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通过金相显微镜、扫描电镜等分析方法对铁素体钢低倍检验后发现的疑似白点缺陷进行了分析判断,发现疑似白点缺陷在金相显微镜下呈锯齿状裂纹,为白点裂纹形貌特征。通过对低倍试样上断口的检验发现,低碳铁素体钢宏观断口处分布有银灰色圆形斑点,为白点缺陷特征,铁素体不锈钢宏观断口无明显白点特征,但铁素体不锈钢的疑似白点显微断口有沿晶断裂和以夹杂物为裂纹源的解理断裂两种,都具有氢脆断口特征,由此判断,两种铁素体钢中缺陷均为白点缺陷。铁素体不锈钢中的白点缺陷与常见白点断口上的浮云状、波纹状、解理羽毛、显微疏松等形貌特征有所不同,而且不同铁素体不锈钢试样上的白点缺陷断口形貌也不同,一处为沿晶断裂,一处为以夹杂物为裂纹源的解理断裂。 相似文献
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应用超声波探伤,低倍,宏观断口,金相和扫描电镜检验方法,对低碳合金钢板中白点缺陷进行了检验和研究。详细介绍了钢板中白点缺陷的宏观特征和遭到同特征和微观貌及消除措施。 相似文献
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钢中白点及其形成机理 总被引:3,自引:0,他引:3
白点是热轧钢坯和大型锻件中比较常见的低倍缺陷。白点的破坏性极大,作为钢中的显微裂纹,可能成为疲劳裂纹源,降低钢的强度。为此,研究了钢中白点的形成机理,找出消除白点的根本措施。 相似文献
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对42CrMo大截面锻材的低倍检验,发现锻材的中心裂纹其实是白点,经采用去氢退火工艺后,白点消除,锻材探伤合格率、成材率明显提高。有电弧炉单炼,钢锭锻造由Φ250以睛的钢材时,去氢退火应是保证钢材内部质量的有效手段。 相似文献
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主要对本钢产的车轮轮毂用钢BG420CL钢在冲压成型过程中出现的开裂进行了研究,通过低倍检验、金相检验及扫描电子显微镜断口观察发现钢板冲压开裂是连铸坯表面的裂纹缺陷残存在成品表面形成裂纹源而引起的。 相似文献
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某风电齿轮箱在运行3年6个月后监测到运行异常,拆解后发现其中一个行星轮发生断齿失效。实验通过对行星轮断口宏微观形貌分析、化学成分分析、力学性能分析、金相组织分析、残余应力分析和晶粒分布分析等,确定了行星轮轮齿的断裂原因。分析结果表明,行星轮材料母材各化学元素含量及轮齿表面碳元素含量均满足标准规范要求。行星轮轮齿力学性能满足标准规范要求,轮齿渗碳层金相组织和行星轮母材金相组织均未见异常,表明行星轮渗碳工艺和热处理工艺均满足材料使用要求。轮齿断口起裂源区存在大尺寸非金属夹杂物的聚集是运行过程中在该处萌生裂纹并扩展的主要原因。 相似文献
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针对邯钢Q345RT中厚板生产中出现的钢板探伤不合格缺陷,并且在钢板缺陷处取样,断口有时存在层状现象.采用化学分析、气体含量检验、铸坯低倍检验、金相组织分析和扫描电镜、断口形貌分析等方法,分析钢板探伤不合格的原因.结果表明:铸坯中心偏析严重,因偏析产生的少量马氏体、贝氏体组织导致轧后应力集中,在冷却速度较快的条件下钢板产生微裂纹,以条状MnS和CaO-A12O3为基体的硫化物夹杂和硅酸盐类夹杂物较高,铸坯中氢含量偏高引起氢致裂纹,均可导致钢板探伤不合格.通过控制炼钢工艺过程,减少了铸坯中的夹杂物和氢含量,该中厚板探伤合格率由92%提高到98.2%. 相似文献
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T. R. Pinchback S. P. Clough L. A. Heldt 《Metallurgical and Materials Transactions A》1975,6(9):1479-1483
Alloy 260 brass specimens under stress were exposed at room temperature to 15 N aqueous ammonia solution with 8 g/1 of cupric
copper predissolved. This environment causes tarnishing of the brass surface and intergranular stress corrosion cracking.
Scanning electron microscopy, energy dispersive X-ray analysis, and Auger electron spectroscopy were employed to study fractography,
corrosion product composition and distribution within the stress corrosion crack, and fracture surface chemistry characteristic
of stress corrosion cracking in this system. A thin oxidized film was detected by Auger spectroscopy at the leading edge of
the propagating crack. With continued exposure to the corrosive environment, deposits form on the fracture surface, then coalesce
to form a continuous tarnish film that is depleted of zinc. No bulk depletion of zinc was detected in the alloy at the stress
corrosion crack leading edge. No evidence of noncrystallographic crack arrest marks was found on the intergranular fracture
surface. 相似文献
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在汽车钢板u型螺栓生产过程中,调质后发现工件都有纵向开裂现象,造成产品报废。本文对报废产品取样进行了化学成份、金相高、低倍、硬度等项目的检测分析。分析发现螺栓用原材料工件为∮28mm正是处于最危险淬裂尺寸范围,其化学成份碳、锰、铬等元素均处于标准要求的上限,从而提高了其淬透性,在淬火冷却时,表面拉应力超过材料的断裂强度造成开裂。 相似文献
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《Acta Metallurgica》1986,34(9):1721-1735
By means of fracture mechanics analyses, acoustic emission techniques, and fracture surface analyses by scanning Auger microscopy and X-rays, it was determined how segregated phosphorus, yield strength and grain size affect the equilibrium and growth characteristics of hydrogen-induced intergranular cracking in high strength steels. The effect of yield strength on the threshold stress intensity was found to be greater than those of phosphorus segregation and grain size. The intergranular phosphorus segregation greatly accelerated the growth rate of hydrogen-induced intergranular cracking and caused a large number of acoustic signals to be emitted during the crack growth. The crack growth rate increased in a steel with segregated phosphorus and slightly decreased in high purity steels, where only occasional acoustic emissions were measured during the cracking process, by increasing grain size. Fracture surface analyses indicated more featureless intergranular fracture facets and higher levels of residual strain in the lattice adjacent to the fracture surface in the phosphorus-doped steel than in the high purity steels. These results suggest that while in steels with segregated impurities the macrocrack tends to grow by discretely rapid formation of intergranular microcracking which gives rise to dislocation emissions at the growing crack tip, in high purity steels slow growth of intergranular microcracking proceeds which is accompanied by either the absence or substantial mitigation of dislocation generation at the crack tip. 相似文献
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G. P. Zhang Ph.D. Student Z. G. Wang G. Y. Li S. D. Wu 《Metallurgical and Materials Transactions A》1997,28(3):665-672
The effect of crystallographic orientation on the fatigue-crack initiation and propagation in Ni3Al(CrB) single crystal was studied using a compact-tension specimen. Stage I crystallographic cracking and cleavage fracture
were observed. Crystallographic cracking can occur on two or more {111} slip planes simultaneously. It was shown that the
threshold stress intensity for crack initiation from the notch root exhibits a dependence on crystallographic orientation.
In addition, an effect of orientation on microcracking behavior was also shown. The number of {111} planes intersecting with
each other determines the different microscopic features on the cleavage fracture surface. 相似文献
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The effects of air and vacuum on the fatigue behavior of a nickel-base superalloy, Mar-M200, in single crystal form were investigated.
Between 800° and 1400°F fracture is entirely in the Stage I mode in air and vacuum, and fatigue life is unaffected by environment.
At 1700° F in both environments, fracture is predominantly in the Stage II mode and fatigue life in air is greater than that
in vacuum. At both temperatures, fatigue cracking in air is internally initiated, whereas in vacuum cracking is generally
initiated at the specimen surface. Identical fatigue lives in air and in vacuum between 800° and 1400° F are attributed to
the fact that internally initiated cracks in air are actually propagating in a high vacuum, surface cracking being inhibited
by dynamic oxidation of emerging surface slip offsets. The subsurface portion of the Stage I fracture surface produced in
air tests and all of the Stage I fracture produced in vacuum tests shows a dimpled structure, whereas the Stage I fracture
surface produced while the crack propagation is in air shows a cleavage appearance. At 1700° F, bulk oxidation of surface
initiated cracks interferes with the plastic blunting mechanism of Stage II crack growth normally observed at this temperature,
internally initiated cracks causing ultimate failure. Shorter lives in vacuum are thought to result from enhanced Stage II
surface crack propagation.
Formerly with Materials Engineering and Research Laboratory, Pratt and Whitney Aircraft, Middletown, Conn. 相似文献