JP60涡轮增压器压气机性能模拟与试验

本文采用Numeca数值分析软件建立了JP60增压器压气机总成内部网格模型,并计算出稳态增压器压气机性能曲线,将模拟结果与试验所测取的JP60压气机运行曲线进行了对比,结果表明：模拟分析曲线与试验曲线变化趋势一致。此外,对压气机内部流场的分布也进行了分析,为该增压器的优化设计提供理论依据。     

JP60涡轮增压器压气机性能模拟与试验

本文采用Numeca数值分析软件建立了JP60增压器压气机总成内部网格模型,并计算出稳态增压器压气机性能曲线,将模拟结果与试验所测取的JP60压气机运行曲线进行了对比,结果表明:模拟分析曲线与试验曲线变化趋势一致。此外,对压气机内部流场的分布也进行了分析,为该增压器的优化设计提供理论依据。     

车用涡轮增压器压气机叶轮强度计算与分析

通过对车用增压器压气机叶轮内应力特点的分析,确定了叶轮强度的计算方法,介绍了利用有限元分析软件对叶轮内部应力进行分析的过程,并就强度分析中的关键步骤和技术难点进行了讨论。通过有限元计算结果分析,找到了车用增压器压气机叶轮应力集中的位置,研究了如何利用几何参数的修改来减小集中应力。计算并讨论了叶片气动载荷和温度场对压气机叶轮应力的影响,建立了车用增压器压气机叶轮强度分析的过程和方法。     

增压器气动噪声特性及贡献度的数值分析

基于数值计算方法,研究了船用低速柴油机增压器气动噪声特性,并分析了压气机和涡轮对增压器气动噪声的贡献度。首先分别建立了压气机和涡轮的数值模型,计算了增压器设计工况下二者的非定常流场,并获取了用于噪声计算的声源信息;进一步采用声学边界元方法计算了压气机和涡轮的气动噪声。结果表明:压气机和涡轮气动噪声谱成分均为离散单音噪声和宽频噪声,噪声峰值依赖于叶轮叶片数;压气机气动噪声声压级明显高于涡轮气动噪声,是增压器主要噪声源。     

车用涡轮增压器压气机叶轮振动特性分析

利用CAD软件对增压器的压气机叶轮进行了三维实体造型,并运用有限元分析软件I-DEAS对叶轮进行振动特性分析,得到了叶轮在不同转速下的固有频率值及相应振型,通过Matlab软件绘制Camp-bell图,找到了叶轮容易发生共振时的转速和激振频率.从而为该增压器叶轮的优化设计提供依据.     

涡轮增压器压气机气体流动特性数值模拟研究

基于雷诺平均纳维-斯托克斯方程与Realizable k-ε双方程湍流模型,利用CFD软件建立了某型涡轮增压器离心式压气机内部气体的可压缩流动仿真模型。分析了不同工况下压气机的压比和效率随着流量的变化关系,深入研究了转子区域和扩压区域的气体流动速度与压力的分布、形成过程及相互影响。研究结果表明:增压器在28 200r/min时工作效率最高,叶轮主流叶片压力面中部靠近叶尖区域出现低压区引起的气体回流现象及叶片吸力面出现低压区引起的气体紊流现象是影响压气机效率变化的原因;叶片前缘及尾部流场特性存在较大差异;扩压器叶片入口处极易出现涡流损失。     

增压器压气机水冷蜗壳设计及其内部流场分析

提出对柴油机涡轮增压器的压气机进行冷却的方法——在原压气机蜗壳外部加装散热片与冷却水道,从冷却系统散热器后取水,实现增压与中冷的集成。建立离心式压气机整级物理模型,根据基于有限元的有限体积法,采用全隐式多网格耦合求解技术对不同冷却程度下的压气机内部非定常流动进行三维CFD模拟,考察了蜗壳内部压力场、速度场与气体密度的分布,为高原进气水冷需求论证提供参考,增压台架试验验证了模拟的准确性。研究结果表明:若冷却水可以使压气机出口温度降低10.3℃,压比最大增加11.8%,效率增加11.1%,气体密度最大增加12.8%;同时,流场沿蜗壳流程分布没有压力集中与显著涡流的出现,说明压气机蜗壳设计合理。     

蜗壳冷却对增压器压气机性能的影响分析

本文采用ANSYS-CFX对压气机进行三维流动数值模拟,获得了采用蜗壳冷却技术和不采用冷却技术两种情况下的压力和温度的三维流场分布情况,分析了蜗壳冷却技术对压气机流场的影响。结果表明,模拟计算结果与原机试验所测得的结果基本吻合,采用蜗壳冷却技术可以降低压气机出口空气的温度,增大出口空气的压力,进而提高增压器的充气密度,改善了增压器的性能,并为压气机蜗壳冷却技术的优化和改进提供参考。     

增压器压气机叶轮振动特性分析

利用I-DEAS软件对某型涡轮增压器的压气机叶轮进行三维建模，通过ANSYS软件对其进行振动特性分析，得出叶轮在不同转速下的模态参数。通过Matlab软件绘制Campbell图，分析叶轮发生共振时的转速，从而为避免产生共振及噪声提供理论依据。     

增压器压气机叶片结构/振动一体化优化设计

以废气涡轮增压器压气机叶轮为研究对象,创建了压气机叶片的三维参数化模型,通过全三维流场仿真分析,得到压气机的气动性能及叶片表面的压力分布.在不改变叶片形状、保证压气机气动性能的情况下,对叶片的静强度及振动特性进行了一体化优化设计.以叶片4个关键截面的叶顶、叶根厚度为设计变量,以离心力及气动压力作用下叶片的最大Mises应力、叶片的一阶动频为约束,以叶片体积为目标函数,在iSIGHT优化平台上集成了I-DEAS、ANSYS软件,采用混合整型优化和自适应模拟退火算法的组合优化方法,在满足叶片静强度小于屈服强度和一阶动频大于3倍工作频率的条件下,叶片体积(质量)减小了14.7%.     

进气畸变度及分布形式对跨音速轴流压气机工作特性的影响

为了研究进气畸变对压气机的工作特性以及稳定性的影响,以NASA Stage35型跨音速轴流压气机为研究对象,采用全通道计算模型对不同畸变程度和不同畸变分布形式条件下压气机的工作特性及内部流场变化规律进行数值模拟研究。结果表明:随着进气畸变度的不断增加,压气机的峰值效率逐渐下降,由畸变所引起的总压损失在压气机内部流道中逐渐扩大;在保持畸变度和畸变区域总面积不变的条件下,畸变区的分散程度对压气机在峰值效率点附近的工作特性影响较小,但随着畸变分布区分散程度的逐渐增加,压气机的稳定裕度有所提高,压气机内部流道中的总压损失和熵增也有所降低。     

Modeling of air compressor for proton exchange membrane fuel cell

空压机的性能对燃料电池的性能有很大影响,为准确建立空压机数学模型,使用等效电路结构方法,建立关于转速、流量、压力这三个变量的非线性函数。对空压机等效电路数学模型参数和空压机性能参数数据进行拟合,并根据拟合效果依次采用基于最大流量偏差和基于出口压力加权两种方法改进拟合方法,实现对静态模型较高精度的拟合。     

基于扩压因子流型的压气机快速性能预测算法

为快速、准确地获得压气机性能参数、完成压气机性能预测,实现压气机优化设计,基于流线曲率法,将扩压因子作为控制方程、损失模型、熵增修正模型及落后角模型中的关键参数,建立轴流压气机性能快速预测算法。利用该算法对某跨音速轴流压气机性能参数进行计算,并将计算结果与主流商业软件计算结果及试验数据进行对比。通过对比发现：该算法计算效率高,能够快速且较为准确地完成压气机整体性能和沿叶高方向流场参数的预测;计算范围广,在不同转速、不同流量等非设计工况下算法预测结果均与试验及数值模拟数据接近;所选取与完善的经验公式合理可靠,能够较好地描述压气机内部流动。     

Coordination control strategy for the air management of heavy vehicle fuel cell engine

Air supply system is an important subsystem in the fuel cell engine with strongly non-linear and coupling interactions. There are strong coupling problems between air flow and pressure in the air supply system, such as the air compressor and electronic throttle opening. This paper introduces a novel coordination control strategy for the air supply system of high power fuel cell engine in heavy truck. It consists of feed-forward and internal model decoupling control (IMC) with tracking an optimized working line of centrifugal air compressor. The strategy can maintain good control effect for model matching and model mismatching with robustness. The working efficiency of the centrifugal air compressor could be significantly increased and avoid the phenomenon of surge by the coordination control strategy. At the same time, the output current of fuel cell engine can meet the load requirement which has the short response time and good follow effect.     

Power and efficiency optimization for combined Brayton and inverse Brayton cycles

A thermodynamic model for open combined Brayton and inverse Brayton cycles is established considering the pressure drops of the working fluid along the flow processes and the size constraints of the real power plant using finite time thermodynamics in this paper. There are 11 flow resistances encountered by the gas stream for the combined Brayton and inverse Brayton cycles. Four of these, the friction through the blades and vanes of the compressors and the turbines, are related to the isentropic efficiencies. The remaining flow resistances are always present because of the changes in flow cross-section at the compressor inlet of the top cycle, combustion inlet and outlet, turbine outlet of the top cycle, turbine outlet of the bottom cycle, heat exchanger inlet, and compressor inlet of the bottom cycle. These resistances control the air flow rate and the net power output. The relative pressure drops associated with the flow through various cross-sectional areas are derived as functions of the compressor inlet relative pressure drop of the top cycle. The analytical formulae about the relations between power output, thermal conversion efficiency, and the compressor pressure ratio of the top cycle are derived with the 11 pressure drop losses in the intake, compression, combustion, expansion, and flow process in the piping, the heat transfer loss to the ambient, the irreversible compression and expansion losses in the compressors and the turbines, and the irreversible combustion loss in the combustion chamber. The performance of the model cycle is optimized by adjusting the compressor inlet pressure of the bottom cycle, the air mass flow rate and the distribution of pressure losses along the flow path. It is shown that the power output has a maximum with respect to the compressor inlet pressure of the bottom cycle, the air mass flow rate or any of the overall pressure drops, and the maximized power output has an additional maximum with respect to the compressor pressure ratio of the top cycle. When the optimization is performed with the constraints of a fixed fuel flow rate and the power plant size, the power output and efficiency can be maximized again by properly allocating the fixed overall flow area among the compressor inlet of the top cycle and the turbine outlet of the bottom cycle.     

Thermodynamic optimization for an open cycle of an externally fired micro gas turbine (EFmGT). Part 1: Thermodynamic modelling

The principle of optimally tuning the air flow rate and subsequent distribution of pressure drops is applied to optimize the performance of a thermodynamic model for an open regenerative cycle of an externally fired micro gas turbine power plant with pressure drop irreversibilities by using finite-time thermodynamics and considering the size constraints of the real plant. There are eight flow resistances encountered by the working fluid stream for the cycle model. Two of these, the friction through the blades and vanes of the compressor and the turbine, are related to the isentropic efficiencies. The remaining flow resistances are always present because of the changes in flow cross-section at the compressor inlet and outlet, the turbine inlet and outlet and the regenerator hot/cold-side inlet and outlet. These resistances associated with the flow through various cross-sectional areas are derived as functions of the compressor inlet relative pressure drop, and control the air flow rate and the net power output and thermal efficiency. The analytical formulae for the power output, efficiency and other coefficients are derived, which indicate that the thermodynamic performance for an open regenerative cycle of an externally fired micro gas turbine power plant can be optimized by adjusting the mass flow rate (or the distribution of pressure losses along the flow path). It is shown that there are optimal air mass flow rates (or the distribution of pressure losses along the flow path) which maximize the net power output.     

进口畸变下涡流发生器对压气机流场的影响

为研究进口总压畸变条件下涡流发生器对压气机流场的影响,建立单级轴流压气机模型,计算和分析了不同工况下的压气机内部流场.计算结果显示:在进口畸变条件下,压气机流场恶化,性能降低;使用涡流发生器后,可以有效改善静叶叶根附近的流场,控制叶片尾缘分离,降低沿叶高方向的压力波动,从而削弱进口畸变对效率的负面影响,改善出口压力场,...