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首页> 外文期刊>Atomization and Sprays: Journal of the International Institutes for Liquid Atomization and Spray Systems >EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE INFLUENCE OF PARTIAL NEEDLE LIFT ON NOZZLE FLOW IN DIESEL FUEL INJECTORS
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EXPERIMENTAL AND COMPUTATIONAL STUDY OF THE INFLUENCE OF PARTIAL NEEDLE LIFT ON NOZZLE FLOW IN DIESEL FUEL INJECTORS

机译:针头部分升幅对柴油机喷油嘴喷流影响的实验与计算研究

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摘要

This paper presents an experimental and computational study with the aim of developing a fundamental understanding of the nozzle internal flow behavior in a prototype piezo-stack injector with a multi-orifice nozzle, which allows controlling the needle position at different percentages of its maximum lift. In order to characterize the flow behavior, several measurements of mass flow rate and spray momentum flux have been carried out at different rail pressures (up to 200 MPa). Furthermore, to develop a deep understanding of the internal flow behavior, computational fluid dynamic simulations have been carried out using the software OpenFOAM in order to determine the pressure drop through the nozzle seat and estimate the real needle lift at different conditions. The experimental results demonstrate the nozzle flow behavior and the commonly used nondimensional coefficients; an interesting reduction in the nozzle discharge coefficient at partial lifts (needle positions smaller than the maximum lift) is shown. The computational results allow the estimation of the pressure and velocity profiles in the needle seat at different needle positions. Afterwards, the pressure drop through the needle seat and the real needle lift is determined for each test condition. Thus, with the velocity profiles obtained, the variation in both the dynamic pressure and flow directionality at the orifice inlet could be determined. Thus the decrease of effective area and its dependency on the lift were justified since the calculation of these nondimensional coefficients assumes only static pressure upstream the hole conditions.
机译:本文提出了一项实验和计算研究,目的是对带有多孔喷嘴的原型压电堆喷射器中的喷嘴内部流动行为有一个基本的了解,从而可以在最大升程的不同百分比下控制针的位置。为了表征流动特性,已经在不同的轨道压力(最高200 MPa)下对质量流量和喷雾动量通量进行了多次测量。此外,为了深入了解内部流动行为,已使用OpenFOAM软件进行了计算流体动力学模拟,以确定通过喷嘴座的压降并估计不同条件下的实际针升程。实验结果证明了喷嘴的流动特性和常用的无量纲系数。显示了在部分升程(针位置小于最大升程)时喷嘴排放系数的有趣降低。计算结果允许估计不同针位置处针座中的压力和速度曲线。然后,针对每种测试条件确定通过针座的压力降和实际针升程。因此,利用获得的速度曲线,可以确定孔口入口处的动态压力和流动方向性的变化。因此,有效面积的减小及其对升程的依赖性是合理的,因为这些无量纲系数的计算仅假设孔条件上游的静压力。

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