YT62型液力偶合器故障分析及处理

针对YT62型液力偶合器在实际运行过程中经常出现的泵轮侧推力轴承温度偏高、泵轮和涡轮侧推力瓦块烧毁以及泵轮叶片断裂等故障进行分析及探讨,提出了改造偶合器泵轮侧推力瓦块定位盘,扩大泵轮侧径向推力轴瓦中分面的油槽通流面积,在断裂的泵轮叶片最接近180°对称的叶片上挖去和断裂叶片大小相同的部分,将转子动平衡校验后回装等处理方法和改进措施。改进后的实际运行效果表明,设备安全可靠性得到了很大提高,运行良好。     

Numerical Simulation on Effects of Pressure Distribution of Wind Turbine Blade with a Tip Vane

It is important to study the pressure distribution on the blade and in the adjacent area while searching the poweraugmentation theory with adding a tip vane to the wind turbine.This paper shows the CFD simulation relation-ship of the pressure distribution on the rotor blade and in the adjacent area,after calculating the pressure of thedifferent chordwise and spanwise point on the blade with the tip vane-V(8.8x8) and without the tip vane under tipspeed ratio λ4.5.Combining the isobaric section figure in certain location,it can be seen that the tip vane im-prove the pressure difference between pressure and suction surface.The most influenced zone is found and thesecan further display the power augmentation theory of the wind turbine using the tip vane.The simulation calcula-tion was based on N-S equations.3-D,steady,implicit solver was chosen.Turbulence model was k-ω SST.Dis-cretization scheme is SECOND ORDER UPWIND.Pressure-velocity coupling was a typical SIMPLE scheme.Inthe whole grid system,two-divided grid formation was adopted,that is,inner region and outer region.Inner re-gion including rectangular solid blade and neighboring,outer region is semi-cylinder.There were together720,000 nodes with tetra-prism unstructured mesh.     

9H级燃气-蒸汽联合循环机组主厂房结构设计方案研究

目的 针对9H级燃气-蒸汽联合循环机组主厂房结构设计方案研究,找出最佳的主厂房布置。 方法 通过结构型式、计算方法及设计参数取值进行优化,对技术、初投资、建设工期及施工组织等方面进行详细论述与分析。 结果 分析结果表明：钢筋混凝土结构与钢结构均为可行的,考虑经济性等诸多因素,推荐采用钢筋混凝土结构,屋面采用钢屋架。 结论 主厂房结构采用钢筋混凝土结构,屋面主承重结构采用钢屋架。     

300 MW机组变压运行方式的研究

针对300 MW机组运行经济性问题,通过试验测定了不同负荷下定压运行或变压运行时的供电煤耗、热耗、汽耗、汽动给水泵单耗、再热汽温等指标,并进行了对比和分析。结果显示,机组负荷在240 MW以下时采用四阀全开变压运行比较经济。     

M701F型燃气轮机的在线运行负荷特性

分析了重型燃气轮机负荷特性的影响因素,提出了研究重型燃气轮机负荷特性的技术路线。基于此,针对某M701F型燃气轮机,以国际标准化组织(International Organization for Standardization,ISO)的标准条件为基准,由机组的在线运行数据获得其负荷特性曲线,并建立负荷特性的数学模型。考察该燃气轮机6 940组实际数据,得出结论:当折算基准功率不小于18MW时,其负荷特性数学模型的最大相对误差不超过5.73%。     

Internal surface protection of gas turbine blade by Si‐aluminide coating

A laboratory‐scale slurry silicoaluminizing process has been developed to apply coating into cooling passageways of a first‐stage gas turbine blade. Analytical techniques for characterizing the coatings comprised optical microscopy, SEM, EDS, and XRD. The results of metallographic examinations demonstrated that acceptable coatings had been formed in almost all of the passageways. The amounts of Al and Si in the topcoat were found to be in the ranges of 24–26 wt% and 4.5–6 wt%, respectively. The heat treated coating consisted largely of β‐NiAl phase as the coating matrix with uniform distribution of <2 µm‐size precipitates. In addition, oxidation and hot corrosion performance of the coatings were investigated by cyclic exposure to 1100 °C and the furnace method using a mixture of sodium sulfate‐40 wt% sodium vanadate‐10 wt% sodium chloride at 780 °C, respectively. It was found that the presence of Si in the coating improves both oxidation and hot corrosion Type II properties.     

Evaluation of wind load integration in disproportionate collapse analysis of steel moment frames for column loss

The design of steel structures, in most cases, depends majorly on the level of wind loads which are prescribed by codes and regulations and are used in the structural analysis due to the fact that steel structures being light and ductile systems are strongly affected from a slight difference in the values of wind loading. During the last decades, disproportionate collapse analysis has become of major interest mainly due to the increasing number of failures occurring in that pattern. Commonly accepted guidelines and methods of analysis have been produced, the most dominating of which being the Department of Defense Facilities criteria or DoD. In the DoD, as well as in other criteria, the event of a column loss is suggested as the modeling scenario which has to be sustained by a structural system in order to be robust. However, all the guidelines so far have disconnected the column loss analysis from wind loads and have only performed it for gravity loading. This paper presents the dynamic time history disproportionate collapse analysis of steel frames, including various levels of wind loading. Interesting aspects are discussed through the parametric analysis of five different numerical examples of moment resisting frames.     

Apparent wind load effects on the tether of a kite power generator

This paper is devoted to analytical modeling of apparent wind load effects on a tether constraining a power kite performing a fast crosswind motion. The refined crosswind motion law generalized for accounting the kite control is derived in the case of equilibrium motion of the kite. The paper also presents the study of the effect of tether sag based on the mathematical model of a gently sloping tether line.     

TC4钛合金风扇转子叶片模锻工艺和性能研究

研究了TC4钛合金风扇转子叶片的锻造加热工艺、模锻成形及热处理工艺。在叶片的各部位进行了室温和400℃拉伸试验、冲击试验、400℃持久试验,综合评价了模锻叶片的加工性能和叶片各部位的性能。结果表明,叶片各部位的力学性能分布较均匀,叶身的强度比叶顶和榫头的略高,塑性水平基本相同,即室温下三者的σb均值分别为966,962和963 MPa,σ0.2分别为916,905和912 MPa,δ5约为15%,ψ约为47%;400℃下σb均值分别为669和643 MPa,δ5约为16%,ψ约为67%。整体叶片具有均匀、良好的冲击性能,αkv,HB(d)均值分别为0.46 MJ.m-2,3.47 mm。同时,叶片在大载荷(σ为560 MPa)下具有良好的持久寿命(τ大于101 h)。     

An experimental study on self-output-control characteristics of micro downwind rotor with coning soft blades

In this short paper,we have treated the aerodynamic performance of micro downwind rotor with coning soft blades experimentally.The test wind rotor has the tip diameter of 1.5 m and three two-dimensional NACA0018 blades of 0.15 m chord whose material is light,soft and pliable foam plastic for perfect safety.From the wind tunnel test,it is realized that the performance is manageable by the coning angle of the rotor blade.In the present case,an improvement of the performance in lower wind speeds is achieved by...