丁羟推进剂高压燃速及其调控方法研究进展
Research Progress on High-pressure Burning Rate and Regulation Methods of HTPB Propellants
查看参考文献80篇
|
文摘
|
从丁羟推进剂的燃烧波结构出发,分析了高低压下推进剂燃烧火焰结构和燃面结构的变化,并借助燃速表达式阐明气固两相的传热传质是影响燃速的重要因素。综述了HTPB、AP粒径分布、RDX和HMX粒径等对丁羟推进剂高压燃速的影响,总结了金属氧化物、二茂铁及其衍生物、纳米催化剂、碳材料及其复合物、复合燃速调节剂在燃烧性能调控方面的研究进展,并分析了高压下丁羟推进剂发生燃速突增的可能原因。最后指出今后应加强以下几方面研究: (1)研究配方对丁羟推进剂高压燃烧性能的影响,阐明燃速拐点压强的变化规律; (2)研究压强对丁羟推进剂中各个组分燃烧特性以及组分之间相互作用的影响; (3)开发新型燃速调节剂,实现对丁羟推进剂高压燃烧性能的有效调控。 |
|
其他语种文摘
|
The combustion wave structure of HTPB propellants was introduced,and the changes of the combustion flame structure and burning surface structure of the propellants under different pressures were analyzed. The burning rate expression was used to clarify that the heat and mass transfer between the gas-phase and condensed-phase were important affecting factors for the burning rate of propellant. The effects of HTPB,AP particle size distribution,particle size of RDX and HMX in HTPB propellants on high-pressure burning rate were reviewed,the research progress of metal oxides,ferrocene and its derivatives,nano-catalysts,carbon materials and their composites,and catalyst composites in the control of combustion performance was summarized,and the possible reasons for the drastically increase on the burning rate under high pressure were analyzed. Ultimately,it is pointed out that the following researches should be strengthened in the future: (1) Studying the effect of formulations on the high-pressure combustion characteristics of HTPB propellants and clarifying the change law of the pressure where the pressure exponent breaks; (2) Studying the effect of pressure on the combustion characteristics of each component and the interaction between components in the HTPB propellants; (3) Developing new types of burning rate agents to effectively control the high-pressure combustion performance of HTPB propellants. |
|
来源
|
火炸药学报
,2022,45(4):452-465 【核心库】
|
|
DOI
|
10.14077/j.issn.1007-7812.202203002
|
|
关键词
|
丁羟推进剂
;
高压燃速
;
燃速调节剂
;
调控方法
;
研究进展
|
|
地址
|
西北工业大学, 燃烧、热结构与内流场重点实验室, 陕西, 西安, 710072
|
|
语种
|
中文 |
|
文献类型
|
综述型 |
|
ISSN
|
1007-7812 |
|
学科
|
武器工业;航天(宇宙航行) |
|
基金
|
国家自然科学基金
|
|
文献收藏号
|
CSCD:7288120
|
参考文献 共
80
共4页
|
|
1.
任庆华. 固体小运载火箭发动机的现状及发展趋势分析.
现代防御技术,2016,44(5):40-45
|
CSCD被引
4
次
|
|
|
|
|
2.
吴太霞. 国外坦克武器系统精确打击技术现状及发展趋势.
兵工学报,2010,31(2):66-69
|
CSCD被引
2
次
|
|
|
|
|
3.
胡松启. 高压强下推进剂燃速特性初步分析.
中国宇航学会固体火箭推进专业委员会第二十一届年会,2004
|
CSCD被引
1
次
|
|
|
|
|
4.
中国航天工业总公司.
世界导弹与航天发动机大全,1999
|
CSCD被引
15
次
|
|
|
|
|
5.
Kubota N.
Propellants and Explosives: Thermochemical Aspects of Combustion,2015
|
CSCD被引
5
次
|
|
|
|
|
6.
Hedman T D. The diffusion flame structure of an ammonium perchlorate based composite propellant at elevated pressures.
Proceedings of the Combustion Institute,2013,34(1):649-656
|
CSCD被引
1
次
|
|
|
|
|
7.
Isert S. Oxidizer coarse-to-fine ratio effect on microscale flame structure in a bimodal composite propellant.
Combustion and Flame,2016,163:406-413
|
CSCD被引
4
次
|
|
|
|
|
8.
Gross M L. Coupling micro and meso-scale combustion models of AP/HTPB propellants.
Combustion and Flame,2013,160(5):982-992
|
CSCD被引
6
次
|
|
|
|
|
9.
Zou X. Investigation on the microscale combustion characteristics of AP/HTPB propellant under wide pressure range.
Fuel,2021,306(15):121652
|
CSCD被引
6
次
|
|
|
|
|
10.
Li S. Research on the combustion machanism of the high burning rate solid propellant under high transient pressure conditions.
51st AIAA/SAE/ASEE Joint Propulsion Conference,2015
|
CSCD被引
1
次
|
|
|
|
|
11.
Kuo K K.
Applications of Turbulent and Multi-Phase Combustion,2012
|
CSCD被引
1
次
|
|
|
|
|
12.
Chen J K. Chemistry and kinetics of hydroxyl-terminated polybutadiene (HTPB) and diisocyanate-HTPB polymers during slow decomposition and combustion-like conditions.
Combustion and Flame,1991,87(3/4):217-232
|
CSCD被引
2
次
|
|
|
|
|
13.
Cai W. A model of AP/HTPB composite propellant combustion in rocket-motor environments.
Combustion Science and Technology,2008,180(12):2143-2169
|
CSCD被引
24
次
|
|
|
|
|
14.
Chiaverini M J. Pyrolysis behavior of hybrid-rocket solid fuels under rapid heating conditions.
Journal of Propulsion and Power,1999,15(6):888-895
|
CSCD被引
12
次
|
|
|
|
|
15.
Dennis C. On the combustion of heterogeneous AP/HTPB composite propellants: A review.
Fuel,2019,254(15):115646.1-115646.15
|
CSCD被引
11
次
|
|
|
|
|
16.
胡松启.
固体火箭发动机燃烧基础,2015
|
CSCD被引
3
次
|
|
|
|
|
17.
Cohen N S. Role of binders in solid propellant combustion.
AIAA Journal,2012,12(12):107
|
CSCD被引
2
次
|
|
|
|
|
18.
孙晓飞. 不同粘合剂对燃气发生剂燃烧性能的影响.
固体火箭技术,2018,41(4):462-466
|
CSCD被引
1
次
|
|
|
|
|
19.
Dillier C. Veryhigh-pressure burning rates of aluminized and nonaluminized AP/HTPB-composite propellants.
Journal of Propulsion and Power,2021(1):1-8
|
CSCD被引
1
次
|
|
|
|
|
20.
Boggs T L. Deflagration rate,surface structure,and subsurface profile of self-deflagrating single crystals of ammonium perchlorate.
AIAA Journal,1970,8(5):867-873
|
CSCD被引
2
次
|
|
|
|
|
了解气象卫星更多信息，请访问