旋转冲压发动机驻涡燃烧技术研究现状分析  

Progress of Research on Trapped Vortex Combustion Technology in Rotated Ramjet

作　　者：邓洋波[1] 钟兢军[1] 

机构地区：[1]大连海事大学机电与材料工程学院,辽宁大连116026

出　　处：《燃气涡轮试验与研究》2006年第3期58-62,共5页Gas Turbine Experiment and Research

摘　　要：旋转冲压发动机是一种全新概念发动机,采用激波增压和驻涡燃烧技术,其显著的高效、低污染特性引起越来越多人关注。本文首先扼要介绍了旋转冲压发动机总体结构,然后介绍了驻涡燃烧技术的概念和研究现状,最后描述了旋转冲压发动机中驻涡燃烧室的结构特点。A new conceptional turbine engine-rotated ramjet, with shock wave compression and trapped vortex combustion technologies, enjoys significant superiority in respect of higher combustion efficiency and lower pollution level. In this paper, the whole structure of rotated ramjet is introduced, the concept and research progress of trapped vortex combustion technology are reviewed and the structure characteristics of rotated ramjet are analyzed.

关 键 词：旋转冲压发动机 激波压缩 驻涡燃烧技术 

分 类 号：V235.21[航空宇航科学与技术—航空宇航推进理论与工程]