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Design and Optimization of Brush Seal in Gas Turbine Bearing Cavity |
DOI:10.13949/j.cnki.nrjgc.2025.02.014 |
Key Words:brush seal orthogonal experiment porous media flow field analysis |
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Abstract:Aiming at the sealing problem of the gas turbine bearing cavity, a two-stage staggered brush seal structure was designed. A porous media model was used to analyze the pressure and velocity distribution of the seal under specific working conditions. The effects of structural parameters on the sealing performance of the brush seal, such as the fiber diameter, the thickness of the bristle and the inclination angle of the brush, were investigated by using the finite element analysis method. Orthogonal test method was used to analyze the leakage of different combinations of structural parameters. The structural parameters that have effects on the sealing performance from the strongest effects to the least effects are fiber diameter, back baffle gap, bristle thickness, cant angle of brush and front baffle gap. Combined with the actual processing capability, the structural parameters were optimized. The preferred structural parameters include fiber diameter 0.005 mm, bristle thickness 3 mm, cant angle of brush 20°, front baffle gap 1.6 mm and back baffle gap 0.6 mm. The mass flow rate of the optimized structure is 11.24 g/s, and the sealing performance of the optimized structure is improved by 62.51% compared with that before optimization. |
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