Development of microstructural inhomogeneity in multi-pass flow forming of TA15 alloy cylindrical parts

Revealing the development of microstructural inhomogeneity in the multi-pass flow forming of titanium alloy components is of great significance to the microstructure control and property tailoring. To this end, the microstructural inhomogeneity of TA15 alloy spun cylindrical parts was analyzed based on the deformation history. The results indicate that the material underwent significant compressive strain in the normal direction (ND), tension strain in the rolling and circumferential directions (RD and CD), while tension strain in the CD is slightly small due to the limited material flow in this direction. These strain characteristics make the microstructure, especially the primary α (α_p), present different morphologies in the different planes of the part. Meanwhile, the combined effects of inhomogeneous deformation and temperature distribution in the ND also cause the inhomogeneity of microstructure morphology and parameters in this direction. Quantitative analyses show that with the forming pass increasing, the aspect ratio of α_p increases most in the normal-rolling plane, then in the normal-circumferential plane and least in the circumferential-rolling plane, whereas α_p content decreases in an opposite trend. Along the ND, the aspect ratio and content of α_p is relatively high in the outer and inner surface areas but lowest in the central area, and these inhomogeneous characteristics can be gradually diminished with the forming pass increasing. Furthermore, the variation of hardness inhomogeneity factor indicates that a four-pass forming with the total reduction ratio of 63% could obtain a homogenous microstructure along the ND of the TA15 alloy spun cylindrical part.     

基体曲率对热障涂层结合强度影响的无损检测研究

 针对复杂型面航空发动机涡轮叶片表面热障涂层(TBCs)的失效问题,采用交流阻抗谱(IS)法和洛氏硬度(RH)压痕法对比研究了制备在平板基体和曲率基体上,热障涂层在热循环过程中微观结构和界面结合强度的演变规律。交流阻抗谱法的结果表明:两种涂层试样的热生长氧化(TGO)层厚度及陶瓷层内裂纹数量均随着热循环时间增加而增长,但曲率试样的微观结构恶化速度更快;洛氏硬度压痕法的结果验证了经热循环后,曲率基体上热障涂层界面结合强度低于平板样品。     

工件底孔直径对Q460高强度钢冷挤压内螺纹的影响

试验研究了工件底孔直径对Q 460高强度钢冷挤压内螺纹的影响,包括分析工件不同底孔直径下内螺纹牙形、表面残余应力、硬度及端面表面形貌的变化。结果表明,冷挤压加工后内螺纹端面堆积体呈两边高、中间低的凹陷形,随着工件底孔直径的减小,端面堆积的高度不断增加,堆积程度也就变得愈加严重,螺纹牙顶、牙侧与牙根处表层硬度与表面残余压应力均升高。工件底孔直径的选择,在正确保证螺纹质量和丝锥寿命的前提下应尽可能取最大值,但是,一般情况下没有必要过分要求最高的牙高率,否则将给内螺纹挤压成形带来许多困难。Q 460高强度钢冷挤压内螺纹的工件底孔直径最佳取值范围为21.20～21.30 mm,牙高率超过80%,完全符合螺纹质量要求。     

乏信息材料布氏硬度测量误差的灰自助预报

乏信息材料布氏硬度测量误差的预报是硬度计量领域的新兴课题,有别于传统的统计学理论,综合灰色系统理论和自助法的理论知识,提出一种实现乏信息材料布氏硬度测量误差预报新方法.对小样本空间的材料布氏硬度测量数据中各误差源影响进行标定,计算各误差源对测量结果的误差传递系数,并对各误差源数据序列进行自助法抽样,通过灰自助融合建模获得误差源标定预测值;按照误差合成的方法实现乏信息材料布氏硬度测量误差的灰自助预报.通过具体的实例进行计算,所得的预报结果与采用标准硬度机所得测量结果一致,验证了乏信息材料布氏硬度测量误差灰自助预报新方法.     

LY2铝合金的激光冲击强化区硬度和残余应力测试分析

为了研究激光冲击处理对LY2航空铝合金力学性能的影响,采用Nd:YAG激光器对航空铝合金LY2进行了激光冲击强化处理,测定其显微硬度和残余应力.结果表明,经过激光冲击处理后,试样表面没有受强脉冲激光和冲击波的破坏,而显微硬度和残余压应力明显提高,激光冲击处理后的强化区与光斑相当,深度约为1.2mm.     

超声波硬度传感器在大口径管件内镀层硬度测量中的应用

通过分析超声波硬度传感器的特点,提出采用超声波硬度传感器技术实现对管件镀层硬度进行现场无损测量的方法.     

基于数字图像处理的布氏硬度压痕直径测量方法

在分析布氏硬度试验压痕图像的基础上,提出了基于数字图像处理的布氏硬度压痕直径测量方法.利用CCD相机获取压痕图像,通过图像分割、目标区域处理、压痕圆拟合等步骤完成图像处理,由此实现对压痕尺寸的自动精确测量.     

钽的氮离子注入法研究

实验研究证实，通过氮离子注入的方法对钽基材进行表面强化，可大大提高钽村的表层硬度及耐蚀性能。俄歇电子能谱及Ｘ射线衍射分析表明，Ｔａ注入Ｎ＋后生成了新相ＴａＮｏ．１。     

Radiation testing of a commercial 6-axis MEMS inertial navigation unit at ENEA Frascati proton linear accelerator

We present the first results of a novel collaboration activity between ENEA Frascati Particle Accelerator Laboratory and University La Sapienza Guidance and Navigation Laboratory in the field of Radiation Hardness Assurance (RHA) for space applications.The aim of this research is twofold: (a) demonstrating the possibility to use the TOP-IMPLART proton accelerator for radiation hardness assurance testing, developing ad hoc dosimetric and operational procedures for RHA irradiations; (b) investigating system level radiation testing strategies for Commercial Off The Shelf (COTS) components of interest for SmallSats space missions, with focus on devices and sensors of interest for guidance, navigation and control, through simultaneous exploration of Total Ionizing Dose (TID), Displacement Damage (DD) dose and Single-Event Effects (SEE) with proton beams.A commercial 6-axis integrated Micro Electro-Mechanical Systems (MEMS) inertial navigation system (accelerometer, gyroscope) was selected as first Device Under Test (DUT). The results of experimental tests aimed to define an operational procedure and the characterization of radiation effects on the component are reported, highlighting the consequence of the device performance degradation in terms of the overall navigation system accuracy. Doses up to 50 krad(Si) were probed and cross sections for Single-Event Functional Interrupt (SEFI) evaluated at a proton energy of 30 MeV.     

洛氏硬度标准装置不确定度的评定

详细给出了洛氏硬度标准装置不确定度的评定方法及步骤。