最小喉道面积比对多级轴流压气机性能影响

推进技术 ›› 2015, Vol. 36 ›› Issue (1): 47-53.

最小喉道面积比对多级轴流压气机性能影响

邓熙 ,刘波,李俊

西北工业大学动力与能源学院/翼型叶栅国防科技重点实验室，陕西西安 710072,西北工业大学动力与能源学院/翼型叶栅国防科技重点实验室，陕西西安 710072,西北工业大学动力与能源学院/翼型叶栅国防科技重点实验室，陕西西安 710072

发布日期:2021-08-15
作者简介:邓熙(1989—)，男，硕士生，研究领域为叶轮机械气动热力学。
基金资助:
国家自然科学基金重点项目(51236006)。

Effects of Minimum Throat Area Ratio on Multistage Axial-Flow Compressor Performance

School of Power and Energy/National Key Laboratory of Aerodynamic Design and Reseach， Northwestern Polytechnical University， Xi’an 710072， China,School of Power and Energy/National Key Laboratory of Aerodynamic Design and Reseach， Northwestern Polytechnical University， Xi’an 710072， China and School of Power and Energy/National Key Laboratory of Aerodynamic Design and Reseach， Northwestern Polytechnical University， Xi’an 710072， China

Published:2021-08-15

摘要/Abstract

摘要： 为了研究最小喉道面积比对多级轴流压气机性能的影响，开发了一套基元叶栅最小喉道面积比的计算程序。通过对基元叶栅进行最小喉道面积比计算，得到压气机叶片沿展向的最小喉道面积比分布，同时分析了转子和静子的最小喉道面积比分布规律。最后采用修改基元叶型的前段弯度比与最大厚度来改变基元叶栅的最小喉道面积比分布，分析了不同最小喉道面积比分布对多级轴流压气机性能的影响。结果表明，压气机的阻塞流量与最小喉道面积比成正相关，并且存在最佳前段弯度比使压气机设计点效率与压比达到最大，最大厚度变小能改善压气机整体性能。

关键词: 喉道面积比；多级压气机；阻塞流量；基元叶型；弯度比；最大厚度

Abstract: A set of process for calculating primitive cascades minimum throat area ratio was built，in order to study the effects of minimum throat area ratio on multistage axial-flow compressor performance. The span-wise distribution of minimum throat area ratio was obtained through calculating primitive cascade，and the minimum throat ratio distribution rule of rotor and stator are analyzed. Then the front camber ratio and maximum thickness of primitive blade was modified to study the different distribution of minimum throat area ratio impacting on multistage axial-flow compressor performance. The result shows that block mass-flow and minimum throat area ratio have a linear relationship. Having a best front camber ratio makes the compressor total pressure ratio and efficiency to achieve the maximum at design point. And reducing thickness is able to improve compressor performance.

Key words: Throat area ratio；Multistage compressor；Block mass-flow；Primitive blade；Camber ratio；Maximum thickness

邓熙,刘波,李俊. 最小喉道面积比对多级轴流压气机性能影响[J]. 推进技术, 2015, 36(1): 47-53.

DENG Xi , LIU Bo,LI Jun. Effects of Minimum Throat Area Ratio on Multistage Axial-Flow Compressor Performance[J]. Journal of Propulsion Technology, 2015, 36(1): 47-53.

参考文献

[1] 苏三买, 张蕾, 蔡元虎, 等. 弹用喷气发动机发展及关键技术分析[J]. 航空动力学报, 2009, 11: 002.
[2] 解亚东, 单鹏. 小流量多级高负荷轴流压气机设计[J]. 航空动力学报, 2012, 27(9): 2113-2121.
[3] 沈伟, 辛彦秋, 颜青钦. 小型涡喷发动机整机流场数值模拟技术研究[J]. 航空计算技术, 2011, 41(6): 73-75.
[4] 郑涛, 赵克云, 吴仁辉. 水流法测量涡轮导向器喉道面积[J]. 推进技术, 1997, 18(4).(ZHENG Tao, ZHAO Ke-yun, WU Ren-hui.Measurement of Turborotor Throat Area by Water Flow[J]. Journal of Propulsion Technology, 1997, 18(4).)
[5] Wadia A R, Copenhaver W W. An Investigation of the Effect of Cascade Area Ratios on Transonic Compressor Performance[J]. Journal of Turbomachinery, 1996, 118(4): 760-770.
[6] Yin J, Li P, Pees S. Optimization of Turbocharger Ported Shroud Compressor Stages[C]. Orlando: ASME Turbo Expo 2009: Power for Land, Sea, and Air, 2009.
[7] Messenger H E, Kennedy E E. Two-Stage Fan, I. Aerodynamic and Mechanical Design[R]. PWA-4148, 1972.
[8] Steinke R J. Design of 9.271-Pressure-Ratio Five-stage Core Compressor and Overall Performance for First Three Stages[R]. NASA-TP-2597, 1986.
[9] Reid L, Moore R D. Design and Overall Performance of Four Highly Loaded, High Speed Inlet Stages for an Advanced High-pressure-ratio Core compressor[R]. NASA, 1978, TP-1337.
[10] 李相君, 楚武利, 张皓光, 等. 高负荷跨音速轴流压气机的叶型优化设计[J]. 计算机仿真, 2012, 29(7): 75-79.
[11] 宋立明, 李军, 丰镇平, 等. 三维跨音速压气机叶栅多目标气动优化设计[J]. 工程热物理学报, 2007, 28(2): 223-225.
[12] 张宏武, 陈乃兴, 徐燕骥, 等. 跨音速单转子压气机气动设计的优化[J]. 工程热物理学报, 2005, 26(4): 581-583.
[13] 朱国东, 李培军, 单鹏. 超跨音速轴流风扇, 压气机级最大负荷能力研究[J]. 航空动力学报, 2002, 17(5): 538-541.
[14] 王掩刚, 刘波, 管继伟, 等. 多级压气机非定常流场数值分析[J]. 工程热物理学报, 2008 (z1): 125-128.
[15] 项效镕, 刘波, 王庆伟, 等. 小型轴流压气机静叶排出口尾迹流动特性[J]. 航空学报, 2009, 30(11): 2045-2051.(编辑:朱立影)　　　　　　　　　　　　　*　收稿日期:2014-01-06；修订日期:2014-03-05。基金项目:国家自然科学基金重点项目(51236006)。作者简介:邓熙(1989—),男,硕士生,研究领域为叶轮机械气动热力学。E-mail:dengxi20001@163.com