Research Progress of Aluminum Core-shell Materials Coated with Fluorine-containing Polymer Materials

被引:0
|
作者
Guo X. [1 ]
Zhou J. [1 ]
Li H. [2 ]
Wu C. [1 ]
Fang H. [1 ]
Deng P. [1 ]
Zhu Y. [1 ]
Liu R. [1 ]
机构
[1] State Key Laboratory of Explosive Science and Technology, Beijing Institute of Technology, Beijing
[2] Liaoning Qingyang Special Chemical Co., Ltd., Liaoning, Liaoyang
来源
Binggong Xuebao/Acta Armamentarii | 2024年 / 45卷 / 05期
关键词
aluminum core-shell material; coating; composite solid propellant; fluorinated polymer;
D O I
10.12382/bgxb.2022.1022
中图分类号
学科分类号
摘要
Aluminum (Al) is the most popular metal additive in the field of composite solid propellants due to its high calorific value, high density and low oxygen consumption. In order to improve the performance of composite solid propellant, it is necessary to take measures to modify Al. In recent years, the fluorine-containing polymer coated Al has attracted wide attention due to its excellent comprehensive properties. This paper introduces the different kinds of metal aluminum core-shell materials coated with fluorine-containing polymer materials, the different coating methods, the properties of aluminum core-shell materials and the mechanism of action of fluorine-containing polymers and aluminum. The enhanced ignition and combustion performances of aluminum core-shell materials are due to the surface reaction between the fluorine-containing polymer and the alumina layer, resulting in a violent oxidation process. At the same time, the combustion agglomeration and combustion efficiency of aluminum core-shell material modified propellant are significantly improved. The problems existing in the research of fluorine-containing polymer coated aluminum materials are discussed, and the conclusion, prospect and possible research direction are put forward. © 2024 China Ordnance Industry Corporation. All rights reserved.
引用
收藏
页码:1534 / 1546
页数:12
相关论文
共 76 条
  • [1] GAO F, ZHANG Z., Review on performance evaluation of solid rocket motors with charge defects, Acta Armamentarii, 42, 8, pp. 1789-1802, (2021)
  • [2] MAHDAVI M, FARROKHPOUR H, TAHRIRI M., Investigation of simultaneous formation of nano-sized CuO and ZnO on the thermal decomposition of ammonium perchlorate for composite solid propellants, Journal of Thermal Analysis & Calorimetry, 132, 2, pp. 879-893, (2018)
  • [3] ARISAWA H, BRILL T B., Flash pyrolysis of hydroxyl-terminated polybutadiene (HTPB) 域: implications of the kinetics to combustion of organic polymers [J], Combustion and Flame, 106, 1, pp. 144-154, (1996)
  • [4] JAIN S, GUPTA G, KSHIRSAGAR D R, Et al., Burning rate and other characteristics of strontium titanate (SrTiO<sub>3</sub> ) supplemented AP / HTPB / Al composite propellants-ScienceDirect [J], Defence Technology, 15, 3, pp. 313-318, (2019)
  • [5] PANG W Q, LI Y, DELUCA L T, Et al., Effect of metal nanopowders on the performance of solid rocket propellants: a review, Nanomaterials, 11, 10, pp. 2749-2774, (2021)
  • [6] AO W, FAN Z M, LIU L, Et al., Agglomeration and combustion characteristics of solid composite propellants containing aluminum-based alloys, Combustion and Flame, 220, 10, pp. 288-297, (2020)
  • [7] VELLAISAMY U, BISWAS S., Effect of metal additives on neutralization and characteristics of AP/ HTPB solid propellants [J], Combustion and Flame, 221, 11, pp. 326-337, (2020)
  • [8] TU C Y, CHEN X, LI Y K, Et al., Experimental study of Al agglomeration on solid propellant burning surface and condensed combustion products, Defence Technology, 26, pp. 111-122, (2023)
  • [9] YUAN J F, LIU J Z, ZHOU Y N, Et al., Aluminum agglomeration of AP/ HTPB composite propellant, Acta Astronautica, 156, 3, pp. 14-22, (2019)
  • [10] WANG D Q, CAO X F, LIU J, Et al., TF-Al/ TiC highly reactive composite particle for application potential in solid propellants [J], Chemical Engineering Journal, 425, 12, (2021)