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

膨胀循环发动机推力室传热优化
引用本文:宣智超,刘中祥,齐戎.膨胀循环发动机推力室传热优化[J].火箭推进,2012,38(6):8-15.
作者姓名:宣智超  刘中祥  齐戎
作者单位:北京航天动力研究所,北京,100076
摘    要:针对膨胀循环发动机推力室身部燃气侧的内壁增强换热结构和冷却剂侧的冷却通道结构这两个影响推力室身部换热最关键的结构分别进行多种结构下的数值模拟对比。通过分析各结构的模拟结果,得到了能够合理提高推力室身部换热能力的内壁加肋结构和圆柱段冷却通道深宽比的结构特征。

关 键 词:膨胀循环发动机  推力室  换热增强结构  传热优化

Heat transfer optimization of thrust chamber in expansion cycle engine
XUAN Zhi-chao,LIU Zhong-xiang,QI Rong.Heat transfer optimization of thrust chamber in expansion cycle engine[J].Journal of Rocket Propulsion,2012,38(6):8-15.
Authors:XUAN Zhi-chao  LIU Zhong-xiang  QI Rong
Institution:(Beijing Aerospace Propulsion Institute,Beijing 100076,China)
Abstract:To further enhance the heat transfer capacity while maintaining the pressure drop of the cooling channels and gas wall temperature in control is one of the key technologies in the design of advanced expander cycle engine. Numerical simulation of inner wall heat transfer enhancement struc- ture at the hot-gas side of thrust chamber and the cooling channel structure at the coolant side was made in this paper. The two structures are the most important ones which affect on the thrust chamber heat transfer. By analyzing the numerical simulation results of each structure, the inner structure with ribs which can enhance the heat transfer capacity of the thrust chamber reasonably and the structure characteristics which can improve depth-to-width ratio of cooling channel at the cylindrical section were obtained.
Keywords:expansion cycle engine  thrust chamber  enhancement structure of heat transfer  heat transfer optimization
本文献已被 CNKI 维普 万方数据 等数据库收录!
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