RETARDATION AND REPAIR OF FATIGUE CRACKS BY ADHESIVE INFILTRATION

Abstract— This paper presents results which demonstrate that polymeric filler materials, such as low-viscosity epoxies, can be vacuum-infiltrated into fatigue cracks in 7050 aluminium alloy to produce significant levels of fatigue crack retardation. It was found that the main test variable affecting the degree of retardation was the stress level at which the adhesive was introduced and cured. Two infiltrated adhesives were tested.
Infiltration at 0% (of the original) peak fatigue stress level produced negligible retardation, while infiltration at the 80% stress level produced about 300% increase in fatigue life for one adhesive and 3000% for the other adhesive. For the highest infiltration stress level both crack-face wedging and adhesion contributed initially to the retardation, but the adhesive component ceased after a crack grew through the adhesive to the original crack tip position. The results are discussed in terms of the applicability of the technique to highly-stressed aircraft components.     

How to study drying shrinkage microcracking in cement-based materials using optical and scanning electron microscopy?

Three different ‘destructive’ microscopy methods were tested on their ability to show drying shrinkage microcracks on a specimen cross-section. The first two were methods in which the microcracks were impregnated with a fluorescent epoxy and examined with fluorescence microscopy. In one method, the impregnation was applied before making the cross-section and in the other after making the cross-section. In the third method, the sample was kept wet constantly and examined in an environmental scanning electron microscope (ESEM). It was concluded that the method in which the dried specimen was impregnated before making the cross-section was the most reliable method to record drying shrinkage microcracks. With this method, it was possible to impregnate the complete drying shrinkage microcrack pattern in the studied cement-based materials from the surface, and there was no risk of recording microcracks introduced by sample preparation.     

高强度船板纵裂纹的成因及预防

针对高强度船板纵裂纹轧后退废过高的现状，分析原因并优化冶炼、连铸工艺及操作，有效地降低高强度船板的退废率。     

控制连铸板坯星状裂纹的对策

回顾重钢七厂连铸板坯星状裂纹导致轧制钢板表面产生龟裂缺陷、以及对钢坯产生星裂的机理的认识过程,借助国外在这方面的研究成果进行对比分析,认为控制板坯星裂的最重要技术措施是采用"结晶器软冷却”工艺、以及控制钢的铁素体势和铜当量。     

压铸条件和淬火时效对GD—AlSi9Cu3合金力学性能的影响

通过改变压铸工艺参数和淬火时效，测定在静态载荷和动态循环载荷下ＧＤＡｌＳｉ９Ｃｕ３合金的力学性能和断裂力学性能，试验所获得的数据可用来估算压铸件的失效风险率     

单塔汽提水罐开裂原因分析及解决对策

单塔汽提装置原料水罐产生腐蚀裂纹的原因分析判断为低温HCN-H2S-H2O环境下的硫化物应力腐蚀开裂,根据腐蚀成因制定了合理的焊接补焊工艺;涂料防护施工的重点在于表面处理,喷砂后用面粘效果理想且节约施工时间,可延长涂层寿命。     

气相色谱-质谱法联用定性2,2-二羟甲基丁醛

应用气-质谱联用法。并结合质谱解析及化学合成，探讨了2，2-二羟甲基丁醛的裂解方式。确定了该物质的质谱谱图。     

浅析SRT-Ⅳ裂解炉炉管弯曲及断裂原因

主要分析计算了裂解炉炉管受力情况，进而得出结论：裂解炉自身结构的相互约束力和炉管渗碳是导致炉管弯曲、断裂的主要原因，并提出了相应的解决措施。     

液化石油气球罐裂纹成因分析与讨论

对两台1500m3液化石油气球罐在用检验中所发现裂纹的成因进行了分析。有限元应力计算和X射线衍射残余应力测试表明,球罐赤道环焊缝位置存在较高的工作应力和焊接残余应力;对典型裂纹中夹杂物能谱分析表明,这些夹杂物是焊渣;在分析球罐现场组焊焊接工艺的基础上,得出焊缝裂纹主要是由于焊接工艺不当所致,进而提出了修复方案。     

裂解汽油加氢装置二段反应器缺陷分析

对中国石油吉林石化公司300 kt/a乙烯装置汽油加氢二段反应器接管与筒体焊接接头的缺陷进行详细分析。阐明了缺陷的产生是由于在焊接过程中焊缝熔合区内形成马氏体、增碳层并伴有δ-铁素体的分解而使熔合区内及焊缝处的材质脆化。由于选用焊接材料的错误,产生较高的焊接残余应力致使焊缝开裂。分析了焊缝马氏体、增碳层及δ-铁素体分解的原因。