高负荷轴流压气机设计与试验验证

doi:10.7527/S1000-6893.2017.620990

航空发动机内流与传热技术发展专栏

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高负荷轴流压气机设计与试验验证

李清华^1,2, 安利平², 徐林², 米攀², 庞超²

1. 南京航空航天大学能源与动力学院, 南京 210016;
2. 中国航发四川燃气涡轮研究院, 成都 610500

收稿日期:2016-11-25 修回日期:2017-04-04 出版日期:2017-09-15 发布日期:2017-05-12
通讯作者: 李清华 E-mail:liqinghuapc@sina.com

Design and test verification of high load axial-flow compressor

LI Qinghua^1,2, AN Liping², XU Lin², MI Pan², PANG Chao²

1. College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China;
2. AECC Sichuan Gas Turbine Establishment, Chengdu 610500, China

Received:2016-11-25 Revised:2017-04-04 Online:2017-09-15 Published:2017-05-12

摘要/Abstract

摘要：

为了提高高负荷轴流压气机气动性能，探索高负荷压气机设计方法。首先，对高负荷压气机轴向载荷和参数分布进行研究与筛选优化；然后，利用二维正/反问题设计与分析方法优化压气机载荷展向分布；最后，利用三维流场分析方法进行精细分析，从而使高负荷压气机级间参数达到良好的匹配。将该方法应用于一台高负荷压气机设计中，并将试验值与计算结果进行了比较分析。结果显示：该技术有效地提高了压气机全工况的性能，使压气机各级工作在合理的参数下，相对于第4代发动机的压气机平均级压比提高了16%，效率提高了1%。

关键词: 高负荷, 轴流压气机, 级间匹配, 优化, 试验验证

Abstract:

In order to improve the aerodynamic performance of the high load axial-flow compressor and to explore the design method for the high load compressor. The axial load and parameter distribution of the high load compressor is studied and selectively optimized. The span load distribution of the compressor is then optimized using 2D direct and inverse solution design and analysis method. 3D flow filed analysis is applied to conduct refinement analysis. Stage parameters of the high load compressor are matched well. The method is used to design one high load compressor. Test results and calculation results are compared and studied. Results show that this technique can effectively improved compressor performance under all operation conditions and can allow the compressor to work with reasonable parameters at each stage. With this design technique, the average stage pressure ratio of the compressor can be increased by 16% and efficiency can be increased by 1% over the 4th generation aero-engine compressor.

Key words: high load, axial-flow compressor, stage matching, optimization, test verification

中图分类号:

V231.3

李清华, 安利平, 徐林, 米攀, 庞超. 高负荷轴流压气机设计与试验验证[J]. 航空学报, 2017, 38(9): 520990-520990.

LI Qinghua, AN Liping, XU Lin, MI Pan, PANG Chao. Design and test verification of high load axial-flow compressor[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2017, 38(9): 520990-520990.

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E-mail：hkxb@buaa.edu.cn

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主管单位：中国科学技术协会主办单位：中国航空学会北京航空航天大学

高负荷轴流压气机设计与试验验证

Design and test verification of high load axial-flow compressor

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