Ablation behavior of thin-blade co-deposited C/Cx-SiCy composites under the influence of the complex fluid conditions of the oxyacetylene torch

This paper offers a new way of testing the ablation property of material under an oxyacetylene torch using a thin-blade specimen, which costs much less time to reach the maximum temperature and provides a harsh turbulence fluid field that's closer to reality. The thin-blade specimen experiences a higher turbulent intensity than the traditional disk-like specimen, leading to more efficient heat exchange. The fluid field simulation agrees with the testing results. In addition, we manage to synthesize the C/Cx-SiCy composites with the co-deposition chemical vapor infiltration (CVI) method. The C/Cx-SiCy composites exhibit a similar anti-ablation property as C/C composites and consist of enough SiC phase simultaneously, combining the advantages of both C/C composites and C/SiC composites. The thin-blade C/Cx-SiCy composites show a lower linear ablation rate (1.6 μm/s) than C/C composites (4.1 μm/s) and C/SiC composites (19.6 μm/s) during the oxyacetylene test. The glass layer formed on the surface of C/Cx-SiCy could cling to the bulk material instead of peeling off due to the high PyC content in the matrix could protect the SiO₂ from blowing away.     

丙烯酸装置循环气压缩机叶片损伤分析与修复

某石化公司丙烯酸装置循环气压缩机在运行过程中,一级叶片突然发生断裂,导致机组停机。采用宏观检查、扫描电子显微镜、能谱分析等方法对断裂叶片进行检验和检测,将断裂叶片的材质、裂纹及断口特征检测结果与疲劳断裂特征和机组运行状况进行对比,确定压缩机叶片的断裂系其达到疲劳寿命所致,提出采用激光熔覆方法对压缩机叶片进行修复,介绍了修复工艺操作程序要点,可为同类故事的处理提供参考。     

Numerical study of a concept for major repair and replacement of offshore wind turbine blades

Repair and replacement of offshore wind turbine blades are necessary for current and future offshore wind turbines. To date, repair activities are often conducted using huge jack‐up crane vessels and by applying a reverse installation procedure. Because of the high costs associated with installation and removal of offshore wind turbine components and the low profit margin of the offshore wind industry, alternative methods for installation and removal are needed. This paper introduces a novel concept for replacement or installation of offshore wind turbine blades. The concept involves a medium‐sized jack‐up crane vessel and a tower climbing mechanism. This mechanism provides a stable platform for clamping, lowering, and lifting of a blade. A case study of a 5‐MW offshore wind turbine is shown, where common engineering practices were applied and numerical simulations of the marine operations were carried out using finite element and multibody simulation tools. Operational limits for wave and wind actions were established to demonstrate the technical feasibility of the proposed concept.     

径向式汽轮机叶轮参数分析及优化

径向式汽轮机叶轮的叶片角度,叶轮进口直径和叶片宽度等因素直接影响着它的蒸汽利用率和机械效率。针对目前径向式汽轮机效率不高,能量损失偏大等问题,以某径向式汽轮机叶轮为研究对象,利用Proe、Ansys等软件对其进行流体域建模,然后进行网格划分、数值模拟、流场分析等一系列工作,分析了该径向式汽轮机的工作效率和损失,并提出了优化叶轮参数的具体方法。     

5 000 t公务船调距桨桨叶数选型研究

针对国内外调距桨桨叶数选型依靠经验为主，对不同桨叶数对推进器整体性能的影响始终缺乏定量分析的现状，以某5 000 t公务船为目标船型，通过调距桨分别配置不同的桨叶数，分析不同桨叶数对目标船型综合性能的影响。总结了公务船调距桨桨叶数选型的方法，归纳了不同叶数调距桨的优劣，可为后续新造船桨叶数的选取提供参考。     

航空发动机复杂扭曲叶片分步电解加工研究

为实现复杂扭曲叶片在较小间隙下的稳定加工,提出了一种分步式电解加工的工艺方法,建立了复杂扭曲叶片小间隙(0.2 mm)和大间隙下(0.5 mm)扭曲流道的流道模型,采用有限元法进行了流场仿真研究,结果表明增加流道间隙可以解决流道中涡流和流场紊乱的问题。开展了复杂扭曲叶片小间隙连续式加工和分步式加工的试验研究。结果表明,采用小间隙连续式加工,当阴极进给至3.8 mm位置时,在叶片排气边靠近叶根流道扭曲处出现短路打火情况;而采用分步式加工方式能够实现加工的顺利进行。     

TRT叶片腐蚀与磨损的研究

研究了TRT叶片腐蚀磨损的原理,选择合适的材料,采用合理的喷涂方式,通过实验表明,试样1(Co-87WC)涂层是抗冲蚀磨损的最佳选择,而试样4涂层(Ti N)则不适合TRT叶片的使用环境。     

基于儒可夫斯基变换的涡轮钻具叶片设计及性能分析

为提高涡轮钻具叶片使用性能和创新叶片设计理论,提出了基于儒可夫斯基保角变换法与经典水力翼型相结合的涡轮钻具叶片设计新方法,以?127涡轮钻具叶片为研究对象,运用搭建的涡轮钻具叶型参数化设计平台和自主设计的涡轮钻具性能测试台架,完成了5种翼型的造型设计,研究了5种叶片流场性能,开展了设计叶片的性能测试实验,对比分析了设计叶片与塔里木油田某型在役?127涡轮叶片的实际效能。实验及仿真结果表明,基于新方法设计的NACA-0012翼型加厚叶片在600 r/min转速及15 L/s流量的设计工况下,其单级扭矩达5.83 N·m,较相同条件下某在役?127涡轮的单级扭矩提高约6.4%,级效率提高约1.16%,整体性能有了实质提升。     

划片刀配方对砷化镓晶圆切割崩裂的影响

利用试验设计方法(design of experiment, DOE)，以不同配方的划片刀划切砷化镓晶圆，并检测其正、背、侧面的崩裂尺寸，找出划片刀配方对砷化镓晶圆切割崩裂尺寸的影响规律。研究表明:划片刀的磨料粒度与砷化镓晶圆切割质量密切相关，即磨料粒度越细，正、背、侧面崩裂尺寸越小；而磨料浓度和结合剂强度与砷化镓晶圆正、背、侧面的切割质量相关性并不显著。可通过缩小磨粒尺寸的方式提高划切质量，并视情况调整磨料浓度和结合剂强度。      

混合叶片吸力面径向槽对燃烧室性能影响的数值研究

为了分析混合叶片吸力面上的径向槽对超紧凑燃烧室性能的影响,基于Wilson混合叶片的试验,设计了6种不同二次气流量的工况,利用FLUENT软件的Realizable k-ε湍流模型、混合分数/概率密度函数(PDF)燃烧模型、离散坐标(DO)辐射模型和离散相模型对燃烧室的流动及燃烧进行数值模拟。结果表明:随着二次气流量的增加,燃烧环内压力和离心力逐渐增大;二次气流量的变化对燃烧效率影响较小,对出口燃气温度分布系数、压力损失和出口污染物排放量影响较大;叶片径向槽起到了迁移环内燃烧产物和进一步掺混燃油和空气的重要作用,改善了出口燃气径向平均温度分布,提高了出口燃气温度场品质。