The rapid H2 release from AlH3 dehydrogenation forming porous layer in AlH3/hydroxyl-terminated polybutadiene (HTPB) fuels during combustion

被引:70
作者
Chen, Suhang [1 ]
Tang, Yue [2 ]
Yu, Hongsheng [1 ]
Bao, Lirong [1 ]
Zhang, Wei [1 ]
DeLuca, Luigi T. [3 ]
Shen, Ruiqi [1 ]
Ye, Yinghua [1 ]
机构
[1] Nanjing Univ Sci & Technol, Sch Chem Engn, Nanjing 210094, Jiangsu, Peoples R China
[2] Jiangsu Police Inst, Dept Forens Sci & Technol, Nanjing 210031, Jiangsu, Peoples R China
[3] Politecn Milan, Space Prop Lab SPLab, Dept Aerosp Sci & Technol, I-20156 Milan, Italy
基金
中国国家自然科学基金;
关键词
AlH3; dehydrogenation; HTPB; Avrami-Erofeev mechanism; Porous layer; HYDROXYL-TERMINATED POLYBUTADIENE; THERMAL-DECOMPOSITION; ALUMINUM-HYDRIDE; HYDROGEN GENERATION; ROCKET PROPELLANTS; REGRESSION RATE; STORAGE; KINETICS; PERFORMANCE; BEHAVIOR;
D O I
10.1016/j.jhazmat.2019.02.045
中图分类号
X [环境科学、安全科学];
学科分类号
08 ; 0830 ;
摘要
Although the motivation of AlH3 enhancing combustion were recognized in many research, the promotion mechanism have been rarely explored. Herein, a previously unreported porous layer mechanism when combustion were determined in HTPB/AlH3 fuels by SEM, thermo-analysis and a new simplified calculation method, owing to rapidly released gas phase H-2 from AlH3 dehydrogenation exposing in melting layer. 5/10% 40-80 mu m and 10% 80-200 mu m AlH3-HTPB formulas show the regression rate increase by, 25.7%, 29.0% and 43.0% at Gox = 350 kg/m(2).s, while by 57.2%, 42.0% and 44.2% enhancement at Gox = 150 kg/m(2).s. The low AlH3 content (<= 10%) promotes the regression rate obviously, while excess AlH3 content (>= 20%) promotes slightly as a result of comprehensive factors combined by energy release, a certain porous layer mechanism, aggregated Al2O3 attached on the burning surface and the blocking effect of the gaseous released H-2. A new model predicting the overlapping process of AlH3 dehydrogenation and Al oxidation in air atmosphere was developed by superimposing AlH3 dehydrogenation simulation and corresponding separated Al oxidation simulation. A 1.5th Avrami-Erofeev (A-E) simulation was proposed for Al passivation weight gain between 420 and 520 K with an activation energy of 124.92 kJ/mol and the pre-exponential of 10(boolean AND)12.35.
引用
收藏
页码:53 / 61
页数:9
相关论文
共 38 条
[1]   Combustion characteristics of aluminum hydride at elevated pressure and temperature [J].
Bazyn, T ;
Eyer, R ;
Krier, H ;
Glumac, N .
JOURNAL OF PROPULSION AND POWER, 2004, 20 (03) :427-431
[2]  
Calabro M., 2004, 40 AIAA ASME SAE ASE, DOI [10.2514/6.2004-3823, DOI 10.2514/6.2004-3823]
[3]   Combustion enhancement of hydroxyl-terminated polybutadiene by doping multiwall carbon nanotubes [J].
Chen, Suhang ;
Tang, Yue ;
Yu, Hongsheng ;
Guan, Xinyan ;
DeLuca, Luigi T. ;
Zhang, Wei ;
Shen, Ruiqi ;
Ye, Yinghua .
CARBON, 2019, 144 :472-480
[4]   Effect of azodicarbonamide particles on the regression rate of hydroxyl-terminated polybutadiene (HTPB)-based fuels for hybrid rocket propulsion [J].
Chen, Suhang ;
Tang, Yue ;
Zhang, Wei ;
Shen, Ruiqi ;
DeLuca, Luigi T. ;
Ye, Yinghua .
International Journal of Energetic Materials and Chemical Propulsion, 2017, 16 (02) :103-114
[5]   Regression rate behavior of hybrid rocket solid fuels [J].
Chiaverini, MJ ;
Serin, N ;
Johnson, DK ;
Lu, YC ;
Kuo, KK ;
Risha, GA .
JOURNAL OF PROPULSION AND POWER, 2000, 16 (01) :125-132
[6]   Combustion of alane and aluminum with water for hydrogen and thermal energy generation [J].
Connell, Terrence L., Jr. ;
Risha, Grant A. ;
Yetter, Richard A. ;
Young, Gregory ;
Sundaram, Dilip S. ;
Yang, Vigor .
PROCEEDINGS OF THE COMBUSTION INSTITUTE, 2011, 33 :1957-1965
[7]   Physical and ballistic characterization of AlH3-based space propellants [J].
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. .
AEROSPACE SCIENCE AND TECHNOLOGY, 2007, 11 (01) :18-25
[8]   Characterization of HTPB-based solid fuel formulations: Performance, mechanical properties, and pollution [J].
DeLuca, L. T. ;
Galfetti, L. ;
Maggi, F. ;
Colombo, G. ;
Merotto, L. ;
Boiocchi, M. ;
Paravan, C. ;
Reina, A. ;
Tadini, P. ;
Fanton, L. .
ACTA ASTRONAUTICA, 2013, 92 (02) :150-162
[9]  
DeLuca L.T., 2011, PROGR PROPULSION PHY, V2, P405, DOI [DOI 10.1051/EUCASS/201102405, 10.1051/eucass/201304075]
[10]   On the kinetics of AlH3 decomposition and the subsequent Al oxidation [J].
Eisenreich, Norbert ;
Kessler, Armin ;
Koleczko, Andreas ;
Weiser, Volker .
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2014, 39 (11) :6286-6294