考虑到叶片的相对位置,模拟轴流风机中的颗粒流和侵蚀作用

A. Ghenaiet
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引用次数: 0

摘要

轴流风扇是飞机通风系统中的重要配件,但它们可能会受到颗粒流的侵蚀,导致效率随时间下降。本研究考虑了叶片面对进气导叶的相对位置,研究了两种类型的沙粒在轴流风机中的运动轨迹和侵蚀情况。使用内部代码模拟了颗粒的运动,该代码采用拉格朗日方法和随机颗粒-涡流相互作用模型。流场单独求解,并将流动数据传输到粒子轨迹代码中。通过有限元方法,可以跟踪粒子穿过计算单元,并准确确定其撞击位置。半经验侵蚀相关性用于评估局部侵蚀率、质量去除和几何劣化。结果表明,转子的叶片前缘受到冲击的频率很高,侵蚀也很严重,一直延伸到压力侧的上角和叶片顶端,以及吸气侧的前端。在入口导叶中,侵蚀沿整个压力侧扩散,但侵蚀率低于转子叶片。为了更好地反映侵蚀模式,对不同节距位置上获得的侵蚀模式进行了累计。在最高浓度的 MIL-E5007E 砂(0-1000 美元/unicode{x03BC}$ m)中暴露 10 小时后,叶片的质量减少了 0.29%,叶尖弦减少了 0.45%,叶尖间隙增加了 0.23%。另一方面,AC 粗砂(0-200 μm)导致叶片质量减少 0.23%,叶尖弦减少 0.4%,叶尖间隙增加 0.16%。现有数据可用于监测类似设计的轴流风扇的寿命,并选择适当的涂层来防止侵蚀。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Simulation of particle-laden flows and erosion in an axial fan stage considering the relative position of the blades
Axial fans are vital accessories in aircraft ventilation systems, but, they may experience erosion from particulate flows, causing a decline in effectiveness over time. This study investigated the trajectories of two types of sand particles and erosion in an axial fan stage, considering the relative position of the blades facing the inlet guide vanes. The movement of particles was simulated using an in-house code that implements a Lagrangian approach along with a stochastic particle-eddy interaction model. The flow field was solved separately and the flow data was transferred to the particle trajectory code. The finite element method allowed for the tracking of particles through the computational cells and accurate determination of their impact positions. A semi-empirical erosion correlation was used to evaluate the local erosion rates, mass removal, and geometry deterioration. As a result, the rotor exhibits a high frequency of impacts and significant erosion on the leading edge of the blade, extending to the upper corner of the pressure side and blade tip, as well as the front of the suction side. In the inlet guide vane, the erosion is spread out along the entire pressure side but at lower erosion rates compared to the rotor blade. The erosion patterns obtained at different pitch-wise positions were cumulated to get better representation of erosion patterns. After being exposed to MIL-E5007E sand (0–1000 $\unicode{x03BC}$ m) at the highest concentration for 10 hours, the blade experienced a reduction of a 0.29% in mass, a 0.45% decrease in tip chord, and a 0.23% increase in tip clearance. On the other hand, AC-coarse sand (0–200 μm) resulted in a 0.23% decrease in blade mass, a 0.4% reduction in tip chord, and a 0.16% increase in tip clearance. The data that is available can be used to monitor the lifespan of axial fans of similar design and select appropriate coatings to protect against erosion.
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