轴流压气机一维特性计算方法简介及展望

王进; 周玲; 季路成

doi:10.11729/syltlx20200088

轴流压气机一维特性计算方法简介及展望

- 1.
  北京理工大学宇航学院, 北京 100081
- 2.
  清华大学航空发动机研究院, 北京 100083
基金项目:
国家科技重大专项（2017-II-0006-0020，2017-II-0001-0013）

详细信息

作者简介:
王进(1995-), 男, 湖北十堰人, 硕士研究生。研究方向: 压气机一维设计分析。通信地址: 北京市海淀区北京理工大学宇航学院(100081)。E-mail: 2504571042@qq.com

通讯作者: 周玲, E-mail: lingzhou@bit.edu.cn

中图分类号: V231.1
收稿日期: 2020-07-18

修回日期: 2020-10-12

刊出日期: 2021-04-01

Brief introduction and prospect of calculation methods for one-dimensional characteristics of axial flow compressor

- 1.
  School of Aerospace and Engineering, Beijing Institute of Technology, Beijing 100081, China
- 2.
  Institute for Aero Engine, Tsinghua university, Beijing 100083, China

More Information

Corresponding author: Ling ZHOU, E-mail: lingzhou@bit.edu.cn

Received Date: 18 July 2020

Revised Date: 12 October 2020

Publish Date: 01 April 2021

摘要

摘要:
一维特性计算作为压气机设计体系的关键环节，在压气机的初始设计阶段发挥了重要作用。作为一种高度经验化的工程近似计算方法，一维性能计算需要大量实验数据的支撑。从实验数据中总结得到的经验关联式的质量，是决定一维计算成功与否的关键。在充分调研欧美以级叠加方法和平均线方法为主的一维性能分析方法的基础上，回顾了轴流压气机一维特性计算方法的起源，讨论了其发展趋势与研究现状。对一维特性计算方法的基本原理及其所使用的经典经验关联式进行了整理总结，指明了压气机一维性能分析未来进一步发展的方向。
- 轴流压气机 /
- 特性计算 /
- 级叠加法 /
- 平均线法 /
- 一维
Abstract:
One-dimensional (1-D) characteristic calculation, as a key link of the compressor design system, plays an important role in the initial design stage of the compressor. As a highly empirical engineering approximate calculation method, one-dimensional performance calculation requires the support of a large amount of experimental data. The quality of the empirical correlation obtained from the experimental data is the key to the success of the one-dimensional calculation. By fully investigating the 1-D performance analysis methods in Europe and the United States, which are mainly based on the stage stacking method and the meanline method, this paper reviews the origin of the 1-D characteristic calculation methods of the axial compressor, and discusses its development trend and research status. In addition, the basic principles of the 1-D characteristic calculation methods and the classic empirical correlations used are summarized, and the direction of future development of 1-D performance analysis of the compressor is pointed out.
- axial flow compressor /
- performance calculation /
- stage stacking method /
- meanline method /
- one-dimensional

HTML全文

图 1 典型的级性能^[7]

Figure 1. Typical stage performance^[7]

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图 2 非设计转速下的级性能^[15]

Figure 2. Stage performance at off-design speed^[15]

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图 3 C135压气机首级的性能^[14]

Figure 3. First stage performance of C135 compressor^[14]

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图 4 C135压气机首级转子平均半径处的马赫数与最佳攻角、失速攻角以及堵塞攻角的关系^[14]

Figure 4. Maximum efficiency, stall and choke incidences and rotor inlet Mach numbers at mean radius for first stage of C135 compressor^[14]

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图 5 HARIKA程序计算框架

Figure 5. Calculation framework of HARIKA program

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图 6 某三级压气机特性^[33]

Figure 6. A 3-stage compressor characteristic^[33]

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图 7 平均线方法

Figure 7. Meanline method

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图 8 叶片表面附面层和尾迹的发展^[51]

Figure 8. Development of surface boundary layers and wake in flow about cascade blade sections^[51]

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图 9 激波结构示意图^[51]

Figure 9. Schematic representation of shock wave configuration^[51]

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图 10 上端壁处的叶尖泄露涡和通道涡

Figure 10. Tip leakage vortex and passage vortex at tip endwall

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图 11 C135两级跨音压气机特性

Figure 11. C135 two-stage transonic compressor prediction

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轴流压气机一维特性计算方法简介及展望

作者简介: 王进(1995-), 男, 湖北十堰人, 硕士研究生。研究方向: 压气机一维设计分析。通信地址: 北京市海淀区北京理工大学宇航学院(100081)。E-mail: 2504571042@qq.com

通讯作者: 周玲, E-mail: lingzhou@bit.edu.cn

Brief introduction and prospect of calculation methods for one-dimensional characteristics of axial flow compressor

Corresponding author: Ling ZHOU, E-mail: lingzhou@bit.edu.cn

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作者简介:
王进(1995-), 男, 湖北十堰人, 硕士研究生。研究方向: 压气机一维设计分析。通信地址: 北京市海淀区北京理工大学宇航学院(100081)。E-mail: 2504571042@qq.com