高负荷离心压气机扩压器叶片前缘开槽参数化研究

张英杰 1; 韩戈 1; 董旭 1; 赵胜丰 1; 张燕峰 1; 2; 卢新根 1; 2

doi:10.7652/xjtuxb201909005

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高负荷离心压气机扩压器叶片前缘开槽参数化研究

更新时间：2025-07-09

- 高负荷离心压气机扩压器叶片前缘开槽参数化研究
- Parametric Investigation on the Effects of Slotted Diffuser on a Highly Loaded Centrifugal Compressor
- 西安交通大学学报 2019年53卷第9期页码：34-41
- 作者机构：
  
  1. 中国科学院工程热物理研究所,北京,100190
  2. 中国科学院大学,北京,100049
- 作者简介：
- 基金信息：
  
  : 2019-02-14。作者简介: 张英杰(1994—),女,博士生;卢新根(通信作者),男,研究员。基金项目: 国家自然科学基金资助项目(51606187)
- DOI：10.7652/xjtuxb201909005
  中图分类号： V231.3
- 网络首发：2019-09-10，
  
  纸质出版：2019
- 稿件说明：
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张英杰 1, 韩戈 1, 董旭 1, 等. 高负荷离心压气机扩压器叶片前缘开槽参数化研究[J]. 西安交通大学学报, 2019,53(9):34-41.

Parametric Investigation on the Effects of Slotted Diffuser on a Highly Loaded Centrifugal Compressor[J]. 2019, 53(9): 34-41.
张英杰 1, 韩戈 1, 董旭 1, 等. 高负荷离心压气机扩压器叶片前缘开槽参数化研究[J]. 西安交通大学学报, 2019,53(9):34-41. DOI： 10.7652/xjtuxb201909005.

Parametric Investigation on the Effects of Slotted Diffuser on a Highly Loaded Centrifugal Compressor[J]. 2019, 53(9): 34-41. DOI： 10.7652/xjtuxb201909005.

摘要

针对离心压气机在近失速工况点运行时

扩压器进口气流角为正攻角

造成其吸力面发生流动分离

从而导致压气机发生失速甚至喘振等问题

为进一步扩大离心压气机的稳定工作范围

需对扩压器近失速工况点的流动分离进行抑制。以某高负荷离心压气机为研究对象

利用经过校核的数值模拟方法开展了扩压器叶片前缘开槽的参数化研究

详细探讨了开槽长度、深度对离心压气机性能、稳定裕度的影响规律

归纳总结了离心压气机扩压器的最佳开槽参数。研究结果表明:随着开槽深度、长度的增加

失速裕度有所提高但压气机性能有所下降; 实际设计中开槽深度不应超过叶片高度的9%

最佳开槽长度不应超过叶片弦长的6%～12%; 当扩压器开槽深度为叶片高度的3%、开槽长度为叶片弦长的6%～12%时

压气机性能最佳。扩压器开槽可有效抑制其通道内的流动分离

并提高压气机的失速裕度。

Abstract

When a centrifugal compressor operates near the stall point

the positive incidence angle at the diffuser inlet makes flow separation appear near the diffuser suction side

leading to compressor stall and surge.The leading edge structure of diffuser has an important effect on the compressor's performance and flow field.To extend stable operating range of centrifugal compressors

the flow separations within the diffuser passage near stall point need to be suppressed.In this research

numerical simulations were performed for a highly loaded centrifugal compressor to investigate the design method of slotted diffuser and discuss the influences of slot length and depth on the stage performance and stall margin.The results indicate that the compressor performance is deteriorated with the increase of slot length and depth

although the stall margin is expanded.In conclusion

the slot depth should not exceed 9% of the diffuser vane height

and the optimal slot length should not be more than 6%

关键词

Keywords

references

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