{"title":"边界层摄取(BLI)风扇的系统综述:现状与未来展望","authors":"Tao Ma , Hanan Lu , Qiushi Li","doi":"10.1016/j.paerosci.2025.101082","DOIUrl":null,"url":null,"abstract":"<div><div>The distributed propulsion system has a significant potential for reducing the fuel consumption, noise and pollution emissions for the next-generation aircraft and become a current hot research topic. As the core component of the distributed propulsion system, the boundary layer ingestion fan has been continuously operating under the distorted inflow conditions, which largely degrades the aerodynamic performance of the fan itself. In turn, the degradation of the BLI fan performance will have a severe impact on the overall aerodynamic benefits achievement of the aircraft. This paper has conducted a systematic review of the boundary layer ingestion fan. Firstly, the aerodynamic benefits of BLI propulsion system has been overviewed. Then, different types of BLI fan based propulsion configurations have been introduced and the distinguished features of the distorted inflows for each configuration are analyzed in detail. Thirdly, the fan aerodynamic responses to the BLI distorted inflow are given and the influences of the BLI inflow distortion on the fan aerodynamic performances and internal flow fields are fully investigated. Subsequently, the potential performance evaluation methods, mainly the low-order computational approaches, used in the preliminary design stage of the fan have been comprehensively overviewed. Finally, the research works concerning the attempts for the fan/compressor design under non-uniform inflow condition are reviewed and some perspectives of the distortion-tolerant BLI fan design in the future have also been presented. The motivation of this work is to provide some useful guidelines for the upcoming research works concerning the BLI fan based propulsion systems.</div></div>","PeriodicalId":54553,"journal":{"name":"Progress in Aerospace Sciences","volume":"154 ","pages":"Article 101082"},"PeriodicalIF":11.5000,"publicationDate":"2025-04-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":"{\"title\":\"A systematic review of boundary layer ingestion (BLI) fan: Current Status and future perspectives\",\"authors\":\"Tao Ma , Hanan Lu , Qiushi Li\",\"doi\":\"10.1016/j.paerosci.2025.101082\",\"DOIUrl\":null,\"url\":null,\"abstract\":\"<div><div>The distributed propulsion system has a significant potential for reducing the fuel consumption, noise and pollution emissions for the next-generation aircraft and become a current hot research topic. As the core component of the distributed propulsion system, the boundary layer ingestion fan has been continuously operating under the distorted inflow conditions, which largely degrades the aerodynamic performance of the fan itself. In turn, the degradation of the BLI fan performance will have a severe impact on the overall aerodynamic benefits achievement of the aircraft. This paper has conducted a systematic review of the boundary layer ingestion fan. Firstly, the aerodynamic benefits of BLI propulsion system has been overviewed. Then, different types of BLI fan based propulsion configurations have been introduced and the distinguished features of the distorted inflows for each configuration are analyzed in detail. Thirdly, the fan aerodynamic responses to the BLI distorted inflow are given and the influences of the BLI inflow distortion on the fan aerodynamic performances and internal flow fields are fully investigated. Subsequently, the potential performance evaluation methods, mainly the low-order computational approaches, used in the preliminary design stage of the fan have been comprehensively overviewed. Finally, the research works concerning the attempts for the fan/compressor design under non-uniform inflow condition are reviewed and some perspectives of the distortion-tolerant BLI fan design in the future have also been presented. The motivation of this work is to provide some useful guidelines for the upcoming research works concerning the BLI fan based propulsion systems.</div></div>\",\"PeriodicalId\":54553,\"journal\":{\"name\":\"Progress in Aerospace Sciences\",\"volume\":\"154 \",\"pages\":\"Article 101082\"},\"PeriodicalIF\":11.5000,\"publicationDate\":\"2025-04-01\",\"publicationTypes\":\"Journal Article\",\"fieldsOfStudy\":null,\"isOpenAccess\":false,\"openAccessPdf\":\"\",\"citationCount\":\"0\",\"resultStr\":null,\"platform\":\"Semanticscholar\",\"paperid\":null,\"PeriodicalName\":\"Progress in Aerospace Sciences\",\"FirstCategoryId\":\"5\",\"ListUrlMain\":\"https://www.sciencedirect.com/science/article/pii/S0376042125000089\",\"RegionNum\":1,\"RegionCategory\":\"工程技术\",\"ArticlePicture\":[],\"TitleCN\":null,\"AbstractTextCN\":null,\"PMCID\":null,\"EPubDate\":\"\",\"PubModel\":\"\",\"JCR\":\"Q1\",\"JCRName\":\"ENGINEERING, AEROSPACE\",\"Score\":null,\"Total\":0}","platform":"Semanticscholar","paperid":null,"PeriodicalName":"Progress in Aerospace Sciences","FirstCategoryId":"5","ListUrlMain":"https://www.sciencedirect.com/science/article/pii/S0376042125000089","RegionNum":1,"RegionCategory":"工程技术","ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"Q1","JCRName":"ENGINEERING, AEROSPACE","Score":null,"Total":0}
A systematic review of boundary layer ingestion (BLI) fan: Current Status and future perspectives
The distributed propulsion system has a significant potential for reducing the fuel consumption, noise and pollution emissions for the next-generation aircraft and become a current hot research topic. As the core component of the distributed propulsion system, the boundary layer ingestion fan has been continuously operating under the distorted inflow conditions, which largely degrades the aerodynamic performance of the fan itself. In turn, the degradation of the BLI fan performance will have a severe impact on the overall aerodynamic benefits achievement of the aircraft. This paper has conducted a systematic review of the boundary layer ingestion fan. Firstly, the aerodynamic benefits of BLI propulsion system has been overviewed. Then, different types of BLI fan based propulsion configurations have been introduced and the distinguished features of the distorted inflows for each configuration are analyzed in detail. Thirdly, the fan aerodynamic responses to the BLI distorted inflow are given and the influences of the BLI inflow distortion on the fan aerodynamic performances and internal flow fields are fully investigated. Subsequently, the potential performance evaluation methods, mainly the low-order computational approaches, used in the preliminary design stage of the fan have been comprehensively overviewed. Finally, the research works concerning the attempts for the fan/compressor design under non-uniform inflow condition are reviewed and some perspectives of the distortion-tolerant BLI fan design in the future have also been presented. The motivation of this work is to provide some useful guidelines for the upcoming research works concerning the BLI fan based propulsion systems.
期刊介绍:
"Progress in Aerospace Sciences" is a prestigious international review journal focusing on research in aerospace sciences and its applications in research organizations, industry, and universities. The journal aims to appeal to a wide range of readers and provide valuable information.
The primary content of the journal consists of specially commissioned review articles. These articles serve to collate the latest advancements in the expansive field of aerospace sciences. Unlike other journals, there are no restrictions on the length of papers. Authors are encouraged to furnish specialist readers with a clear and concise summary of recent work, while also providing enough detail for general aerospace readers to stay updated on developments in fields beyond their own expertise.