Inicio  /  Aerospace  /  Vol: 8 Par: 1 (2021)  /  Artículo
ARTÍCULO
TITULO

Numerical Analysis of Flow across Brush Elements Based on a 2-D Staggered Tube Banks Model

Xiaolei Song    
Meihong Liu    
Xiangping Hu    
Xueliang Wang    
Taohong Liao and Junfeng Sun    

Resumen

In order to improve efficiency in turbomachinery, brush seal replaces labyrinth seals widely in the secondary air system. A 2-d staggered tube bank model is adopted to simulate the gas states and the pressure character in brush seal, and computational fluid dynamics (CFD) is used to solve the model in this paper. According to the simulation results, the corrected formula of the Euler number and dimensionless pressure are given. The results show that gas expands when flow through the bristle pack, and the gas expansion closes to an isotherm process. The dynamic pressure increases with decreasing static pressure. The Euler number can reflect the seal performance of brush seals in leakage characteristics. Compared with increasing the number of rows, the reduction of the gap is a higher-efficiency method to increase the Euler number. The Euler number continually increases as the gap decreases. However, with the differential pressure increasing, Euler number first increases and then decreases as the number of rows increases. Finally, the pressure distribution on the surface of end rows is asymmetric, and it may increase the friction between the bristles and the back plate.

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