中压进汽腔的流场数值模拟比较

通过数值模拟计算,对中压对称进汽和切向进汽两种结构的流场进行了分析比较,结果表明,单一切向进汽腔的总压损失更小,出口汽流角的周向分布均匀度更好。更进一步,为整体评估中压进汽腔的流场以及对叶片级的流动影响,对中压进汽腔及第1级叶片的整体流体域流场情况进行了分析比较,结果表明,采用大几何角静叶的切向进汽腔气动性能最优;当采取切向进汽腔时,需合理选择第1级静叶几何角并耦合计算,才能实现进汽腔的气动优化。     

Identification of Thiols in Yellow Onion (Allium cepa L.) Using Solvent Vented Large Volume Injection GC‐MS

Thiols are often highly odor active molecules and as such can significantly contribute to aroma while being present at extremely low concentrations. This paper details the identification of thiols in yellow onion juice by solvent extraction followed by thiol enrichment using a mercuric agarose gel column. Due to the inherent thermal instability and low concentrations of thiols in onion, chromatographic analysis utilized larger volume solvent elimination injections. New sulfur compounds in onion included 1,1‐propanedithiol, bis‐(1‐sulfanylpropyl)‐sulfide, 1‐methylsulfanyl‐1‐propanethiol, 1‐propylsulfanyl‐1‐propanethiol, and 1‐allylsulfanyl‐1‐propanethiol. A discussion on the potential route of formation for each compound is included along with the orthonasal and retronasal evaluations of the synthesized molecules. This work investigated and identified 5 newly identified compounds present in onions that can impart onion character at low concentrations levels.     

Methodology to determine the appropriate amount of excess air for the operation of a gas turbine in a wet environment

This paper addresses the impact of excess air on turbine inlet temperature, power, and thermal efficiency at different pressure ratios. An explicit relationship is developed to determine the turbine inlet temperature as a function of excess air, pressure ratio and relative humidity. The effect of humidity on the calculation of excess air to achieve a pre-established power output is analyzed and presented. Likewise it is demonstrated that dry air calculations provide a valid upper bound for the performance of a gas turbine under a wet environment.     

Numerical calculation of the dynamic behavior of solid particles through the inlet box with complex geometry of a fluid machine

A finite element method is used to calculate the three-dimensional gas flow field in the inlet box of a large-size fluid machinery,The dynamic behaviors of solid particles through the inlet box are obtained numerically by the “one way coupling” method .The trajectories of different-sized particles and the distribution of particle positions on the outlet plane of inlet box are investigated.     

Velocity profiles between two baffles in a horizontal circular tube

The shell and tube heat exchanger is an essential part of a power plant for recovering heat transfer between the feed water of a boiler and the wasted heat.The baffles are also an important element inside the heat exchanger.Internal materials influence the flow pattern in the bed.The influence of baffles in the velocity profiles was observed using a three-dimensional particle image velocimetry around baffles in a horizontal circular tube.The velocity of the particles was measured before the baffle and between them in the test tube.
Results show that the flows near the front baffle flow were parallel to the vertical wall,and then concentrate on the upper opening of the front baffle.The flows circulate in the front and rear baffles.These flow profiles are related to the Reynolds number（Re） or the flow intensity.The velocity profiles at lower Re number showed a complicated mixing,concentrating on the lower opening of the rear baffle as front wall.
Swirling flow was employed in this study,which was produced using tangential velocities at the inlet.At the entrance of the front baffle,the velocity vector profiles with swirl were much different from that without swirl.However,velocities between two baffles are not much different from those without swirl.     

液压冲击机构阀后腔缸体回油口设计研究

对液压冲击机构配油套阀后腔缸体回油位置变化对冲击性能参数影响的理论模拟和实验结果进行了分析、研究。为设计同类液压冲击设备提供了依据。     

Computations of Inlet／Isolator for SCRAMjet Engine

IntroductionThe Supersonic Combustion Ramjet (SCRAMjet)engine is an available air-breathing engine for the vehicleflying with a hypersonic velocity. Inletlisolator is one ofthe important parts of the SCRAMjet engine. It isutilized to enhance the static pressure and temperatllre ofthe inflow by using the dynamic pressure of itself. Theprinciple of integration designing must be kept for thevehicle flying at a high Mach "umbeL For theSCRAMjet engine, the character of the inlet not onlyaf…     

多层泄孔运行方式对二级斜坡进口浅水垫消力池水力特性的影响

针对某水电站工程消力池体型不合理及调度运行方式不当而导致池内流态不良、消力池临底流速过大、底板冲刷破坏等问题,通过1∶45模型试验分析了二级斜坡进口式浅水垫消力池在多层泄洪孔不同运行方式下的水力特性。结果表明,新提出的消力池体型能够明显改善面流流态及水跃不稳定等问题,针对该工程,优先采用溢流表孔泄流比采用冲沙底孔泄流池内流态更佳,消力池临底及岸边流速更低,消能防冲效果更好。     

基于功率前馈的燃气轮机可转导叶角度控制规律研究

针对某型发电燃气轮机在负载突变过程中可转导叶角度与压气机转速互相耦合、控制失稳的问题,提出了“功率前馈”控制策略——即根据负载功率对可转导叶角度进行调整。首先,通过粒子群寻优算法,将压气机喘振裕度作为目标,对不同工况下的导叶角度进行寻优匹配;其次,采用“功率前馈”对燃气轮机突增负荷和甩负荷过程中的导叶角度进行调节;最后,以船用发电型间冷燃气轮机为研究对象,建立三转子燃气轮机整机模型,针对突变工况过程可转导叶角度的控制规律开展研究。结果表明：采用“功率前馈”控制模式,在突增负荷过程中,动力涡轮转速超调量减小11%,高压涡轮进口温度降低了3%;在甩负荷过程中动力涡轮转速超调量减少10%,高压涡轮进口温度超调量降低11.9%,低压压气机最小喘振裕度由0.87%提高至9.1%。     

Effect of cathode inlet manifold configuration on performance of 10-cell proton-exchange membrane fuel cell

A 10-cell proton-exchange membrane fuel cell (PEMFC) stack with 10 cathode flow channels is employed to investigate the effect of airflow inlet manifold configuration on the overall performance. Four different types of airflow inlet manifold with a 90° turn are considered. First, the flow patterns according to the manifold configuration are numerically sought. The computational result for the improved inlet manifold predicts about 8.5% increase in the uniformity of the airflow distribution. The experiments are carried out to confirm the numerical predictions by measuring actual airflow distributions through the fuel cell stack. The polarization curve and the power curve for the 10-cell PEMFC are also obtained to determine the effect of inlet manifold configuration on the actual performance. The maximum power output increases by up to 10.3% on using the improved airflow inlet manifold.