摘要
在对核反应堆、发动机和传热系统进行概要分析的基础上,初步探讨了核能航空发动机的技术方案。经分析认为:基于目前的技术水平,采用高温气冷堆、双回路传热系统的双布雷顿循环核能涡扇发动机相对可行。
The preliminary investigatiaon of the technical proposals for nuclear aeroengine were presented based on the technological analyses of nuclear reactor,aeroengine and heat transfer system.The analysis results show that the technical proposals are relatively feasible which are the Bi-Brayton nuclear turbofan combined with high temperature gas cooled reactor and double-loop heat transfer system based on the present tecnology capability.
出处
《航空发动机》
2010年第3期45-49,共5页
Aeroengine
关键词
核能航空发动机
核反应堆
传热系统
nuclear aeroengine
nuclear reactor
heat transfer system
