Effects of Geometry of Plenum Chamber on Losses in the Bleed System of an Axial Compressor

Abstract

To study how the geometry of the plenum chamber in the bleed system of an axial compressor influences the losses therein and to establish a theoretical loss model for this system, a 1.5-stage axial compressor with a bleed system is studied numerically by means of computational fluid dynamics (CFD). The results show that losses in the bleed system occur mainly in the axisymmetric bleed slot and plenum chamber, accounting for ca. 85% of the total loss. For a bleed system with a vertical axisymmetric slot, the loss is more sensitive to the radial height than to the axial width of the plenum chamber. A loss model for each part of the bleed system is established via theoretical analysis, and then, a model of the overall bleed system is established by combining these submodels. The predictions of the theoretical loss model agree well with the CFD results: the maximum prediction error for the coefficient of the stagnation pressure loss in the bleed system is −1.38%, and the average prediction error is −0.8%. This loss model can be used when designing the geometry of a bleed system.

Non-uniform flow characteristics and rotating instability of a transonic high-pressure compressor rotor with cavity bleed

“…Currently, studies on the impact of bleed on the internal flow field of compressors can be classified into two main categories. The first category investigates key parameters such as bleed positions, 3,4 bleed rate, 5,6 bleed configuration, 7,8 and bleed structure, 9,10 aiming to improve the flow field performance and internal flow structure of the compressor through the rational arrangement of the bleed system. 11,12 The second category focuses on studying the effects of flow field distortion induced by bleed in the compressor, considering real-world typical bleed structures.…”