防护与快速清洁相结合等多种方式.针对这些方法的适用范围、清理效果、优缺点等研究现状进行了分析和总结.直升机...     

轴向加荷疲劳试验机动态力校准的研究

研究了电液伺服式和电磁谐振式两类疲劳试验机,在对其力学模型振动分析的基础上,得到了两类试验机动态力值误差的解析表达式。分析了影响惯性力大小的主要因素,如工作频率、连接夹具或试样的质量、刚度等,进行了多组比较试验,对理论分析结果进行了验证。讨论了疲劳试验机动态力误差的修正,并对校准装置和夹具的选择提出了建议。     

Infrared brazing of TiAl intermetallic using BAg-8 braze alloy

TiAl intermetallic alloy joined by infrared brazing using BAg-8 braze alloy was investigated. The microstructural evolution of the brazed joint, shear strength and reaction kinetics across the joint was comprehensively evaluated. According to the experimental observations, silver would not react with the TiAl substrate, but copper reacted vigorously with the TiAl, forming continuous reaction layer. The consumption of copper from molten braze during infrared brazing resulted in depletion of the copper content from the braze. Therefore, chemical composition of the braze deviated from Ag-Cu eutectic into hypoeutectic with increased brazing time and/or temperature. Both AlCuTi and AlCu₂Ti phase were observed at the interface between BAg-8 and TiAl substrate for the specimen brazed at 950°C. By increasing the brazing temperature and time, the growth rate of AlCuTi phase was much faster than that of AlCu₂Ti phase. The maximum shear strength achieved 343 MPa for the specimen infrared brazed at 950°C for 60 s. Further increasing the brazing time resulted in excessive growth of brittle AlCuTi reaction layer, which greatly deteriorated the shear strength of the joint.     

国产CCF300碳纤维单向织物液体成型工艺性及其复合材料力学性能

选取国产碳纤维CCF300所制备的2种单向织物,单向无纬织物U3160及单向无屈曲织物KUC160,分别对其预成型体进行压缩特性和渗透特性测试,以研究2种单向织物的液体成型工艺性,并采用树脂传递模塑(RTM)工艺制备2种单向织物/双马来酰亚胺树脂基复合材料,测试并对比其面内力学性能。结果表明:预成型体压缩试验中,嵌套效应受压力及织物层数影响较大,压力越高、层数越多,嵌套效应越显著。U3160织物的嵌套效应较KUC160织物更为明显,在较高压力下,KUC160织物预成型体的纤维体积分数较U3160织物的下降了约20%。渗透率测试结果表明:相比U3160织物,KUC160织物0°方向的渗透率较高,而90°方向的渗透率有所降低;这是由于经编线的绑缚作用能促进0°方向的宏观流动,而阻碍90°方向的微观渗透。此外,KUC160织物的经编线与U3160织物的纬向纱线的导流作用也对渗透率有影响。力学性能试验结果表明:相比U3160织物增强复合材料,KUC160织物增强复合材料0°方向的拉伸、弯曲和压缩性能均有所下降,拉伸强度和弯曲模量降幅最大,分别约为11%和21%;而层间剪切强度有小幅提高,增幅约为8%。