级间进出口几何角度对压气机气动性能和封严效果的影响

doi:10.13675/j.cnki.tjjs.190254

推进技术 ›› 2020, Vol. 41 ›› Issue (5): 1063-1071.DOI: 10.13675/j.cnki.tjjs.190254

级间进出口几何角度对压气机气动性能和封严效果的影响

王广¹，楚武利^1,2

1.西北工业大学动力与能源学院，陕西西安 710129;2.先进航空发动机协同创新中心，北京 100191

发布日期:2021-08-15
作者简介:王广，博士生，研究领域为叶轮机械气动热力学。E-mail：wangguang@mail.nwpu.edu.cn
基金资助:
国家自然科学基金（51576162）；国家自然科学基金重点项目（51536006）。

Influence of Geometric Angle of Inter-Stage Inlet and Outlet on Aerodynamic Performance and Sealing of Compressor

1.School of Power and Energy,Northwestern Polytechnical University,Xi’an 710072,China;2.Collaborative Innovation Center of Advanced Aero-Engine,Beijing 100191,China

Published:2021-08-15

摘要/Abstract

摘要： 为了削弱级间泄漏流对压气机性能的不利影响，提出了一种基于Coanda型几何进出口的级间结构，并以一个亚声速单级轴流压气机为研究对象，数值模拟了5°，10°，20°三种不同级间进出口几何角度对压气机性能的影响。结果表明：改进后的级间进出口几何结构使得压气机流量和效率均略有提升。分析原因是级间出口泄漏流以较小角度与主流汇合，增大了静叶进口气流的轴向速度、径向速度，使得静子通道流动堵塞程度减轻，总压损失减小，扩压能力增强。同时，新结构还减小了级间泄漏流的流量系数，改善了级间封严效果。5°，10°，20°角度下的压气机效率最大分别提升了0.68%，0.63%，0.62%。

关键词: 压气机;级间封严;气动性能;流量系数;数值模拟

Abstract: In order to weaken the adverse effect of the inter-stage leakage flow on the performance of the compressor, an inter-stage structure based on Coanda type geometry inlet and outlet is proposed. Then, taking a subsonic single-stage axial flow compressor as the research object, the effects of three different geometric angle of 5°, 10° and 20° of inter-stage inlet and outlet on the performance of the compressor were numerically simulated. The results show that the improved inter-stage inlet and outlet geometry makes the compressor flow and efficiency slightly improved. The reason for the analysis is that the leakage flow of the inter-stage outlet merges with the main flow of the compressor at a smaller angle, which increases the axial and radial velocity of the stator passage, so that the flow blockage of the stator passage is weakened, the total pressure loss is also reduced, and the diffuser capability of stator passage is enhanced. At the same time, the new structure also reduces the discharge coefficient of inter-stage leakage flow and improves the sealing effect. The isentropic adiabatic efficiency of the single stage compressor at three angles（5°， 10°， 20°） rise by 0.68%, 0.63% and 0.62%, respectively at the maximum.

Key words: Compressor;Inter-stage seal;Aerodynamic performance;Discharge coefficient;Numerical simulation

王广，楚武利. 级间进出口几何角度对压气机气动性能和封严效果的影响[J]. 推进技术, 2020, 41(5): 1063-1071.

WANG Guang¹, CHU Wu-li^1,2. Influence of Geometric Angle of Inter-Stage Inlet and Outlet on Aerodynamic Performance and Sealing of Compressor[J]. Journal of Propulsion Technology, 2020, 41(5): 1063-1071.

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级间进出口几何角度对压气机气动性能和封严效果的影响

Influence of Geometric Angle of Inter-Stage Inlet and Outlet on Aerodynamic Performance and Sealing of Compressor

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