首页> 外文会议>ASME turbo expo: turbomachinery technical conference and exposition >ROBUST FILM COOLING HOLE SHAPE OPTIMIZATION CONSIDERING SURFACE ROUGHNESS AND PARTIAL HOLE BLOCKAGE
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ROBUST FILM COOLING HOLE SHAPE OPTIMIZATION CONSIDERING SURFACE ROUGHNESS AND PARTIAL HOLE BLOCKAGE

机译:考虑表面粗糙度和部分孔堵塞的鲁棒膜冷却孔形状优化

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High performance film cooling holes with complicated geometries have been regarded as impractical up to now because of manufacturability issues. However, recent advances in additive manufacturing (AM) technology have opened up new doors. Investigating characteristics of film holes built with AM, and finding the optimum shape considering these characteristics are now required to confirm their practical utility. In this paper, the performance of a high-efficiency film hole is numerically investigated. In-hole roughness and blade surface roughness are examined assuming an AM process, and contorted hole shape caused by partial blockage is also considered. A robust hole shape is obtained considering these uncertainties, utilizing a reference hole shape made by combining three cylindrical holes. Hole diameter, injection angle, and two angles for defining the two auxiliary holes are used as design variables to be optimized. For flow field and thermal analysis with roughness, compressible steady Reynolds averaged Navier-Stokes equations with a sand-grain roughness model are used. For the probabilistic assessment of each hole shape, Monte Carlo Simulations with the Kriging surrogate model is used, along with efficient global optimization (EGO) and a genetic algorithm. As a result, a high performance yet robust film cooling hole shape is obtained.
机译:由于可制造性问题,具有复杂几何形状的高性能薄膜冷却孔被认为是现在的不切实际。然而,最近的添加剂制造业(AM)技术的进展已经开辟了新的门。研究随着AM建造的薄膜孔的特性,并考虑了考虑这些特性的最佳形状来证实它们的实用性。在本文中,数值研究了高效膜孔的性能。假设AM工艺检查内孔粗糙度和叶片表面粗糙度,并且还考虑由部分堵塞引起的轮廓孔形状。考虑到这些不确定性,获得鲁棒孔形状,利用通过组合三个圆柱形孔制成的参考孔形状。用于定义两个辅助孔的孔径,注射角度和两个角度用作优化的设计变量。对于具有粗糙度的流场和热分析,使用压缩稳态雷诺平均具有砂粒粗糙度模型的Navier-Stokes方程。对于每个孔形状的概率评估,使用具有Kriging代理模型的蒙特卡罗模拟,以及有效的全局优化(EGO)和遗传算法。结果,获得了高性能且坚固的薄膜冷却孔形状。

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