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粒子分离器结构优化对吞雨性能改进研究

杨群杰 林阿强 王家友 马佳乐 刘高文

哈尔滨工程大学学报2024,Vol.45Issue(7):1305-1313,9.
哈尔滨工程大学学报2024,Vol.45Issue(7):1305-1313,9.DOI:10.11990/jheu.202207058

粒子分离器结构优化对吞雨性能改进研究

Investigation on rain-swallowing performance improvement by structure optimization of a particle separator

杨群杰 1林阿强 2王家友 3马佳乐 1刘高文1

作者信息

  • 1. 西北工业大学 动力与能源学院,陕西西安 710129
  • 2. 西北工业大学 动力与能源学院,陕西西安 710129||西北工业大学深圳研究院,广东深圳 518057
  • 3. 中国航空发动机集团有限公司 沈阳发动机研究所,辽宁 沈阳 110015
  • 折叠

摘要

Abstract

The Eulerian-Lagrangian multiphase flow particle tracking model was used to numerically simulate the particle separator in a turboshaft engine,and the theory of orthogonal experimental design was employed to conduct the experiment and optimize the structure of the particle separator.The effects of the structure parameter of the par-ticle separator on the separation effect and rain-swallowing performance were examined.The results disclosed that,compared with the original model,in dry conditions,the scavenging ratio of the optimized model decreased by 4.3%,and the total pressure loss coefficient decreased by 0.03%;in rain-swallowing conditions,the former de-creased by 0.97%,the latter decreased by 0.039%,and the separation efficiency increased by 5.5%.Therefore,this optimization design basically satisfies the requirements of low total pressure loss and high separation efficiency.In addition,the rain-swallowing performance of the particle separator is improved to a great degree.

关键词

涡轴发动机/粒子分离器/正交试验设计/优化设计/吞雨/扫气比/总压损失系数/分离效率

Key words

turboshaft engine/particle separator/orthogonal experimental design/optimization design/rain swallo-wing/scavenging ratio/total pressure loss coefficient/separation efficiency

分类

航空航天

引用本文复制引用

杨群杰,林阿强,王家友,马佳乐,刘高文..粒子分离器结构优化对吞雨性能改进研究[J].哈尔滨工程大学学报,2024,45(7):1305-1313,9.

基金项目

陕西省自然科学基础研究计划(2023-JC-YB-305) (2023-JC-YB-305)

中国博士后科学基金项目(2023M742834) (2023M742834)

广东省基础与应用基础研究基金项目(2021A1515110063) (2021A1515110063)

航空发动机及燃气轮机基础科学中心项目(P2022-A-II-007-001). (P2022-A-II-007-001)

哈尔滨工程大学学报

OA北大核心CSTPCD

1006-7043

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