摘要
针对发动机排气管来流条件下涡轮一维性能预测模型进行深入研究,建立脉动与空间不均匀来流条件下涡轮性能预测模型,该模型预测得到的涡轮流通能力与试验误差小于2.0%。将该模型与发动机性能预测模型耦合,开发增压发动机自主性能仿真软件,试验验证结果表明发动机整机的性能预测误差小于3.5%。基于该模型,进一步构建了涡轮与发动机耦合匹配方法,并通过双通道涡轮几何优化设计,实现了发动机功率提升2.7%,同时燃油消耗率降低1.6%。
A one-dimensional turbine performance model was investigated under real engine exhaust environment.The model is capable of performance prediction under pulsating boundary conditions and twin-entry scroll configurations.The discrepancies between experimental and simulated results were less than 2.0%.This turbine model was further coupled with a one-dimensional engine code and an in-house engine performance prediction software was developed.The maximum discrepancy of the whole engine model was 3.5%.A joint engine-turbine design method was further developed based on this model and thus turbine geometries could be considered in the engine design process.A newly designed twin-entry turbine was coupled with the turbocharged engine.The engine power and brake specific fuel consumption could be improved by 2.7%and 1.6%.
作者
魏江山
薛颖娴
杨名洋
马泽泰
邓康耀
WEI Jiangshan;XUE Yingxian;YANG Mingyang;MA Zetai;DENG Kangyao(Key Laboratory for Power Machinery and Engineering of State Education Ministry,Shanghai Jiao Tong University,Shanghai 200240,China)
出处
《内燃机工程》
CAS
CSCD
北大核心
2021年第4期70-76,共7页
Chinese Internal Combustion Engine Engineering
基金
船用低速机工程(一期)研制项目(工信部联装函[2017]21号)。
关键词
涡轮
增压发动机
一维模型
双通道
性能预测
一体化仿真
turbine
turbocharged engine
1D model
twin-entry
performance prediction
integrative simulation