首页 | 本学科首页   官方微博 | 高级检索  
     检索      

航空活塞发动机两级增压匹配方法
引用本文:徐斌,夏绍军,杨世春,姬芬竹,胡延领.航空活塞发动机两级增压匹配方法[J].航空动力学报,2012,27(3):496-500.
作者姓名:徐斌  夏绍军  杨世春  姬芬竹  胡延领
作者单位:北京航空航天大学 交通科学与工程学院, 北京 100191
基金项目:国家自然科学基金(50606014)
摘    要:通过对某单级增压活塞发动机的研究,将两级增压应用于该机型,采用压气机串联、涡轮并联的布置方案,并用GT-Power对发动机进行建模.按等流量模式对两级涡轮增压进行匹配,并对地面至高空10km飞机全飞行高度的运行工况进行了预测.对废气放气阀调节流量进行了计算.结果显示涡轮和压气机在全高度都运行在高效率区内,为两级增压系统的研制提供了良好的基础. 

关 键 词:航空活塞发动机    两级增压    全高度匹配    等涡轮流量    调节
收稿时间:4/7/2011 12:00:00 AM
修稿时间:9/8/2011 12:00:00 AM

Matching of two-stage supercharging aircraft piston engines
XU Bin,XIA Shao-jun,YANG Shi-chun,JI Fen-zhu and HU Yan-ling.Matching of two-stage supercharging aircraft piston engines[J].Journal of Aerospace Power,2012,27(3):496-500.
Authors:XU Bin  XIA Shao-jun  YANG Shi-chun  JI Fen-zhu and HU Yan-ling
Institution:School of Transportation Science and Engineering, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
Abstract:Through the single stage supercharging piston engine’s research,two-stage supercharging applications in this type were applied.The air compressor series and the turbine wheel parallel scheme of arrangement were used to establish the modeling of the engine with GT-Power.According to same-flow method,two-stage supercharger matching was conducted and the waste gate valve flow regulation was calculated.The result demonstrates the turbine wheel and the air compressor in the overall height moves in the high efficiency area,and two levels of supercharging system’s developments have provided the good foundation.
Keywords:aircraft piston engines  two-stage supercharging  full-height matching  same-flow turbines  regulation
本文献已被 CNKI 万方数据 等数据库收录!
点击此处可从《航空动力学报》浏览原始摘要信息
点击此处可从《航空动力学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号