内燃机学报2024,Vol.42Issue(4) :358-366.DOI:10.16236/j.cnki.nrjxb.202404042

颗粒冲蚀使径流涡轮机性能劣化的数值仿真

Numerical Simulation on Performance Deterioration of a Radial Flow Turbine due to Particle Erosion

马超 王宁宁 郭姗姗 王任信
内燃机学报2024,Vol.42Issue(4) :358-366.DOI:10.16236/j.cnki.nrjxb.202404042

颗粒冲蚀使径流涡轮机性能劣化的数值仿真

Numerical Simulation on Performance Deterioration of a Radial Flow Turbine due to Particle Erosion

马超 1王宁宁 2郭姗姗 3王任信4
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作者信息

  • 1. 潍坊学院 机械与自动化学院,山东 潍坊 261061;机械工业内燃机增压系统重点实验室,山东 寿光 262718
  • 2. 机械工业内燃机增压系统重点实验室,山东 寿光 262718;康跃科技(山东)有限公司,山东 寿光 262718
  • 3. 潍坊学院 机械与自动化学院,山东 潍坊 261061
  • 4. 玉柴机器股份有限公司研究院,广西 南宁 530000
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摘要

涡轮增压器径流涡轮机作为车用柴油机提升性能和控制排放的关键零部件,长期受到尾气颗粒的高速冲蚀,会造成流道壁面粗糙度增加以及性能劣化.以某 65K 径流涡轮机为研究对象,基于两相流数值仿真方法,研究了流道壁面冲蚀特性的形成机理,并且基于牵引商用车的实际路谱研究了冲蚀对其性能劣化的影响规律.结果表明:流道壁面的局部冲蚀强度与蜗壳几何结构的非对称性密切相关,并在蜗舌位置表现出最高的冲蚀率;在运行时长为 50000 h 内,涡轮机整机效率和相似流量相对变化率仿真预测值分别为-3.5%和 1.1%,其中前 10000 h内的劣化率分别占总劣化率的 56%和 70%;基于牵引车实际路谱的计算结果,发展了涡轮机性能劣化随时间增长的经验公式.

Abstract

As a key component for enhancing the performance and controlling emissions of diesel engines in vehi-cles,the turbine flow channel walls in a turbocharger are subjected to high-speed erosion from exhaust particles.It results in increasing roughness of the channel surfaces and reducing the turbine performance.Using a 65K radial flow turbine as a research object,the formation mechanism of erosion characteristics on flow channel walls and the impact on performance degradation based on two-phase flow numerical simulations were conducted.The results show that the local erosion rate of the flow channel wall is closely related to the asymmetry of the vortex shell ge-ometry,and the highest erosion rate occurs at the tongue of the volute.Within 50000 h of operation,the expected relative changes in the overall efficiency and mass flow parameter of the turbine were-3.5%and 1.1%,respectively,with the deterioration rates for the first 10000 h accounting for 56%and 70%of the total degradation rate,respectively.Based on actual road conditions of a tractor,empirical formulas for the deterioration of turbine performance over time was developed.

关键词

涡轮增压器/径流涡轮机/颗粒冲蚀/两相流

Key words

turbocharger/radial flow turbine/particle erosion/two-phase flow

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基金项目

国家自然科学基金资助项目(5210070756)

潍坊市科技发展计划资助项目(2021GX011)

出版年

2024
内燃机学报
中国内燃机学会

内燃机学报

CSTPCD北大核心
影响因子:0.76
ISSN:1000-0909
参考文献量6
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