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Grain boundary inclination dependence of GN dislocation patterns and density in bicrystal model 双晶模型中GN位错模式和密度对晶界倾角的依赖
Pub Date : 2015-11-27 DOI: 10.1299/TRANSJSME.14-00630
Yoshiki Kawano, N. Tamaru, S. Ishii, T. Mayama, Ryouji Kondou, T. Ohashi
Deformation behaviors of polycrystalline metals are quite complex, and we are not easy to directly investigate them; thus, analyses employing simple models such as bicrystals are required. In this study, we conducted crystal plasticity analysis of unidirectional tensile tests, using compatible-symmetric-type bicrystal models with the not-inclined grain boundary and incompatible-type bicrystal model with the inclined grain boundary; we investigated changes in patterns of geometrically necessary dislocation (GND) bans and the density of GNDs in the initial deformation. In the condition where the grain boundary contacted with the constrained faces, GND bans were formed and the distribution was changed with changing the inclination angle α of the grain boundary. In contrast, GNDs were not localized in high density in the condition where the grain boundary contacted with the free surfaces; the changes were caused by two-reasons: one was changes of compatibility of the bicrystal model with changing the inclination angle α, and the other was that deformation shapes of the bicrystal model under tensile loading were changed with changing the inclination angle α and the deformation was constrained by the constrained faces. The compatibility of and average density of GNDs in the bicrystal model could be estimated using differences of components of Schmid tensors between the crystal grains.
多晶金属的变形行为非常复杂,不容易直接研究;因此,需要采用双晶体等简单模型进行分析。本研究采用非倾斜晶界的相容对称型双晶模型和倾斜晶界的不相容型双晶模型对单向拉伸试验进行了晶体塑性分析;我们研究了初始变形中几何必要位错(GND)带的模式和GND密度的变化。在晶界与约束面接触的情况下,随着晶界倾角α的改变,会形成GND条纹,并改变其分布。而在晶界与自由表面接触的情况下,GNDs密度不高;这种变化是由于两种原因引起的:一是改变双晶模型的相容性随倾角α的变化而变化;二是改变倾角α使双晶模型在拉伸载荷作用下的变形形态发生变化,变形受到约束面的约束。双晶模型中GNDs的相容性和平均密度可以通过晶粒间施密德张量分量的差异来估计。
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引用次数: 4
高温場に挿入されたポリエチレンフィルムの着火・燃焼特性(第1報:着火遅れ時間,燃焼時間に及ぼすフィルム寸法の影響) 插入高温场的聚乙烯薄膜的着火、燃烧特性(第1报:着火延迟时间,薄膜尺寸对燃烧时间的影响)
Pub Date : 2015-08-05 DOI: 10.1299/TRANSJSME.15-00187
光佑 池田
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引用次数: 0
20102 Damage Process of Ceramic Thermal Barrier Coatings Exposed at High Temperature under Tensile Loading 陶瓷热障涂层在拉伸载荷下高温暴露的损伤过程
Pub Date : 2015-03-20 DOI: 10.1299/JSMEKANTO.2015.21._20102-1_
Yuto Shimizu, M. Arai, T. Suidzu
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引用次数: 0
長周期・大振幅地震動の測定を可能にする小型絶対変位振動計の開発研究(達成された成果について) 能够测量长周期、大振幅地震的小型绝对位移振动仪的开发研究(关于已取得的成果)
Pub Date : 2015-01-20 DOI: 10.1299/TRANSJSME.14-00555
一登 背戸, 雄一 岩崎, 充弘 宮崎, 亨 渡辺
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引用次数: 0
Detection of fatigue damage in stainless steel by EBSD analysis (analysis focused on grain boundaries) 基于EBSD分析的不锈钢疲劳损伤检测(晶界分析)
Pub Date : 2013-12-01 DOI: 10.1299/KIKAIA.79.1690
M. Kuroda, M. Kamaya, Takayuki Mori, T. Izaki
In order to develop more sensitive EBSD parameters to detect fatigue damage in austenitic stainless steel used as key material for nuclear reactor components, the new EBSD parameter focused on grain boundaries, which was referred to as the averaged grain boundary local misorientation (BMave), has been proposed by modifying the existing EBSD parameter of the averaged local misorientation (Mave). The applicability of the new parameter BMave to the fatigue damage detection was discussed by comparing with the exiting parameter Mave. As a result, it was found that BMave was more sensitive parameter than Mave. Especially, BMave (Option 1), which was calculated using the crystal orientations at points just adjacent to grain boundaries, was the most effective parameter for the fatigue damage detection.
为了开发更灵敏的EBSD参数来检测核反应堆关键材料奥氏体不锈钢的疲劳损伤,通过对现有的平均局部错向(Mave) EBSD参数进行修正,提出了以晶界为中心的平均晶界局部错向(BMave) EBSD参数。通过与已有参数Mave的比较,讨论了新参数BMave在疲劳损伤检测中的适用性。结果发现BMave是比Mave更敏感的参数。特别是,BMave(选项1)是最有效的疲劳损伤检测参数,它是利用晶界附近点的晶体取向来计算的。
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引用次数: 3
Effect of displacement velocity on elastic plastic fracture toughness of SM490B carbon steel plate in 0.7 MPa hydrogen gas 位移速度对0.7 MPa氢气中SM490B碳钢板弹塑性断裂韧性的影响
Pub Date : 2013-10-15 DOI: 10.1299/KIKAIA.79.1210
Takuya Matsumoto, H. Itoga, Sana Hirabayashi, M. Kubota, S. Matsuoka
©2013 The Japan Society of Mechanical Engineers The elastic-plastic fracture toughness, JIc, of SM490B carbon steel plate was investigated in air and 0.7 MPa hydrogen gas. JIc tests were conducted in accordance with the JSME standard, JSME S001 (1981). JIc was much smaller in hydrogen at a displacement velocity of V = 2 × 10 mm/s (JIc = 10.0 kJ/m) than in air at V = 2 × 10 mm/s (JIc = 248.6 kJ/m). JIc in air does not satisfy the validity requirement. In hydrogen, surprisingly, a further decrease in V did not decrease JIc, but increased it. JIc in hydrogen at V = 2 × 10 mm/s was 60.9 kJ/m. The large and small values of JIc in air and hydrogen corresponded to the fracture morphology. In air at V = 2 × 10 mm/s, a critical stretched zone, SZWc, was formed at the tip of the fatigue pre-crack, followed by dimples. In hydrogen at V = 2 × 10 mm/s, quasi-cleavage instead of SZWc and dimples were formed at the pre-crack tip. In hydrogen at V = 2 × 10 mm/s, SZWc was formed at the precrack tip, followed by dimples again. This elastic-plastic fracture toughness behavior was analyzed assuming HESFCG (hydrogen-enhanced successive fatigue crack growth), which is proposed by the authors to explain the acceleration of fatigue crack growth rate in the presence of hydrogen. The elastic plastic fracture toughness test shown in 0.7 MPa hydrogen gas at V = 2 × 10 mm/s is the same as that shown in a fatigue crack growth test in 0.7 MPa hydrogen gas at a number of cycles of n = 1 and stress ratio of R = 0; and thus JIc in 0.7 MPa hydrogen gas at V = 2 × 10 mm/s is not the real elastic-plastic fracture toughness. We conclude that the real elastic-plastic fracture toughness in 0.7 MPa hydrogen gas can be determined by fracture toughness testing in 0.7 MPa hydrogen gas at V = 2 × 10 mm/s.
对SM490B碳钢板在空气和0.7 MPa氢气条件下的弹塑性断裂韧性(JIc)进行了研究。JIc试验按照JSME标准JSME S001(1981)进行。当位移速度为V = 2 × 10 mm/s (JIc = 10.0 kJ/m)时,氢气中的JIc远小于V = 2 × 10 mm/s (JIc = 248.6 kJ/m)时的JIc。空气中的JIc不满足有效性要求。在氢中,令人惊讶的是,V的进一步降低并没有降低JIc,而是增加了它。在V = 2 × 10 mm/s时,氢的JIc为60.9 kJ/m。空气和氢气中JIc值的大小与断口形貌相对应。在V = 2 × 10 mm/s的空气中,疲劳预裂纹尖端形成临界拉伸区SZWc,随后形成韧窝。在V = 2 × 10 mm/s的氢条件下,预裂尖端形成了准解理而不是SZWc和韧窝。在V = 2 × 10 mm/s的氢气条件下,预裂尖端形成了SZWc,随后又形成了韧窝。采用HESFCG(氢增强连续疲劳裂纹扩展)模型分析了该材料的弹塑性断裂韧性行为。HESFCG是作者提出的解释氢存在下疲劳裂纹扩展速率加快的理论。0.7 MPa氢气条件下V = 2 × 10 mm/s的弹塑性断裂韧性试验结果与0.7 MPa氢气条件下n = 1次循环次数、应力比R = 0的疲劳裂纹扩展试验结果相同;因此,在V = 2 × 10 mm/s条件下,0.7 MPa氢气条件下的JIc并不是真正的弹塑性断裂韧性。得出0.7 MPa氢气条件下的真实弹塑性断裂韧性可以通过V = 2 × 10 mm/s的0.7 MPa氢气条件下的断裂韧性测试来确定。
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引用次数: 11
Observation of the fracture behavior in A1050-ADC12 functionally graded porous aluminum under impact compression A1050-ADC12功能梯度多孔铝冲击压缩断裂行为观察
Pub Date : 2013-10-15 DOI: 10.1299/KIKAIA.79.1076
N. Kubota, Kousuke Saito, Y. Hangai, T. Utsunomiya, T. Ishima, H. Kawashima, O. Kuwazuru, N. Yoshikawa
Porous aluminum is a lightweight material with high energy absorption properties. In this study, impact test of A1050-ADC12 functionally graded porous aluminum fabricated by friction stir processing (FSP) route was carried out. It was shown that deformation began from low strength A1050 layer and thereafter high strength ADC12 layer deformed. This result is consistent with the result of static compression test of A1050-ADC12 functionally graded porous aluminum. Consequently, it was shown that A1050-ADC12 functionally graded porous aluminum has the potential for its location of deformation to be controlled.
多孔铝是一种轻质材料,具有较高的吸能性能。本研究对采用搅拌摩擦加工(FSP)工艺制备的A1050-ADC12功能梯度多孔铝进行了冲击试验。结果表明,变形从低强度的A1050层开始,然后是高强度的ADC12层变形。该结果与A1050-ADC12功能梯度多孔铝的静态压缩试验结果一致。结果表明,A1050-ADC12功能梯度多孔铝具有控制变形位置的潜力。
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引用次数: 0
Detection of fatigue damage in stainless steel by EBSD analysis (comparison with TEM observation) 用EBSD分析检测不锈钢疲劳损伤(与透射电镜观察对比)
Pub Date : 2013-10-15 DOI: 10.1299/KIKAIA.79.1102
M. Kuroda, K. Yasunaga, M. Kamaya, Teruaki Yamada
In order to develop high-reliable maintenance systems to secure the structural integrity of reactor components, analytical and diagnostic techniques for the detection of fatigue damage should be developed further. In the present study, crystal orientation analysis and microstructural observation were performed for Type 316 austenitic stainless steel subjected to cyclic loading by electron backscatter diffraction (EBSD) and transmission electron microscope (TEM) to clarify the relationship between the changes in the crystal orientation and the microstructure introduced by fatigue cycles. As a result of the comparison between the EBSD analysis and the TEM observation, it was concluded that the change in the local misorientation identified by the EBSD analysis was due to the formation of the dislocation cell structures identified by the TEM observation.
为了开发高可靠性的维修系统以保证反应堆部件的结构完整性,需要进一步发展用于检测疲劳损伤的分析和诊断技术。本文采用电子背散射衍射(EBSD)和透射电镜(TEM)对循环加载的316型奥氏体不锈钢进行了晶体取向分析和显微组织观察,阐明了疲劳循环引起的晶体取向变化与微观组织的关系。通过EBSD分析与TEM观察的对比,认为EBSD分析发现的局部错取向的变化是由于TEM观察发现的位错胞结构的形成。
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引用次数: 3
Stress analysis of a light-cured composite resin due to polymerization shrinkage 光固化复合树脂聚合收缩应力分析
Pub Date : 2013-10-10 DOI: 10.1299/KIKAIA.79.1406
K. Arakawa, Sane Jae Yoon, M. Nishimura
This study examined the shrinkage stress of a light-cured composite resin on cavity wall experimentally and analytically. The shrinkage force was measured using artificial cylindrical cavities fabricated in two stainless steel plates and a load-cell attached to the steel plate. An analytical model was introduced to evaluate the stress distribution in the cavities and to compare the shrinkage force experimentally determined, and following results were obtained: (1) The shrinkage force was dependent on both the cavity depth and irradiation time of the resin. (2) The analytical model can predict all the important features of the shrinkage force. (3) The stress on the cavity wall was dependent on the irradiation time.
本文对光固化复合树脂在空腔壁上的收缩应力进行了实验和分析研究。收缩力的测量采用在两块不锈钢板上制造的人造圆柱形空腔和连接在钢板上的测力元件。采用解析模型对空腔内的应力分布进行了分析,并与实验测定的收缩力进行了比较,得到了以下结果:(1)收缩力与空腔深度和树脂辐照时间有关。(2)该分析模型可以预测收缩力的所有重要特征。(3)腔壁上的应力与辐照时间有关。
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引用次数: 0
Time-dependent deformation of CFRP quasi-isotropic laminates caused by relaxation of thermal residual stress and physical aging 热残余应力松弛和物理老化引起的CFRP准各向同性层合板的时效变形
Pub Date : 2013-08-19 DOI: 10.1299/KIKAIA.79.950
Tomoyuki Niwa, Y. Arao, H. Kawada
In this paper, time-dependent dimensional change in quasi-isotropic laminates induced by relaxation of thermal residual stress and physical aging was predicted by the classical lamination theory. CFRP with pitch-based carbon fiber and cyanate ester resin was chosen for the study. Viscoelastic properties were investigated by performing tensile creep test for unidirectional laminates in the transverse direction. In addition, shrinkage strain induced by physical aging was studied by measuring the strain change of unidirectional laminates as well. Shrinkage strain in off–axis layers was calculated by using the coordinate-transform method. Shrinkage strain in 60° and 45° laminates were measured and the results were compared with the calculation. From the comparison, it was found that shrinkage strain of off-axis layers can be calculated by using the coordinate-transform method. Experimental results were applied to the classical theory in order to predict the time-dependent dimensional change of quasi-isotropic laminates. The strain change in quasi-isotropic laminates was obtained experimentally, and the result was compared with the prediction. It was verified that the time-dependent deformation of quasi-isotropic laminates can be predicted with a -order by using proposed prediction method.
本文用经典层合理论预测了由热残余应力松弛和物理老化引起的准各向同性层合板的时变尺寸变化。选择沥青基碳纤维和氰酸酯树脂复合的CFRP材料进行研究。通过横向拉伸蠕变试验研究了单向层合板的粘弹性。此外,还通过测量单向层合板的应变变化,研究了物理时效引起的收缩应变。采用坐标变换法计算了离轴层的收缩应变。测量了60°和45°层合板的收缩应变,并与计算结果进行了比较。通过比较发现,可以用坐标变换法计算离轴层的收缩应变。为了预测准各向同性层合板尺寸随时间的变化,将实验结果应用于经典理论。实验得到了准各向同性层合板的应变变化,并与预测结果进行了比较。结果表明,所提出的预测方法可以用- 2022阶来预测准各向同性层合板的随时间变形。
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引用次数: 1
期刊
Transactions of the Japan Society of Mechanical Engineers. A
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