Inconel625合金高速热变形动态再结晶的临界条件

通过等温热压缩试验获得Inconel625合金在变形温度为1000～1200℃,应变速率为1～80S^-1条件下的真应力-应变曲线,利用加工硬化率,结合lnθ-ε曲线上的拐点判据及-δ（1nθ）／δε-ε曲线上的最小值,来研究Inconel625合金动态再结晶的临界条件。结果表明,在该实验条件下,Inconel625合金的lnθε曲线均出现拐点特征,对应的-δ（lnθ）／δε-ε曲线出现最小值,该最小值处对应的应变即为临界应变;临界应变随应变速率的增大和变形温度的降低而增加,并且临界应变和峰值应变之间有一定的关系,即εc=0．69εp;动态再结晶时临界应变的预测模型可以表示为εc=4．41×10^-4Z^0.14261。     

50Mn钢凸轮轴的中频感应淬火

凸轮轴是柴油机的重要传动件之一,要求根据所采用的材料进行渗碳淬火或表面淬火,以提高其表面硬度和耐磨性。50Mn钢凸轮轴采用BVH-1000双工位中频淬火机床、仿形感应器和专用夹具等设备,以及10％～15％AQ251聚合物水溶液进行感应淬火。结果,凸轮轴的表面硬度、硬化层深度分布和显微组织均达到了要求,生产成本明显低于进行渗碳淬火的20Cr钢凸轮轴。     

AA7050高强铝合金在固溶淬火过程中的温度变化及固溶制度(英文)

采用温度记录系统、组织观察、力学性能测试、电导率测试和DSC热分析研究7050高强铝合金固溶过程中的温度变化,确定合理的固溶热处理制度。采用了2种不同尺寸规格的试样进行试验。研究表明,在本试验条件下的固溶热处理过程中,大尺寸试样固溶温度相对较低,固溶时间较短,导致合金中强化析出相的体积分数减少。对于尺寸为25mm×25mm×2.5mm和70mm×60mm×20mm的试样,合理的固溶热处理制度分别为(480℃,30min)和(480℃,90min)。小尺寸试样中的GP区和η′相密度大于大尺寸试样中相应的密度,这与合金性能测试的结果一致。     

TWIP钢Fe-23Mn-2Al-0.2C的组织及拉伸变形机制

研究了TWIP钢Fe-23Mn-2Al-0.2C固溶处理后的组织演变和拉伸变形行为,并对其变形机制进行了探讨。结果表明:随固溶温度升高,实验钢的晶粒尺寸逐渐增大,屈服强度和抗拉强度均降低,伸长率增大,强塑积先增大后减小,在900℃时达到最高;实验钢的拉伸变形呈现连续屈服,同时随固溶温度升高,加工硬化速率(dσ/dε)与真应变(ε)的变化关系由2阶段变为3阶段。通过OM和TEM观察显示,随着晶粒尺寸的增加,变形过程中形变孪晶数量增多,孪晶诱导塑性(TWIP)效应增大。     

冷加工和时效处理顺序对6061铝合金力学性能的影响(英文)

研究不同的析出硬化和冷加工组合对6061铝合金拉伸性能的影响。结果表明,在不同的热处理过程中,在180℃单时效4h能提高合金的强度和伸长率。然而,双时效处理不能改善其力学性能。另外,预时效对随后的析出硬化有负面影响。合金力学性能的变化归因于析出硬化、应变硬化和加工软化的竞争而引起的显微组织演变。     

Influence of substrate bias, deposition temperature and post-deposition annealing on the structure and properties of multi-principal-component (AlCrMoSiTi)N coatings

Nitride films are deposited from a single equiatomic AlCrMoSiTi target by reactive DC magnetron sputtering. The influence of the substrate bias and deposition temperature on the coating structure and properties are investigated. The bias is varied from 0 to − 200 V while maintaining a substrate temperature of 573 K. And the temperature is changed from 300 to 773 K whilst maintaining a substrate bias of − 100 V. From X-ray diffraction analysis, it is found that all the as-deposited coatings are of a single phase with NaCl-type FCC structure. This is attributed to the high mixing entropy of AlN, CrN, MoN, SiN, and TiN, and the limited diffusion kinetics during coating growth. Specific aspects of the coating, namely the grain size, lattice constant and compressive stress, are seen to be influenced more by substrate bias than deposition temperature. In fact, it is possible to classify the deposited films as large grained (~ 15 nm) with a reduced lattice constant (~ 4.15 Å) and low compressive residual stresses for lower applied substrate biases, and as small grained (~ 4 nm) with an increased lattice constant (~ 4.25 Å) and high compressive residual stresses for applied biases of − 100 V or more. A good correlation between the residual stress and lattice constant under various deposition conditions is found. For the coatings deposited at − 100 V, and at temperatures above 573 K, the hardness could attain to the range of 32 to 35 GPa.Even after annealing in vacuum at 1173 K for 5 h, there is no notable change in the as-deposited phase, grain size or lattice constant of the coatings but an increase in hardness. The thermal stability of microstructure is considered to be a result of the high mixing entropy and sluggish diffusion of these multi-component coatings. For the anneal hardening it is proposed that the overall bonding between target elements and nitrogen is enhanced by thermal energy during annealing.     

Improving the Mechanical Properties of Mg-Gd-Y-Ag-Zr Alloy via Pre-Strain and Two-Stage Ageing

In this study, we investigated the effects of single-stage ageing (SSA), two-stage ageing (TSA), 2% pre-strain + single-stage ageing (P2%SSA) and 2% pre-strain + two-stage ageing (P2%TSA) on the mechanical properties of as-extruded Mg–8Gd–3Y–0.5Ag–0.5Zr alloy (E alloy). Compared with the SSA treatment, the TSA treatment increased the number density of $\beta ^{\prime}$ phase. The P2%SSA and P2%TSA treatments generated the $\gamma ^{\prime}$ phase and chain-like precipitates in addition to the $\beta ^{\prime}$ phase. The contributions of these ageing treatments to the alloy strengthening can be ranked as P2%TSA > P2%SSA > TSA > SSA, because the increments in the tensile yield strength were estimated to be 199 MPa > 148 MPa > 144 MPa > 110 MPa. Different from the traditional strengthening of $\beta ^{\prime}$ phase in the E + SSA and E + TSA alloys, the composite precipitates comprising the $\beta ^{\prime}$ phase, $\gamma ^{\prime}$ phase and chain-like precipitates in the E + P2%SSA and E + P2%TSA alloys provided better combined strengthening effect. The $\beta ^{\prime}$ phase was still dominated in the strengthening effect of the composite precipitates. Owing to the higher number density of $\beta ^{\prime}$ phase in the composite precipitates, the E + P2%TSA alloy exhibited the better mechanical performance as compared with the E + P2%SSA alloy. Finally, the E + P2%TSA alloy had the ultimate tensile strength of 452 MPa, the tensile yield strength of 401 MPa and elongation to failure of 3.3%.     

铸造用CO2硬化聚乙烯醇粘结剂促硬剂的研究

研究了CO2更化聚乙烯醇粘结剂的促硬剂,是由Ca(OH)2、硅酸盐水泥及一种水硬性材料复合混制而成,原料来源广泛,价格低廉.加入促硬剂后,缩短硬化时间,大幅度提高粘结剂的粘结强度,并加入交联剂、偶联剂进一步提高粘结剂工艺强度.试验中通过正交试验优化各组分的添加比例,并对混合后型砂的可使用时间、吹制砂芯的存放性、溃散性和发气性等工艺性能进行了试验,并对性能增强机理进行简要的分析.     

R60705锆合金的热处理工艺及性能

通过力学性能测试和显微组织分析研究了R60705锆合金的热处理工艺与组织性能之间的关系。结果表明,R60705锆合金经870℃加热水冷淬火加550℃时效的热处理后具有较高的综合力学性能。组织中α相呈短条状分布,基体组织较细密。经该工艺处理后的综合力学性能满足了设备主轴的服役要求。     

Al-6.3Zn-2.8Mg-1.8Cu铸造铝合金的组织和室温力学性能

研究了Al-6.3Zn 2.8Mg-1.8Cu铸造铝合金的组织和室温力学性能.研究表明,在金属型铸造条件下,Al-6.3Zn-2.8Mg-1.8Cu合金的铸态组织为近等轴晶,相组成为α（Al）基体、枝晶间α（Al）+η（MgZn₂）共晶、晶内游离η相（MgZn₂）、少量T相（Mg₃Zn_xCu₃-_xAl₂）及少量颗粒状Al₇Cu₂Fe.固溶处理后,原铸态组织中的η（MgZn₂）相大部分溶解消失,但形成新的沿晶界分布的S相（Al₂CuMg）.实验确定了固溶态Al-6.3Zn-2.8Mg-1.8Cu合金较优的单级和双级时效工艺.与单级时效工艺相比,采用双级时效工艺处理后,抗拉强度由480 MPa增加至490 MPa,延伸率由0.2%增加至2.2%.