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FeNi基r'沉淀强化抗氢合金氢脆机理的研究
其他题名Study on the Hydrogen Embrittlement Mechanism of FeNi Based r' Strengthened Austenitic Alloys
张建
学位类型博士
导师戎利建
2008-05-23
学位授予单位中国科学院金属研究所
学位授予地点金属研究所
学位专业材料加工工程
关键词Feni基奥氏体合金 析出相 氢脆机理 正电子湮没寿命 氢致内耗
摘要本文采用透射电镜、扫描电镜、EDS、快-快符合正电子湮没寿命谱、动态机械分析仪、高压热充氢以及不同温度拉伸等试验方法系统地研究了两类FeNi基r'相沉淀强化奥氏体合金的氢脆机理。研究了合金中析出相的形貌、数量和分布,及析出相对合金氢脆性能的影响。同时还探讨了氢含量、预变形等实验条件对合金抗氢脆性能的影响以及最后一火锻造变形量对合金力学性能的影响。 正电子湮没寿命实验结果表明,充氢使固溶态合金中的空位减少,空位团和韧窝数量增多。在峰值时效态合金中,当r'相和r基体共格时,r'与r的界面不是氢陷阱,当r'相尺寸增大与r基体失去共格关系后,r'与r的界面成为氢陷阱。过时效合金中的晶界碳化物是氢的强陷阱,它能够吸引氢聚集到晶界,造成沿晶断裂。在720 ℃时效过程中,随着时效时间增加,晶界碳化物增多,氢致塑性损减增加,沿晶界断裂特征愈加明显。 内耗实验结果表明,在充氢合金中氢引起一个内耗峰,峰的高度随着氢的释放而降低,激活能计算显示该峰是由于氢和含有大量eta相和少量碳化物的晶界相互作用造成的。氢致内耗峰的出现说明含有eta相和碳化物的晶界是氢的强陷阱,氢在晶界聚集造成明显的塑性损减和沿晶断裂。添加硼后,合金的晶界上没有观察到eta相,只有少量碳化物。此时的氢致内耗峰出现在较低温度,表明晶界吸引氢的能力被减弱,氢在晶界的聚集减少。力学性能试验结果表明合金的氢致塑性损减下降,沿晶断裂倾向减小。 氢含量、预变形、应变速率和试验温度等都对合金的抗氢脆性能有明显影响。随着氢含量增加,时效合金中位错切割粒子的应力下降,位错可动性增加,平面滑移加强,交滑移减弱,氢脆敏感性增大。随着预变形量增加,时效合金中的位错密度增大,氢降低位错的开动应力导致塑性增加,氢致塑性损减相应下降。 为了提高合金的室温和高温力学性能,最后一火锻造变形量应控制在10~15%之间。当最后一火锻造变形量小于10%时,晶粒大小不均匀,存在粗大晶粒;而当最后一火锻造变形量大于15%时,晶粒内又会出现大量孪晶和碳化物,这些都不利于合金性能的提高。
其他摘要TEM, SEM, fast-fast coincidence positron annihilation spectra, dynamic mechanical analysis(DMA), thermal hydrogen charging and tensile tests at different temperatures have been used to study the hydrogen embrittlement mechanism of two types of FeNi based r'phase-strengthened austenitic alloys. The morphology, number and size of precipitates, and their influences on the hydrogen embrittlement of the alloys have been investigated. The effects of experimental conditions such as, hydrogen concentration, tensile rate on the hydrogen embrittlement of the alloys, and the effect of last pass forging deformation on the mechanical properties have been investigated as well. The results of positron annihilation experiments show that hydrogen charging decreases the number of vacancy and increases the number of vacancy cluster in the solution-treated alloy. In the aged alloy, when r'phase and r matrix are in coherency, the r'-r interfaces are not traps for hydrogen atoms. However, the loss of coherency due to the growth of r' phase leads the r'-r interfaces to become traps for hydrogen atoms. In the overaged alloy, hydrogen atoms are trapped by a significant number of grain-boundary carbides, resulting in a dramatic loss of plasticity and intergranular fracture. Experimental alloys aged at 720 ℃ for different time validates that, the amount of grain-boundary carbide increases with the increasing of aging time, which results in increase tendency of the loss of plasticity and intergranular fracture with the aging time. Internal friction measurements on DMA indicate that hydrogen induced an internal friction peak in the experimental alloy. The height of the peak decreased as the degassing of hydrogen. The calculated activation energy suggests that the peak is caused by the interaction between hydrogen atom and grain boundaries which are decorated with a significant amount of eta phases and a few of carbides. It is revealed that the grain boundaries are strong traps for hydrogen atoms, and the accumulation of hydrogen atoms at the grain boundaries causes plasticity loss and intergranular fracture. Addition of boron can suppress the precipitation of eta phases at grain boundaries. The hydrogen-induced internal friction peak for the alloy with boron appears at a lower temperature and has smaller activation energy. It is implied that due to the introduction of boron, the interactions between hydrogen and the grain boundaries decrease, and less hydrogen atoms accumulate at grain boundaries. Testing conditions such as hydrogen concentration, predeformation, strain rate and test temperature can remarkablely influence hydrogen embrittlement of the alloy. As the hydrogen concentration increases, the stress needed to cut particles for dislocation is decreased and the mobility of dislocation is increased, and coplanar slipping is enhanced while cross slipping is weakened, resulting in the decrease of hydrogen-induced plasticity loss. When the predeformation increases, the density of dislocation goes up, hydrogen reduces the starting stress of dislocation movement, leading to the increase of plasticity and the decrease of hydrogen-induced plasticity loss. The last pass forging deformation should be controlled in the range of 10-15% in order to improve the room-temperature and high-temperature properties of the alloy. When the last pass forging deformation is less than 10%, the grain size is not homogeneous and super coarse grains still exist, while the last pass forging deformation is larger than 15%, a significant number of twin boundaries and carbides appear within grains, and all of those are harmful to properties of alloy.
页数138
语种中文
文献类型学位论文
条目标识符http://ir.imr.ac.cn/handle/321006/17164
专题中国科学院金属研究所
推荐引用方式
GB/T 7714
张建. FeNi基r'沉淀强化抗氢合金氢脆机理的研究[D]. 金属研究所. 中国科学院金属研究所,2008.
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