Deposition Characteristics of Particles with Different Diameters in an Impingement-Effusion Structure with a Double-Wall Blade

被引:0
|
作者
Zhang, W. [1 ]
Zhang, P. [1 ]
Wang, Y. D. [1 ]
机构
[1] Shenyang Aerosp Univ, Dept Aeroengine, Shenyang 110000, Peoples R China
基金
中国国家自然科学基金;
关键词
Impingement-effusion structure; Deposition model; Particle size; Deposition distribution; Degradation of cooling performance; ADHESION; REMOVAL;
D O I
10.47176/jafm.16.09.1681
中图分类号
O414.1 [热力学];
学科分类号
摘要
Ingestion and deposition of fine particles on the surface of the coolant passage degrade the blade's cooling performance. This paper proposes a deposition model to investigate the complex deposition characteristics of fine particles during repeated collision, adhesion, rebound, and removal events in the small space inside a typical impingement-effusion structure with a double-wall blade. The results show that the particles rarely collide with the wall and escape directly from the film hole outlet when the particle diameters are smaller than 0.5 & mu;m. Most particles with diameters of 0.5 to 1.0 & mu;m are deposited after the first collision around the stagnation point in an area 0.35 times the pin-fin diameter. Some particles with diameters of 1.0 to 3.0 & mu;m are deposited in the stagnation region, but most are deposited between the two pin fins and near the film hole after the second collision. Particles with diameters larger than 3.0 & mu;m are mainly deposited on the region enclosed by the adjacent pin fins and film holes after multiple collisions, and the escape rate of particles is higher than 30%. The escape rates of particles with diameters of 0.5 to 1.0 & mu;m and 1.0 to 3.0 & mu;m have the same trends, exhibiting a decrease followed by an increase with the increasing particle diameter. The particles entering the impingement-effusion structure, especially those with diameters of 0.7 -0.8 & mu;m and 1.4 -2.4 & mu;m, are primarily deposited on the target surface, resulting in the cooling performance degradation of double-walled blade.
引用
收藏
页码:1818 / 1827
页数:10
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