Room temperature tensile deformation behavior of a Ni-based superalloy with high W content

K416B Ni-based superalloy with high W content has good high temperature properties and low cost, which has a great development potential. To investigate the room temperature tensile property and the deformation feature of K416B superalloy, tensile testing at room temperature was carried out, and optical microscopy (OM), scanning electron microscopy (SEM) and transmission electron microscopy (TEM) were used to analyze the deformation and damage mechanisms. Results show that the main room temperature tensile deformation features of the K416B nickel-based superalloy are dislocations slipping in the matrix and shearing into γ′ phase. The <110> super-dislocations shearing into γ′ phase can form the anti-phase boundary two coupled (a/2)<110> partial-dislocations or decompose into the configuration of two (a/3)<112> partial dislocations plus stacking fault. In the later stage of tensile testing, the slip-lines with different orientations are activated in the grain, causing the stress concentration in the regions of block carbide or the porosity, and cracks initiate and propagate along these regions.

     

铸造镍基高温合金增材修复技术的研究现状

铸造镍基高温合金广泛用于燃气轮机与航空发动机叶片等高温部件,长时间运行过程中经常发生叶片局部损伤失效,其维修或更换成本极高.通过增材修复来恢复局部损伤叶片的性能,将极大地降低制造成本、缩短制造周期、节约资源,具有极大的社会效益和市场价值.本文针对燃气轮机与航空发动机用铸造镍基高温合金部件的服役工况与失效形式,结合铸造镍...     

航空航天用金属表面热防护涂层的研究进展

高温合金材料凭借其优异的综合性能而广泛应用于航空航天领域热端部件.近年来,随着航空航天技术的不断发展,飞行器的热端部件正逐渐面临着更为严峻和复杂的服役环境,因此对高温合金的耐高温、抗氧化等使用性能提出了更高的要求.表面涂层技术由于具有约束条件少、可设计性强、技术类型和材料的选择空间大、经济环保等优点,成为目前最常用的热...     

DZ125高温合金超高周疲劳裂纹萌生与扩展

裂纹的萌生与扩展是研究合金材料超高周疲劳行为的重要方面.本研究分析与探讨了温度和表面状态对DZ125合金的超高周疲劳裂纹萌生与扩展特征的影响.不同温度下,DZ125合金的超高周疲劳裂纹萌生位置和扩展方式不同.室温下,裂纹均沿表面起源,裂纹扩展以拉伸模式为主;700 ℃下,裂纹均沿亚表面起源,裂纹扩展以剪切模式为主.室温下,DZ125合金经激光冲击处理前后的超高周疲劳裂纹萌生位置和扩展方式均存在差异.经过激光冲击处理后,裂纹萌生于合金的内部孔洞缺陷,裂纹扩展完全以剪切模式进行.     

不同气氛对激光熔覆IN718涂层形貌、组织与性能的影响

目的研究不同气氛条件下激光熔覆IN718高温合金涂层的微观偏析。方法利用激光熔覆技术,在不同送粉气和不同保护气条件下制备了IN718高温合金涂层,并对制备的涂层进行双时效热处理。采用光学显微镜观察显微组织结构和特征,采用扫描电镜和能谱仪对涂层组织和相成分进行分析,采用维氏硬度计对涂层热处理前后的硬度进行测定。结果送粉气种类对熔覆层的形貌和组织有一定影响,而保护气种类对熔覆层的形貌和组织影响不明显。与氩气作为送粉气制备的涂层相比,氦气作为送粉气制备的涂层组织更加细密,Laves相的尺寸更小且分布更均匀,Laves相的体积分数由氩气送粉的9.35%减少到氦气送粉的5.25%,并且Laves相中Nb的质量分数由20%下降到16%,涂层硬度由287HV0.2提高到306HV0.2。双时效热处理后,涂层的显微硬度明显提高,氦气作为送粉气制备的涂层硬度为468HV0.2,高于氩气作为送粉气制备的涂层硬度447HV0.2。结论氦气作为送粉气能有效降低激光熔覆IN718涂层的Nb元素偏析,同时细化涂层组织,提高涂层显微硬度。氦气作为保护气对涂层形貌和组织的影响不明显。     

喷丸对一种单晶合金表面完整性和高温缺口疲劳性能的影响

研究了喷丸后单晶合金的表面完整性和高温缺口疲劳性能。喷丸后表面形貌采用白光干涉仪表征,扫描电镜,2个方向观察(平行于受喷表面和截面方向)高分辨透射电镜和电子背散射衍射分析,疲劳性能采用旋转弯曲疲劳模式表征。采用旋转弯曲疲劳极限表征了强化增益作用,并与喷丸显微组织建立联系。结果表明,在760℃到850℃区间,喷丸强化较原始加工状态的疲劳极限增益达到14.8%,主要原因是高密度的缠结位错、加工硬化和晶粒错配。此外,通过表面应力集中系数计算表明,即使在平均粗糙度Ra升高的基础上,喷丸强化后表面应力集中系数也降低。     

Ni-Based Metallic Glass Composites Containing Cu-Rich Crystalline Nanospheres

In this work, a quaternary Ni–Cu–Nb–Ta system has been designed to obtain composite microstructure with spherical crystalline Cu-rich particles embedded in amorphous Ni-rich matrix. The alloy samples were prepared by using singleroller melting-spinning method. The microstructure and thermal properties of the as-quenched alloy samples were characterized by X-ray diffraction, scanning electron microscopy, high-resolution transmission electron microscopy, and differential scanning calorimetry. It shows that the spherical crystalline Cu-rich particles are embedded in the amorphous Ni-rich matrix. The average size of the Cu-rich particles is strongly dependent upon the Cu content. The effect of the alloy composition on the behavior of liquid–liquid phase separation and microstructure evolution was discussed. The phase formation in the Ni-based metallic glass matrix composite was analyzed.     

剪切载荷条件下镍基单晶合金裂纹扩展与微观结构演化行为研究

目前拉伸载荷下的镍基单晶合金的力学性能研究较为广泛,而剪切载荷对镍基单晶合金的力学性能也十分重要但缺乏研究。本文利用分子动力学方法研究了镍基单晶合金在剪切载荷下的裂纹扩展和微观结构演化,分析了应力-应变、势能和裂纹生长速率的变化。同时,揭示了温度和剪切应变率对裂纹扩展和微观结构演化的影响。结果表明,临界分切应力随温度的降低和应变速率的增大而增大;随着温度的升高以及剪切载荷下发生剧烈的热运动,裂缝表现为加速扩展的趋势;而在较高的应变率影响下,会形成位错塞积和孪晶,出现加工硬化现象。     

Steam reforming of n-hexadecane over noble metal-modified Ni-based catalysts

Steam reforming of n-hexadecane, a main constituent of diesel, over noble metal-modified Ni-based hydrotalcite catalyst was carried out in a temperature range of 700–950 °C, at an atmospheric pressure with space velocity of 10,000–100,000 h⁻¹ and feed molar ratio of H₂O/C = 3.0. The catalysts were prepared by a co-precipitation and dipping methods. The noble metal-modified Ni-based hydrotalcite catalyst displayed higher resistance for the sintering of active metal than the Ni-based hydrotalcite catalyst prepared by the conventional method. It was found that the Rh-modified Ni-based catalysts showed high resistance to the formation of carbon compared to Ni-based catalysts. The results suggest that Rh-modified Ni-based catalyst can be applied for the steam reforming (SR) reaction of diesel.     

晶界滑移对镍基合金失延开裂的影响

为了研究镍基合金焊材FM-52M的高温失延裂纹(DDC),采用改进的应变-裂纹(STF)实验方法,提出新的裂纹敏感性判据——晶界滑移量。并将之与裂纹数量相结合定量评估不同温度、不同变形量条件下材料的DDC敏感性。结果表明:本研究中所得到的材料临界变形量6%大于传统STF方法得到的4%的临界变形量。预热处理、峰值温度、变形速率等条件都能显著影响DDC的敏感性。此外,利用显微硬度标记了许多微区,并对实验前后的微区进行了SEM观察,探讨晶界滑移与析出物在DDC的萌生与扩展过程中的作用。