Investigation of Al-Li particle ignition dynamics with different Li content

被引:2
作者
Liu, Lu [1 ]
Zhang, Wenchao [1 ]
Xiong, Weiqiang [2 ]
Liu, Peijin [1 ,3 ]
He, Guoqiang [1 ]
Ao, Wen [1 ,3 ]
机构
[1] Northwestern Polytech Univ, Natl Key Lab Solid Rocket Prop, Xian 710072, Peoples R China
[2] Hubei Inst Aerosp Chemo Technol, Xiangyang 441003, Peoples R China
[3] Northwestern Polytech Univ, Ningbo Inst, Ningbo 315000, Peoples R China
基金
中国国家自然科学基金;
关键词
Aluminum; Al-Li alloy; Combustion; Model; Ignition delay time; COMBUSTION; AGGLOMERATION;
D O I
10.1016/j.combustflame.2024.113734
中图分类号
O414.1 [热力学];
学科分类号
摘要
Promoting the ignition of aluminum powder is considered an effective method to inhibit the agglomeration of aluminum powder in propellants and enhance combustion efficiency. This study utilizes laser ignition technology and high-speed photography to investigate the ignition and combustion processes of single aluminum particles and aluminum-lithium alloy particles. The focus is on comparing the effects of the diameter of micron-sized metal particles and the lithium content in aluminum-lithium alloy particles on the ignition and combustion processes of metal particles. The results show that the ignition delay time is directly proportional to the diameter of the metal particles and inversely proportional to the lithium content. For the aluminum-lithium alloy particle with a lithium content of 3.5 %, even if the diameter is close to 300 mu m, the ignition delay time is only 125.5 ms, which is much smaller than that of the pure aluminum particle with a diameter of 208 mu m. Compared to aluminum particles and aluminum-lithium alloy particles, there is basically no difference between the two during the combustion stage. However, in the ignition stage, aluminum-lithium alloy particles sequentially exhibit a red gas-phase flame corresponding to lithium and a yellow gas-phase flame corresponding to aluminum. This indicates that during the ignition process of aluminum-lithium alloy particles, lithium first reacts with the oxidative atmosphere and releases heat, providing a heat source for the subsequent ignition of aluminum particles. This also explains why the ignition delay time of metal particles is inversely proportional to the lithium content. An ignition model for aluminum particles in a multi-component atmosphere is established, which further considers the chemical reactions between lithium and oxidative gases, making the model applicable to aluminum-lithium alloy particles. This ignition model effectively describes the impact of particle diameter and lithium content on the ignition process of metal particles. The model is further verified, and the results show that the calculated ignition delay is in good agreement with the experimental data. Overall, this study provides deeper experimental and theoretical insights into the ignition and combustion processes of aluminum-lithium alloys, and the findings can guide the application of aluminum-lithium alloys in propellants.
引用
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页数:10
相关论文
共 34 条
  • [1] Agglomeration and combustion characteristics of solid composite propellants containing aluminum-based alloys
    Ao, Wen
    Fan, Zhimin
    Liu, Lu
    An, Yuxin
    Ren, Jiaren
    Zhao, Mingtao
    Liu, Peijin
    Li, Larry K. B.
    [J]. COMBUSTION AND FLAME, 2020, 220 : 288 - 297
  • [2] Tuning the agglomeration and combustion characteristics of aluminized propellants via a new functionalized fluoropolymer
    Ao, Wen
    Liu, Peijin
    Liu, Huan
    Wu, Shixi
    Tao, Bowen
    Huang, Xuefeng
    Li, Larry K. B.
    [J]. CHEMICAL ENGINEERING JOURNAL, 2020, 382
  • [3] Propellant formulation factors and metal agglomeration in combustion of aluminized solid rocket propellant
    Babuk, VA
    Vassiliev, VA
    Sviridov, VV
    [J]. COMBUSTION SCIENCE AND TECHNOLOGY, 2001, 163 (1-6) : 261 - 289
  • [4] Computer modelling of nano-aluminium agglomeration during the combustion of composite solid propellants
    Balbudhe, Kishor
    Roy, Aviral
    Chakravarthy, S. R.
    [J]. PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2015, 35 : 2471 - 2478
  • [5] Agglomeration in Composite Propellants Containing Different Nano-Aluminum Powders
    Cohen, Ortal
    Michaels, Dan
    Yavor, Yinon
    [J]. PROPELLANTS EXPLOSIVES PYROTECHNICS, 2022, 47 (09)
  • [6] Physical and ballistic characterization of AlH3-based space propellants
    DeLuca, L. T.
    Galfetti, L.
    Severini, F.
    Rossettini, L.
    Meda, L.
    Marra, G.
    D'Andrea, B.
    Weiser, V.
    Calabro, M.
    Vorozhtsov, A. B.
    Glazunov, A. A.
    Pavlovets, G. J.
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2007, 11 (01) : 18 - 25
  • [7] Mechanistic model for aluminum particle ignition and combustion in air
    Desjardin, PE
    Felske, JD
    Carrara, MD
    [J]. JOURNAL OF PROPULSION AND POWER, 2005, 21 (03) : 478 - 485
  • [8] Experimental study of stages in aluminum particle combustion in air
    Dreizin, EL
    [J]. COMBUSTION AND FLAME, 1996, 105 (04) : 541 - 556
  • [9] Experimental characterization of the combustion of single lithium particles with CO2
    Fischer, P.
    Schiemann, M.
    Scherer, V.
    Maas, P.
    Schmid, G.
    Taroata, D.
    [J]. FUEL, 2015, 153 : 90 - 101
  • [10] Ivanov V.Me., 1965, Experimental investigation of the combustion process of natural and emulsified liquid fuels