Donghai Hu , Jonathan Emmanuel Mangeleka , Yan Sun , Jing Wang , Wenxuan Wei , Xiaoyan Zhang , Jianwei Li
{"title":"基于多方法融合的燃料电池汽车超高速电动空压机降噪优化","authors":"Donghai Hu , Jonathan Emmanuel Mangeleka , Yan Sun , Jing Wang , Wenxuan Wei , Xiaoyan Zhang , Jianwei Li","doi":"10.1016/j.flowmeasinst.2025.103001","DOIUrl":null,"url":null,"abstract":"<div><div>Operation of super-high-speed electric air compressors (SHSEAC) induces intense turbulent airflow and noise, significantly degrading user comfort. Existing noise studies, primarily focused on low-speed compressors, fail to address SHSEAC's distinct structural, flow, and acoustic characteristics. In this paper, aerodynam-ic noise generated by the SHSEAC is improved based on internal flow performance using a coupled computational fluid dynamics-computational aeroacoustic (CFD-CAA) simulation method. Firstly, a numerical model of SHSEAC was established, and the accuracy of the model was verified through experiments under idle, rated, and peak operating conditions (corresponding to 34000 rpm, 86500 rpm, and 95000 rpm, respectively). Secondly, propose a multi-objective optimization approach (MOOA)-Pareto-based to structure optimization is performed to improve both internal flow and acoustic field. The coupled simulation results indicate that the optimized structure improves the airflow and reduces turbulence between the two stages. The mean noise level (SPL) of the SHSEAC at 1m away from the boundary is minimized by 7.85 %,4.45 %, and 5.15 % at 34000 rpm, 86500 rpm, and 95000 rpm, respectively.</div></div>","PeriodicalId":50440,"journal":{"name":"Flow Measurement and Instrumentation","volume":"106 ","pages":"Article 103001"},"PeriodicalIF":2.7000,"publicationDate":"2025-07-18","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"Optimization of noise reduction for ultra high speed electric air compressor in fuel cell vehicles based on multi method fusion\",\"authors\":\"Donghai Hu , Jonathan Emmanuel Mangeleka , Yan Sun , Jing Wang , Wenxuan Wei , Xiaoyan Zhang , Jianwei Li\",\"doi\":\"10.1016/j.flowmeasinst.2025.103001\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>Operation of super-high-speed electric air compressors (SHSEAC) induces intense turbulent airflow and noise, significantly degrading user comfort. Existing noise studies, primarily focused on low-speed compressors, fail to address SHSEAC's distinct structural, flow, and acoustic characteristics. In this paper, aerodynam-ic noise generated by the SHSEAC is improved based on internal flow performance using a coupled computational fluid dynamics-computational aeroacoustic (CFD-CAA) simulation method. Firstly, a numerical model of SHSEAC was established, and the accuracy of the model was verified through experiments under idle, rated, and peak operating conditions (corresponding to 34000 rpm, 86500 rpm, and 95000 rpm, respectively). Secondly, propose a multi-objective optimization approach (MOOA)-Pareto-based to structure optimization is performed to improve both internal flow and acoustic field. The coupled simulation results indicate that the optimized structure improves the airflow and reduces turbulence between the two stages. The mean noise level (SPL) of the SHSEAC at 1m away from the boundary is minimized by 7.85 %,4.45 %, and 5.15 % at 34000 rpm, 86500 rpm, and 95000 rpm, respectively.</div></div>\",\"PeriodicalId\":50440,\"journal\":{\"name\":\"Flow Measurement and Instrumentation\",\"volume\":\"106 \",\"pages\":\"Article 103001\"},\"PeriodicalIF\":2.7000,\"publicationDate\":\"2025-07-18\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Flow Measurement and Instrumentation\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0955598625001931\",\"RegionNum\":3,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q2\",\"JCRName\":\"ENGINEERING, MECHANICAL\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Flow Measurement and Instrumentation","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0955598625001931","RegionNum":3,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q2","JCRName":"ENGINEERING, MECHANICAL","Score":null,"Total":0}
Optimization of noise reduction for ultra high speed electric air compressor in fuel cell vehicles based on multi method fusion
Operation of super-high-speed electric air compressors (SHSEAC) induces intense turbulent airflow and noise, significantly degrading user comfort. Existing noise studies, primarily focused on low-speed compressors, fail to address SHSEAC's distinct structural, flow, and acoustic characteristics. In this paper, aerodynam-ic noise generated by the SHSEAC is improved based on internal flow performance using a coupled computational fluid dynamics-computational aeroacoustic (CFD-CAA) simulation method. Firstly, a numerical model of SHSEAC was established, and the accuracy of the model was verified through experiments under idle, rated, and peak operating conditions (corresponding to 34000 rpm, 86500 rpm, and 95000 rpm, respectively). Secondly, propose a multi-objective optimization approach (MOOA)-Pareto-based to structure optimization is performed to improve both internal flow and acoustic field. The coupled simulation results indicate that the optimized structure improves the airflow and reduces turbulence between the two stages. The mean noise level (SPL) of the SHSEAC at 1m away from the boundary is minimized by 7.85 %,4.45 %, and 5.15 % at 34000 rpm, 86500 rpm, and 95000 rpm, respectively.
期刊介绍:
Flow Measurement and Instrumentation is dedicated to disseminating the latest research results on all aspects of flow measurement, in both closed conduits and open channels. The design of flow measurement systems involves a wide variety of multidisciplinary activities including modelling the flow sensor, the fluid flow and the sensor/fluid interactions through the use of computation techniques; the development of advanced transducer systems and their associated signal processing and the laboratory and field assessment of the overall system under ideal and disturbed conditions.
FMI is the essential forum for critical information exchange, and contributions are particularly encouraged in the following areas of interest:
Modelling: the application of mathematical and computational modelling to the interaction of fluid dynamics with flowmeters, including flowmeter behaviour, improved flowmeter design and installation problems. Application of CAD/CAE techniques to flowmeter modelling are eligible.
Design and development: the detailed design of the flowmeter head and/or signal processing aspects of novel flowmeters. Emphasis is given to papers identifying new sensor configurations, multisensor flow measurement systems, non-intrusive flow metering techniques and the application of microelectronic techniques in smart or intelligent systems.
Calibration techniques: including descriptions of new or existing calibration facilities and techniques, calibration data from different flowmeter types, and calibration intercomparison data from different laboratories.
Installation effect data: dealing with the effects of non-ideal flow conditions on flowmeters. Papers combining a theoretical understanding of flowmeter behaviour with experimental work are particularly welcome.