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相继增压系统切换过程对增压器辅推轴承轴向力影响与轴承优化研究

李垂孝 张学艳 姜久奎 黄立 李先南 张伟 张博

内燃机工程2024,Vol.45Issue(2):85-92,101,9.
内燃机工程2024,Vol.45Issue(2):85-92,101,9.DOI:10.13949/j.cnki.nrjgc.2024.02.010

相继增压系统切换过程对增压器辅推轴承轴向力影响与轴承优化研究

Influences of Switching Process of Successive Turbocharging Systems on Axial Force of Booster Auxiliary Bearing and Research on Bearing Optimization

李垂孝 1张学艳 1姜久奎 1黄立 1李先南 1张伟 1张博2

作者信息

  • 1. 中国船舶集团有限公司第七一一研究所,上海 201108
  • 2. 中车大连机车研究所有限公司,大连 116021
  • 折叠

摘要

Abstract

The variation law of the axial force of the basic supercharger during system switching was studied by the numerical simulation method,and the improved design method of the auxiliary thrust bearing was put forward.The distribution of aerodynamic parameters of key typical sections of compressor/turbine when the rotor system of the basic supercharger switched was studied by numerical simulation,and the variation law of axial force and direction of the rotor of the basic supercharger during the switching of diesel engine supercharging mode was analyzed.Then the optimization scheme of increasing bearing surface and changing bearing surface material was put forward.The results show that the axial force of the auxiliary thrust bearing of the basic supercharger turns over within 5 s,and it bears about 2 273 N reverse axial force at most,which is the key reason for the wear of the auxiliary thrust bearing during the switching process.The maximum bearing capacity is 4.8 times of that before improvement,which significantly improves the bearing capacity of auxiliary thrust bearing.After the reliability verification of the supercharger platform,rubbing phenomenon did not appear for the improved supercharger auxiliary thrust bearing in the same time duration.

关键词

相继增压/压气机/涡轮/转子轴向力翻转/低速喘振

Key words

sequential turbo charging/compressor/turbine/inversion of rotor axial thrust/low speed surge

分类

能源科技

引用本文复制引用

李垂孝,张学艳,姜久奎,黄立,李先南,张伟,张博..相继增压系统切换过程对增压器辅推轴承轴向力影响与轴承优化研究[J].内燃机工程,2024,45(2):85-92,101,9.

基金项目

船舶动力基础科研计划项目 Marine Power Research&Development Project ()

内燃机工程

OA北大核心CSTPCD

1000-0925

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