• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

改性双基推进剂和富燃料推进剂的点火延迟时间和燃烧速率的对比研究。

Comparative study on ignition delay time and burning rate of modified double-base propellant and fuel-rich propellant.

机构信息

Nanjing Vocational University of Industry Technology, School of Mechanical Engineering, Yangshan North Road Street, 1, 210023 Nanjing, China.

Nanjing Institute of Technology, School of Energy and Power Engineering, Chunhua Street, n/n, 211167 Nanjing, China.

出版信息

An Acad Bras Cienc. 2023 Oct 30;95(3):e20220762. doi: 10.1590/0001-3765202320220762. eCollection 2023.

DOI:10.1590/0001-3765202320220762
PMID:37909562
Abstract

With the higher requirements of various tactical and technical indicators of the weapon systems, the current research on the ignition and combustion characteristics of different types of solid propellants is not comprehensive. In more complex and harsh environmental conditions, the pressure affects the ignition and combustion characteristics. Therefore, the paper studies the ignition and combustion characteristics of the modified double-base propellants (MDB propellants) and fuel-rich propellants (FR propellants) under low-pressure environment. Combining experiment and theory, the ignition delay time and burning rate of two kinds of solid propellants are compared and analyzed at low pressure by the laser ignition experimental device. The results displayed that the burning flames of the FR and MDB propellant presented evident V-shape and cylindrical, respectively. The flame brightness decreased with the decrease in pressure. With the increase of pressure and heat flux, the ignition delay time of the MDB propellant and the FR propellant decreased. By comparison, Model 2 of the ignition delay time was more effective for the estimation of the ignition delay time of the FR propellant. The experimental results are compared with the three burning rate models, which are the Vielle formula (Model 1), Summerfield formula (Model 2), and B-number burning rate formula (Model 3). The results showed the burning rate was more in accord with Model 3.

摘要

随着武器系统各种战术技术指标要求的提高,目前对不同类型的固体推进剂点火燃烧特性的研究还不够全面。在更加复杂和恶劣的环境条件下,压力会影响点火和燃烧特性。因此,本文研究了改性双基推进剂(MDB 推进剂)和富燃料推进剂(FR 推进剂)在低压环境下的点火和燃烧特性。本文结合实验和理论,利用激光点火实验装置,对两种固体推进剂在低压下的点火延迟时间和燃烧速率进行了对比分析。结果表明,FR 和 MDB 推进剂的燃烧火焰分别呈现明显的 V 形和圆柱形。火焰亮度随压力的降低而降低。随着压力和热流的增加,MDB 推进剂和 FR 推进剂的点火延迟时间减小。相比之下,点火延迟时间模型 2 更能有效地估计 FR 推进剂的点火延迟时间。将实验结果与三种燃烧速率模型进行比较,即 Vielle 公式(模型 1)、Summerfield 公式(模型 2)和 B 数燃烧速率公式(模型 3)。结果表明,燃烧速率与模型 3 更吻合。

相似文献

1
Comparative study on ignition delay time and burning rate of modified double-base propellant and fuel-rich propellant.改性双基推进剂和富燃料推进剂的点火延迟时间和燃烧速率的对比研究。
An Acad Bras Cienc. 2023 Oct 30;95(3):e20220762. doi: 10.1590/0001-3765202320220762. eCollection 2023.
2
First applications of ultrasound technology in solid rocket propellant combustion promotion.超声技术在固体火箭推进剂燃烧促进中的首次应用。
Ultrason Sonochem. 2024 Dec;111:107107. doi: 10.1016/j.ultsonch.2024.107107. Epub 2024 Oct 15.
3
Experimental Study of Pyrolysis and Laser Ignition of Low-Vulnerability Propellants Based on RDX.基于 RDX 的低易损推进剂热解及激光点火的实验研究
Molecules. 2020 May 12;25(10):2276. doi: 10.3390/molecules25102276.
4
Combustion process of a promising catalyst [Cu(Salen)] for HMX-CMDB propellants.用于HMX-CMDB推进剂的一种有前景的催化剂[Cu(Salen)]的燃烧过程。
RSC Adv. 2023 Aug 30;13(37):25853-25861. doi: 10.1039/d3ra04671k. eCollection 2023 Aug 29.
5
Experimental Research on Microwave Ignition and Combustion Characteristics of ADN-Based Liquid Propellant.基于ADN的液体推进剂微波点火及燃烧特性的实验研究
Micromachines (Basel). 2022 Mar 25;13(4):510. doi: 10.3390/mi13040510.
6
Effect of Microwave Power and Gas Flow Rate on the Combustion Characteristics of the ADN-based Liquid Propellant.微波功率和气体流量对基于ADN的液体推进剂燃烧特性的影响
Materials (Basel). 2022 Dec 23;16(1):147. doi: 10.3390/ma16010147.
7
Experimental Study on Microwave-Assisted Ignition and Combustion Characteristics of ADN-Based Liquid Propellant.基于ADN的液体推进剂微波辅助点火及燃烧特性的实验研究
ACS Omega. 2021 Aug 26;6(35):22937-22944. doi: 10.1021/acsomega.1c03591. eCollection 2021 Sep 7.
8
On the combustion mechanisms of ZrH in double-base propellant.关于双基推进剂中氢化锆的燃烧机理
Phys Chem Chem Phys. 2017 Dec 13;19(48):32597-32604. doi: 10.1039/c7cp02593a.
9
Enhancing the Ignition and Combustion Performances of Solid Propellants Incorporating Al Particles Inside Oxidizers.提高在氧化剂内部掺入铝颗粒的固体推进剂的点火和燃烧性能。
ACS Appl Mater Interfaces. 2023 Dec 6;15(48):56442-56453. doi: 10.1021/acsami.3c11961. Epub 2023 Nov 17.
10
Synchronized measurement method of burning rate and combustion temperature of a solid propellant specimen.固体推进剂试样燃速与燃烧温度的同步测量方法
Appl Opt. 2024 May 1;63(13):3420-3429. doi: 10.1364/AO.520172.

引用本文的文献

1
Investigation of aluminum agglomeration characteristics in solid propellants with Al/Mg particle additives.含铝/镁颗粒添加剂的固体推进剂中铝团聚特性研究
Sci Rep. 2025 Jul 6;15(1):24124. doi: 10.1038/s41598-025-10533-w.