PDF下载 分享
[1]张蒙正,张 玫,严俊峰,等.RBCC动力系统工作模态问题[J].火箭推进,2015,41(02):1-6.
　ZHANG Meng-zheng,ZHANG Mei,YAN Jun-feng,et al.Discussion about work modal of RBCC power system[J].Journal of Rocket Propulsion,2015,41(02):1-6.
点击复制

RBCC动力系统工作模态问题

《火箭推进》[ISSN:1672-9374/CN:CN 61-1436/V] 卷: 41 期数: 2015年02期 页码: 1-6 栏目: 专论与综述 出版日期: 2015-07-30
Title:
Discussion about work modal of RBCC power system
作者:
张蒙正; 张 玫; 严俊峰; 吕奇伟
西安航天动力研究所，陕西 西安 710100
Author(s):
ZHANG Meng-zheng;  ZHANG Mei;  YAN Jun-feng;  Lü Qi-wei
Xi’an Aerospace Propulsion Institute, Xi’an 710100, China
关键词:
RBCC; 工作模态;  模态转换; 研发
Keywords:
RBCC;  work modal;  modal conversion;  development
分类号:
V434-34
文献标志码:
A
摘要:
具有多种工作模态是RBCC动力系统区别于其他发动机的重要特性。灵活运用不同模态和发动机构型，形成不同方案的RBCC动力系统，满足特定的飞行任务，是RBCC动力系统研发的重要思路。模态间的平稳过渡是确保飞行器经济、安全工作的基本条件。深入研究各模态特性、模态转换中的技术问题及解决途径是RBCC动力系统研发的重要技术基础，对指导和引领当前的关键技术攻关也有着重要作用。RBCC动力系统研发的宗旨在于发挥火箭发动机和冲压发动机的优势，弥补单一发动机功能或者性能的不足，突破点在于国家急需与当今技术成熟度的结合。
Abstract:
The manifold work modal of the rocket based combined cycle (RBCC) power system is its leading difference from other power engines. The RBCC power system solution formed by different work modal and engine configuration is the developmental route of RBCC power system, which can satisfy the needs of specific flight mission. The smooth conversion of diverse work modals is the essential need of spacecraft safe work. The intensive research of modal characteristics, technical issues in modal conversion and resolving method is the base of RBCC power system development, and has the important function of shepherding the key technique development. The purpose of developing RBCC power system is to make full use of the advantages of ramjet and rocket engine, remedy the function disfigurement and performance deficiency of LRE or ramjet. The way rests with combination of ripe technology and national demand.

参考文献/References:

[1]李斌, 张蒙正. 基于火箭/冲压组合的临近空间高速飞行器动力系统方案及面临的挑战[C]. 863-705技术论坛, 长沙: 2008.
[2]张蒙正, 李斌, 王君, 等. 关于动力系统的一点思考[J]. 火箭推进, 2013, 39(1): 1-7.
[3]JOHN E B, JOHN R O, JON G W. Concept assessment of a hydrocarbon fueled RBCC-powered military space plane [R]. USA: AIAA, 2004
[4]SIEBENHAAR A, BUJMAN M J. The Strutjet engine: the overlooked option for space launch, AIAA 95-3124[R]. USA: AIAA, 1995.

[5]JASON E Q. ISTAR: project status and ground test engine design, AIAA 2003-5235[R]. USA: AIAA, 2003.

[6]MELVIN J B, ADMAM S. Combined cycle propulsion: aerojet innovations for practical hypersonic vehicles, AIAA 2011-2397[R]. USA: AIAA, 2011.
[7]SADATAKE T, TETSUO H. Sea-level static tests of a rocket-ramjet combined cycle engine model, AIAA 2007- 5389[R]. USA: AIAA, 2007.
[8]THOMaS M, KRIVANEK J M, ROCHE J P. Affordable flight demonstration of the GTX Air-Breathing SSTO vehicle concept, NASA/TM-2003-212315[R]. USA: NASA/ TM, 2003.
[9]黄生洪, 何洪庆, 何国强. 构型及二次燃烧对RBCC引射模态推力性能的影响[J]. 空气动力学学报, 2005, 23(2):139-143.

相似文献/References:

[1]李永洲,刘晓伟,张蒙正,等.马赫数2.5~7.0的二元变几何进气道设计[J].火箭推进,2015,41(05):17.
　LI Yongzhou,LIU Xiaowei,ZHANG Mengzheng,et al.Design of a two dimensional variable geometry inlet with Mach number 2.5~7.0[J].Journal of Rocket Propulsion,2015,41(02):17.
[2]王洪信,徐 旭.火箭基组合循环发动机性能迭代算法研究[J].火箭推进,2015,41(01):56.
　WANG Hong-xin,XU Xu.Research on performance iterative algorithm of rocket based combined cycle engine[J].Journal of Rocket Propulsion,2015,41(02):56.
[3]张蒙正,李 斌,王 君,等.关于RBCC动力系统的思考[J].火箭推进,2013,39(01):1.
　ZHANG Meng-zheng,LI Bin,WANG Jun,et al.Thinking about RBCC propulsion system[J].Journal of Rocket Propulsion,2013,39(02):1.
[4]路媛媛,张蒙正,严俊峰.火箭推力室喷管内激波对RBCC性能影响分析[J].火箭推进,2013,39(05):46.
　LU Yuan-yuan,ZHANG Meng-zheng,YAN Jun-feng.Influences of shock wave in rocket nozzle on RBCC performance[J].Journal of Rocket Propulsion,2013,39(02):46.
[5]燕 珂,单世群,王莉红,等.液体推进剂热稳定性研究方法探讨[J].火箭推进,2014,40(02):90.
　ZHANG Meng-zheng,LI-Bin,LU Yuan-yuan.Thinking about thrust and resistance characteristics of RBCC power system adapting to rectangle section flow passage[J].Journal of Rocket Propulsion,2014,40(02):90.
[6]安佳宁,徐万武.RBCC引射模态冷流试验研究[J].火箭推进,2012,38(04):38.
　AN Jia-ning,XU Wan-wu.Cold flow experimental research of RBCC ejector modal[J].Journal of Rocket Propulsion,2012,38(02):38.
[7]刘永兴,王 魁,曹再勇.RBCC推进系统主火箭发动机气氧/煤油推力室研究[J].火箭推进,2009,35(06):23.
　Liu Yongxing,Wang Kui,Cao Zaiyong.Investigation of GO2/kerosene thrust chamber of the main rocket engine for the RBCC propulsion system[J].Journal of Rocket Propulsion,2009,35(02):23.
[8]张蒙正,李平,陈祖奎.组合循环动力系统面临的挑战及前景[J].火箭推进,2009,35(01):1.
　Zhang Mengzheng,Li Ping,Chen Zukui.Challenge and perspective of combined cycle propulsion system[J].Journal of Rocket Propulsion,2009,35(02):1.
[9]黄伟,罗世彬,王振国,等.火箭基组合循环(RBCC)发动机性能分析[J].火箭推进,2007,33(05):6.
　Huang Wei,Luo Shibin,Wang Zhenguo.Performance analysis of RBCC engine[J].Journal of Rocket Propulsion,2007,33(02):6.
[10]张留欢,杜泉,张蒙正.RBCC发动机火箭-冲压模态理想热力循环优化分析[J].火箭推进,2016,42(03):21.
　ZHANG Liuhuan,DU Quan,ZHANG Mengzheng.Optimum analysis on ideal thermodynamic cycle of RBCC engine at special rocket-ramjet mode[J].Journal of Rocket Propulsion,2016,42(02):21.

备注/Memo

收稿日期：2014-12-13；修回日期：2015-01-09 作者简介：张蒙正（1964—），男，博士，研究员，研究领域为火箭发动机

更新日期/Last Update: 1900-01-01