火箭基组合循环发动机总体布局研究进展（英文）

论文摘要

本综述从总体布局层面综述火箭基组合循环（RBCC）发动机在各个国家的发展现状,旨在展现该型发动机在单级入轨任务中的发展前景,为设计组合循环发动机以及进行空天往返任务规划提供参考。本文将RBCC按照构型特点进行归类并举例介绍,概述了发动机-机身一体化设计情况,并简要介绍了RBCC动力飞行器的任务规划和多目标优化方法。当前,尽管RBCC的研究面临着很多艰难的挑战,但是RBCC具有单级入轨的潜力,能够降低空天往返的成本。对RBCC发动机系统中各个子系统的研究也有利于促进其他相关学科的发展。

论文目录

• 1 Introduction
• 2 Basic characteristics of RBCC engines
•   2.1 Differences between RBCC and combined engines
•   2.2 Components of RBCC engines
•   2.3 Working process of a typical RBCC engine
• 3 Two main conceptual layouts of RBCC engines and progress in their development
•   3.1 Rectangular section RBCC engine
•     3.1.1 Strutjet
•     3.1.2 Northwestern Polytechnic University research program
•     3.1.3 E3 engine
•   3.2 Axisymmetric RBCC engines
•     3.2.1 Supercharged ejector ramjet （SERJ） and scramjet liquid air cycle engine （ScramLACE）
•     3.2.2 Exchange inlet
•     3.2.3 GTX
• 4 Integration design of RBCC powered aircraft
• 5 Mission planning and multidisciplinary design and optimization （MDO） of an RBCCpowered vehicle
• 6 Discussion
• Appendix A:Development of RBCC engines in different countries

文章来源

类型: 期刊论文

作者: Tian-tian ZHANG,Zhen-guo WANG,Wei HUANG,Jian CHEN,Ming-bo SUN

关键词: 火箭基组合循环发动机,单级入轨,空天往返,发动机机身一体化

来源: Journal of Zhejiang University-Science A（Applied Physics & Engineering） 2019年03期

年度: 2019

分类: 工程科技Ⅱ辑

专业: 航空航天科学与工程,动力工程

单位: Department of Aerospace Science and Engineering, National University of Defense Technology

基金: Project supported by the National Natural Science Foundation of China(No.11502291),the Fund of Outstanding Doctoral Dissertation from the Ministry of Education of China(No.201460)

分类号: V438

页码: 163-183

总页数: 21

文件大小: 3577K

下载量: 184