摘要
提出了一种部分催化发动机方案,该发动机在大范围推力调节时能维持压降基本不变;通过与不催化和全催化方案比较,证明该发动机具有更大的稳定工作范围;对该方案发动机的调节性能开展了仿真研究,当采用斜坡输入时,发动机具有快速、稳定的响应特性.
A partially catalyzed engine scheme was presented. This engine could keep the inject pressure drop almost unchanged when the thrust varies very much. It's proved that this engine functions stably in a wider thrust range if non-catalyzed engine and fully-catalyzed engine are compared. The regulating performance of this engine was also simulated. The results show that the engine's response is rapid and stable when ramp input is employed.
出处
《航空动力学报》
EI
CAS
CSCD
北大核心
2007年第11期1954-1957,共4页
Journal of Aerospace Power
关键词
航空航天推进系统
变推力发动机
稳定性
部分催化
aerospace propulsion system
variable thrust engine
stability
partially cat alyzed