16MnR钢高温疲劳裂纹扩展行为试验研究

对16MnR钢在常温、150℃、300℃和425℃下的疲劳裂纹扩展速率进行了测试和分析,得到了四种温度下的疲劳裂纹扩展规律。结果表明：该材料在150℃和300℃的疲劳裂纹扩展速率比常温和425℃时低,425℃时疲劳裂纹扩展速率最高。     

2.25Cr1Mo和2.25Cr1MoV钢高温疲劳裂纹扩展规律研究

对2.25C r1M o和2.25C r1M oV钢在常温到500℃的温度区间内的多个温度上进行疲劳裂纹扩展速率测试和分析,对疲劳断口形貌进行观察,得到了两种材料的高温疲劳裂纹扩展规律。结果表明:两种材料高温下疲劳裂纹扩展规律基本一致;裂纹扩展速率随着温度的升高而增大;疲劳裂纹扩展方式由穿晶型为主向沿晶型为主转变。     

高温下12Cr1MoV管材的疲劳裂纹扩展速率

用国产１２ＣｒＭｏＶ管材制作成紧凑拉伸试件，在ＭＴＳ疲劳系统上进行５３０℃高温下的疲劳裂纹扩展速率试验，以得出Ｐａｒｉｓ公式中的ｃ、ｎ材料参数。在ｄａ／ｄＮ及△ｋ双对数坐标图中给出了５３０℃及２０℃两种温度条件下的直线，以供对比。     

加氢反应器接管焊缝疲劳裂纹的扩展研究

对 2 .2 5Cr1Mo钢在室温和 42 0℃下的疲劳裂纹扩展速率进行了测试和分析 ,得到了两种温度下的疲劳裂纹扩展规律 ,并根据测试结果对一台加氢反应器接管连接焊缝裂纹的疲劳扩展进行了计算和安全评估 ,为该反应器的安全使用提供了理论依据。     

316L钢高温疲劳裂纹扩展的规律研究

对316L钢在常温、200℃、400℃和550℃。下的疲劳裂纹扩展速率进行了测试和分析，对疲劳断口形貌进行观察，得到了四种温度下的疲劳裂纹扩展规律。结果表明：裂纹扩展率随着温度的升高而增大；高温下氧化作用增强。     

16MnR钢表面裂纹的疲劳扩展

报告了在 P_x∶P_y=0,0.5和1三种双轴载荷作用下,对倾斜角等于0°、30°和45°的表面裂纹所作的疲劳扩展研究。讨论了表面裂纹扩展速率的计算方法,指出必须考虑不同的裂纹倾斜角和不同的双轴载荷比造成的裂纹扩展驱动力的变化对斜表面裂纹扩展速率的影响。因而采用裂纹投影法来处理斜表面裂纹的疲劳扩展问题并提出了修正的 Paris 方程。按照修正的 Paris 方程,根据不同的双轴载荷比和裂纹倾斜角分组整理了试验数据,并作了回归分析、假设检验,给出了含表面裂纹的16MnR 板材在三种不同的双轴载荷比情况下的裂纹扩展速率方程。     

高强度CrNiMoV钢裂纹疲劳扩展行为研究和水晶釜安全寿命评估

对高强度钢ＣｒＮｉＭｏＶ表面裂纹的疲劳扩展速率ｄａ／ｄＮ进行了测试和分析，并据此对某一超高压水晶釜的安全寿命作了评估。     

变幅载荷疲劳裂纹扩展行为的试验研究

用某压力容器实际工况载荷波动所编制的载荷谱,对材料为16MnR的CCT试件进行了变幅载荷谱下的疲劳裂纹扩展试验。根据试验数据,分析了裁荷谱中大载荷级和小载荷级分别对裂纹扩展量的贡献,并对考虑和不考虑超载迟滞效应对小载荷裂纹扩展行为的影响进行了对比。作为这方面的初步探索,本研究获得了一些有意义的结论。     

工程陶瓷疲劳裂纹扩展的实验研究

本文提供了一种新的确定工程陶瓷疲劳裂纹扩展速率公式－－Ｐａｒｉｓ公式中两个常数参量的实验方法。避开了直接测量裂纹工度的麻烦，且成功率很高。给出了以Ａｌ２Ｏ３和ＨＰ０－Ｓｉ３Ｎ４陶瓷为试验材料的实验结果，并在这个结果的基础上对工程陶瓷的疲劳特性作了描述。     

316L钢高温疲劳裂纹扩展的规律研究

对 3 1 6L 钢在 2 5℃、 2 0 0℃、 40 0℃和 550℃下的疲劳裂纹扩展速率进行测试和分析 ,对疲劳断口形貌进行观察 ,得到四种温度下的疲劳裂纹扩展规律。结果表明 :裂纹扩展速率随着温度升高而增大 ;高温下氧化作用增强。     

Oxidation behavior of C/SiC-SiBCN composites at high temperature

In order to improve the anti-oxidation performance of C/SiC composites at high temperature, C/SiC composites should be modified by self-healing components. SiBCN ceramic is an ideal self-healing component because of excellent oxidation resistance and thermal stability. C/SiC composites were modified by PDC SiBCN ceramic (C/SiC-SiBCN) by using CVI combined with polymer infiltration and on-line pyrolysis (PI-OP). The oxidation behaviors of C/SiC composites fabricated by CVI method and C/SiC-SiBCN composites fabricated by CVI + PI-OP method and CVI + PIP method at different temperatures in air were compared. The results showed that the strength retention ratios of the composites fabricated by the three methods decreased with the increase of temperature. Compared with the samples fabricated by the other two methods, the weight loss of the samples fabricated by CVI + PI-OP method was greater, but the strength retention ratio was higher.     

Effect of ceramic-based coatings deposited on low-alloyed steel T/P22 10H2M exposed at high temperature

The study was carried out in order to evaluate oxidation resistance of the ceramic coatings based on SiO₂-B₂O₃-TiO₂-Na₂O composition deposited on the low-alloyed steel T/P22 (10H2M) surface exposed for 1000 h at 540°C in oxidation atmosphere. Kinetic data were recorded periodically every 250 h; macro- and microanalyses as well as chemical composition were carried out using macrolenses, SEM, EDS, EDS X-ray mappings. The results indicated a high degree of protection by ceramic coatings; much lower mass gain was observed for the coated materials than for the uncoated T/P22 (10H2M) steel. No detachment, delamination, chipping of a coating were found from the steel surface; some of the coatings showed perpendicular tiny cracks to the bulk metal surface.     

The use of crack layer theory to predict the lifetime of the fatigue crack growth of high density polyethylene

In the case of high density polyethylene (HDPE), the fatigue crack propagates in a discontinuous manner, which can be observed by distinct striations. In this article, fatigue crack growth (FCG) experiments were conducted on two grades of HDPE pipe with compact‐tension (CT) and cracked round bar (CRB) specimens. The effects of the stress ratio (R‐ratio) which is defined as the ratio of minimum stress and maximum stress of fatigue loadings and the frequency on FCG behavior were experimentally studied. Although FCG rates showed a great dependence on the R‐ratio in terms of the range of the stress‐intensity factor, the effect of the frequency may be considered to be significant in the low crack growth region. In addition, these experimental data were employed for predicting the lifetime on the basis of the crack layer (CL) theory. Only a few steps of FCG are needed to determine all necessary parameters for CL theory, and the FCG behavior can be reconstructed based on a computer program that has been developed for the application of CL theory. The predictions from this program accord with experimental data. POLYM. ENG. SCI., 2009. © 2009 Society of Plastics Engineers     

Epitaxial growth on nickel-plated diamond seeds at high pressure and high temperature

Epitaxial growth on nickel-plated diamond seeds at high pressure and high temperature (HPHT) was observed with graphite as carbon source. The thickness of the electroplating nickel film which acts as a catalyst/solvent ranges from 54.6 μm to 255.6 μm. The relationship between the Ni film thickness and diamond growth rate is investigated. When the nickel film thickness is from 90 μm to 129 μm, diamond crystals can nearly grow up to three times as large as the original seeds at ∼ 5.8 GPa and ∼ 1460 °C within 14 min. The mechanism of the crystal growth with nickel-plated diamond seeds under HPHT is discussed. The results and techniques might be useful for high quality saw-grade diamonds production and large diamond single crystal growth.     

高温型煤复合添加剂的研究

高温型煤复合添加剂,其最佳配方为：乾陵石灰石的添加量为10％,改性氢氧化钙的添加量2．5％,含铁辉石的添加量5％,氧化镁的添加量为2％,碳酸锶的添加量为1％,玉米秸秆粘结剂的添加量为15％,该配比制备的型煤在1200℃时固硫率达56％。该型煤的跌落强度高,且具有防水性。     

Experimental investigation of fatigue crack growth behavior and damage mechanisms of fiber/metal laminates under uniaxial and biaxial loading

The response of the aramid reinforced aluminum-epoxy-laminate to uniaxial and biaxial fatigue loading has been investigated. The fracture process in the laminates propagates mainly in the form of cracks in aluminum layers, delaminations between the resin-rich and fiber-rich prepreg layers, splitting in prepreg layers and fiber fracture. Ultrasonic microscopy has been used to evaluate the shape and size of the damage zone. The ultrasonic images have been calibrated by means of SEM and optical microscopy of the laminates with sequential removal of the layers. Microscopic examination reveals a direct correlation between delamination, fiber fracture, and fatigue crack growth in the aluminum layer. The results of this investigation strongly suggest that the laminate resistance to tension-tension biaxial fatigue is superior to that under uniaxial loading conditions.     

高温下钙基吸附剂吸附CO2的研究

CaO基吸附剂是一种理想的CO2高温吸附剂。利用热重分析仪研究了由不同前体制备的CaO高温下对CO2的吸附性能。利用吸附仪测定了各吸附剂的比表面积等参数。实验发现CaO的最佳吸附温度范围为700—750℃;由CaC2O4.H2O制得的CaC2O4-CaO具有良好的吸附性能,在实验条件下,其吸附量为理论吸附量的89.1%;在较宽的CO2体积分数范围内,CaC2O4-CaO始终保持很高的吸附性能;吸收速率的大小受吸附剂比表面积、孔体积、孔结构等参数的共同影响。高温下,CaO基吸附剂吸附CO2的微观机理有待进一步研究。