Improving the ignition and combustion of JP10/boron-based nanofluid fuel droplets by the interaction of PTFE and boron

被引:8
|
作者
Mao, Zhipeng [1 ]
Zhu, Baozhong [1 ]
Sun, Yunlan [1 ]
Chen, Jiuyu [1 ]
Liu, Jianzhong [2 ]
机构
[1] Changzhou Univ, Sch Petr & Nat Gas Engn, Changzhou 213164, Peoples R China
[2] Zhejiang Univ, Dept Energy Engn, Hangzhou 310058, Peoples R China
基金
中国国家自然科学基金;
关键词
Nanofluid fuel; Boron combustion; Droplet behavior; JP10; POLYTETRAFLUOROETHYLENE; OXIDATION; FLUORINE;
D O I
10.1007/s10973-023-12039-x
中图分类号
O414.1 [热力学];
学科分类号
摘要
With a high demand for high-performance spacecraft, the development of new nanofluid fuels has become a major opportunity and challenge. As solid-liquid hybrid fuels, the combustion of nanofluid fuels is affected by various factors and the combustion performance needs to be improved. In this paper, the JP10/boron (B)-based nanofluid fuel droplets containing polytetrafluoroethylene (PTFE) with 10 mass% nB/PTFE content were prepared by a mechanical mixing method, and their combustion characteristics were investigated, especially the droplet behavior and flame characteristics. Additionally, the effects of nano-sized boron (nB) and nano-sized polytetrafluoroethylene (nPTFE) on the oxygen consumption and reaction characteristics of droplets at different combustion stages were also analyzed. The combustion process of the JP10/B-based nanofluid fuel droplets with nPTFE addition is mainly defined as four stages, namely ignition stage, mixed combustion stage, secondary combustion stage, and boron burning stage. The addition of a small amount of nPTFE to the JP10/B-based nanofluid fuel does not reduce the ignition delay time of the droplet, but the combustible gas products such as CO and CF4 generated by the reaction between nB and nPTFE in the mixed combustion stage can destroy the droplet strongly and enhance the combustion of JP10, so the combustion time of the JP10/B-based nanofluid fuel droplets with nPTFE addition in this stage is shortened by 10.1% compared with that of the JP10/B-based nanofluid fuel droplets. In addition, nPTFE destroys the boron surface oxide layer and improves the combustion efficiency of boron particles, and the maximum burning intensity of droplets can be increased by 47%. The particle size of condensate combustion products is reduced by 85% because the gases generated split the agglomerates into small fragments.
引用
收藏
页码:4185 / 4194
页数:10
相关论文
共 50 条
  • [41] Composition of solid and gaseous primary combustion products of boron-based fuel-rich propellant
    Xu, Peihui
    Liu, Jianzhong
    Zhang, Linqing
    Yuan, Jifei
    Song, Minggang
    Liu, Hui
    ACTA ASTRONAUTICA, 2021, 188 : 36 - 48
  • [42] Enhanced ignition and combustion performance of boron-based energetic materials through surface modification and titanium dioxides coating
    Mondal, Jayanta
    Singh, Sumit Kumar
    Shin, Weon Gyu
    CERAMICS INTERNATIONAL, 2024, 50 (09) : 16598 - 16614
  • [43] Calculation for Primary Combustion Characteristics of Boron-Based Fuel-Rich Propellant Based on BP Neural Network
    Wu Wan'e
    Zhu Zuoming
    JOURNAL OF COMBUSTION, 2012, 2012
  • [44] Elucidating the impact of sodium azide on the thermal and combustion characteristics of boron-based fuel-rich propellants
    Facih, Mohammed El Amin
    Boulkadid, Moulai Karim
    Touidjine, Sabri
    Belkhiri, Samir
    Nourine, Manel
    REACTION KINETICS MECHANISMS AND CATALYSIS, 2024, : 1035 - 1054
  • [45] Theoretical analysis on applying steam reforming to the primary combustion of the boron-based fuel-rich propellant
    Li, Chaolong
    Xia, Zhixun
    Ma, Likun
    Chen, Binbin
    Feng, Yunchao
    Zhang, Jiarui
    Yang, Pengnian
    FUEL, 2024, 361
  • [46] Ignition and combustion of boron-based Al•B•I2 and Mg•B•I2 composites
    Wang, Song
    Abraham, Ani
    Zhong, Ziyue
    Schoenitz, Mirko
    Dreizin, Edward L.
    CHEMICAL ENGINEERING JOURNAL, 2016, 293 : 112 - 117
  • [47] Effect of azide polyether pyrolysis property on combustion and heat release of boron-based fuel-rich propellant
    Zhang, Ximing
    Wu, Wei
    Jin, Peng
    Ding, Shanjun
    Liu, Shuang
    Zhao, Shuai
    Yang, Wu
    Liu, Wenhao
    Luo, Yunjun
    COMBUSTION AND FLAME, 2022, 245
  • [48] Calculation for Primary Combustion Characteristics of Boron-based Fuel-rich Propellant Based on GA-BP Neural Network
    Wu Wan'e
    Zhu Zuoming
    THEORY AND PRACTICE OF ENERGETIC MATERIALS (VOL IX), PROCEEDINGS OF THE 2011 INTERNATIONAL AUTUMN SEMINAR ON PROPELLANTS, EXPLOSIVES AND PYROTECHNICS, 2011, : 923 - 926
  • [49] A Physics-based approach to modeling real-fuel combustion chemistry - III. Reaction kinetic model of JP10
    Tao, Yujie
    Xu, Rui
    Wang, Kun
    Shao, Jiankun
    Johnson, Sarah E.
    Movaghar, Ashkan
    Han, Xu
    Park, Ji-Woong
    Lu, Tianfeng
    Brezinsky, Kenneth
    Egolfopoulos, Fokion N.
    Davidson, David F.
    Hanson, Ronald K.
    Bowman, Craig T.
    Wang, Hai
    COMBUSTION AND FLAME, 2018, 198 : 466 - 476
  • [50] Unraveling the role of dual Ti/Mg metals on the ignition and combustion behavior of HTPB-boron-based fuel
    Arijit Debnath
    Yash Pal
    Sri Nithya Mahottamananda
    Djalal Trache
    Defence Technology, 2024, (02) : 134 - 143