预冷组合动力高超声速空天飞机关键技术研究进展  

Progress on Key Technologies of Hypersonic Aerospace Plane with Pre-Cooled Combined Propulsion

作　　者：邓帆[1,2] 谭慧俊[3] 董昊[4] 付秋军[1] 尘军[1] 

机构地区：[1]中国运载火箭技术研究院空间物理重点实验室,北京100076 [2]谢菲尔德大学机械工程学院 [3]南京航空航天大学能源与动力学院,江苏南京210016 [4]南京航空航天大学航空宇航学院,江苏南京210016

出　　处：《推进技术》2018年第1期1-13,共13页Journal of Propulsion Technology

基　　金：留学基金委航天国际化创新型人才培养项目([2015]5138);中国航天科技集团公司航天科技创新基金资助项目

摘　　要：为进一步加快反应时间、降低发射成本,各国加大了对可重复使用组合动力空天飞机的研发。英国采用预冷组合发动机SABRE的高超声速空天飞机Skylon项目在宽速域组合动力方面已取得突破性进展。本文首先对其动力系统中的关键技术如轻质高效空气预冷器、内循环换热系统以及高度补偿集成喷管进行了介绍;然后分析了面对不同任务需求的各阶段总体方案迭代,重点关注高空低密度条件下的高速布局设计、气动相关问题以及热防护措施;最后对载荷投放成本进行了横向比较,并阐述了欧空局对其作为下一代欧洲空天运输系统的任务规划。To speed up the response time and reduce launch costs,the research of reusable aerospace plane based on combined propulsion is enhanced in many countries. The British hypersonic aerospace plane project Skylon with pre-cooling SABRE engine has made breakthroughs on the propulsion with a wide range of speed.The key technologies of propulsion system of Skylon such as light and efficient air pre-cooler,circulating heat transfer system as well as highly integrated altitude compensating nozzles are presented firstly. Then the various stages of the overall program with different mission objectives are discussed. The discussion mainly focuses on the hypersonic layout design at a high altitude and low density condition,aerodynamic related techniques and thermal protection measures. At last,a comparison with launching costs is carried out and the Skylon performed as the next-generation European aerospace transport system by ESA is expounded.

关 键 词：组合动力 空天飞机 空气预冷器 任务规划 

分 类 号：V211.7[航空宇航科学与技术—航空宇航推进理论与工程] V236