Experimental Investigation on Combustion Characteristics and Agglomeration of Al/NEPE Propellants

被引:2
|
作者
Zhang, Beichen [1 ]
Xu, Jinsheng [1 ]
Feng, Yaya [2 ]
Zhang, Anjie [2 ]
Xiong Chen [1 ]
Cai, Wengxiang [1 ]
Li Yingkun [1 ]
Min Zhu [3 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Mech Engn, Nanjing 210094, Peoples R China
[2] Synthe Chem & Engn Inst Inner Mongolia, Hohhot 010010, Peoples R China
[3] China North Ind Corp, 12 Guanganmen South St, Beijing 100053, Peoples R China
基金
中国国家自然科学基金;
关键词
NEPE propellant; combustion property; ignition pressure; agglomeration; ALUMINUM AGGLOMERATION; COMPOSITE PROPELLANTS; NANO-ALUMINUM; PARTICLE-SIZE; IGNITION; PRODUCTS; MODEL; SANDWICHES; PRESSURE;
D O I
10.1002/prep.202100178
中图分类号
O69 [应用化学];
学科分类号
081704 ;
摘要
In order to understand the ignition and combustion characteristics of NEPE propellants under different pressure conditions and the agglomeration behavior of aluminum particles on the burning surface, the Al/NEPE propellant was tested on a sealed high-pressure laser ignition platform. Laser ignition experiments show that both ignition delay time and combustion time are inversely proportional to ambient pressure. With the increase of pressure, the reduction of ignition delay time and self-sustaining combustion time is reduced. The impact of pressure on ignition and combustion is very complex. We then analyze the effect of pressure on ignition delay time using a theoretical mechanism. High-speed microscopic images display the agglomeration of aluminum particles in propellants mainly through the following three processes: accumulation, aggregation, and agglomeration. It is also found that many aluminum particles are agglomerated on the surface, the aluminum droplet agglomerates formed on the combustion surface are separated from the combustion surface, and the agglomerates rupture and flow out of the liquid alumina during the combustion process. The phenomenon of secondary agglomeration is also observed. The microstructure and elemental composition of combustion products of aluminum particles in NEPE propellant were obtained by scanning electron microscopy (SEM) and energy dispersive spectrometer (EDS). The detection results confirmed some agglomeration phenomena. At 3.0 MPa, the combustion of the propellant sample is sufficient, and the aluminum particles are smooth spherical alumina particles. At 1.0 MPa, the combustion of the propellant sample is insufficient, and the aluminum particles are rough. The particle size under different pressure was analyzed by a laser particle size analyzer. The results show that increasing the pressure can reduce the average agglomeration size of aluminum particles and improve combustion efficiency. The number of large particle aggregates is more at 3 MPa. From the perspective of overall particle size results, within the same diameter interval, the percentage of particle number does not increase or decrease significantly with the increase of pressure.
引用
收藏
页数:16
相关论文
共 50 条
  • [31] Effect of HMX Content on Agglomeration and Condensed Phase Combustion Products of AP/HMX/Al/HTPB Propellants
    Gou D.-L.
    Ao W.
    Liu L.
    Wu H.-M.
    Liu P.-J.
    He G.-Q.
    [J]. Hanneng Cailiao/Chinese Journal of Energetic Materials, 2022, 30 (06): : 571 - 578
  • [32] Experimental and model study of agglomeration of burning aluminized propellants
    Liu, TK
    [J]. JOURNAL OF PROPULSION AND POWER, 2005, 21 (05) : 797 - 806
  • [33] Agglomeration Characteristics of Aluminum Particles in AP/AN Composite Propellants
    Takahashi, Kenichi
    Oide, Sho
    Kuwahara, Takuo
    [J]. PROPELLANTS EXPLOSIVES PYROTECHNICS, 2013, 38 (04) : 555 - 562
  • [34] Experimental and numerical investigations of the effect of pressure and oxygen concentration on combustion characteristics of Al/Mg fuel-rich propellants
    Li, Lian-bo
    Chen, Xiong
    Zhou, Chang-sheng
    Zhu, Min
    Musa, Omer
    [J]. APPLIED THERMAL ENGINEERING, 2020, 167
  • [35] COMBUSTION CHARACTERISTICS OF SOLID PROPELLANTS IN A VACUUM
    Tanaka, Masafumi
    Tanaka, Munenori
    Seki, Yasukazu
    Urakawa, Katsuya
    [J]. INTERNATIONAL JOURNAL OF ENERGETIC MATERIALS AND CHEMICAL PROPULSION, 2009, 8 (03) : 253 - 266
  • [36] Experimental investigation on the condensed combustion products of aluminized GAP-based propellants
    Liu, Huan
    Ao, Wen
    Liu, Peijin
    Hu, Songqi
    Lv, Xiang
    Gou, Dongliang
    Wang, Haiqing
    [J]. AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 97 (97)
  • [37] Experimental studies on agglomeration characteristics of wheat stalk combustion in fluidized bed
    Teng, Hai-Peng
    Li, Shi-Yuan
    Lü, Qing-Gang
    [J]. Kung Cheng Je Wu Li Hsueh Pao/Journal of Engineering Thermophysics, 2010, 31 (03): : 511 - 514
  • [38] Study on combustion characteristics of NEPE propellant at high pressure
    Coll. of Astronautics, Northwestern Polytechnical Univ., Xi'an 710072, China
    不详
    [J]. Tuijin Jishu, 2008, 4 (508-512):
  • [39] Ignition and Combustion Characteristics of NEPE Propellant in Nitrogen and Air
    Tu C.-Y.
    Chen X.
    Zhou C.-S.
    Zhang B.-C.
    Li L.-B.
    [J]. Hanneng Cailiao/Chinese Journal of Energetic Materials, 2022, 30 (08): : 811 - 818
  • [40] Metal agglomeration in solid propellants combustion part 2: Numerical experiments
    Rashkovsky, SA
    [J]. COMBUSTION SCIENCE AND TECHNOLOGY, 1998, 136 (1-6) : 149 - 169