期刊
COMBUSTION THEORY AND MODELLING
卷 24, 期 1, 页码 1-14出版社
TAYLOR & FRANCIS LTD
DOI: 10.1080/13647830.2019.1649727
关键词
agglomeration; combustion; structure analysis; organic fluoride; propellant
资金
- National High-tech Research and Development Program (863 Program) of China
The combustion process of Al particles in an aluminised solid propellant containing organic fluoride (S-OF) has been investigated in comparison to that of a normal solid propellant (S-n). The agglomeration process of ignited Al particles on the burning surface was recorded by means of microscopic high-speed photography. The records showed that the ignited Al particles in propellant S-n tended to form large, homogeneous agglomerates on the burning surface, whereas the ignited Al particles in propellant S-OF tended to form distinct, coherent yet discrete agglomerates with a flocculent structure. The combusting agglomerates were quenched with cold acetone to obtain the burning-interrupted agglomerates, and morphological and surface element distribution analyses were performed on these quenched agglomerates by SEM with EDX. The results showed the quenched agglomerates from S-n to be large (50-100 mu m) and to have an obvious 'cap-core' structure, with the 'cap' and 'core' consisting mostly of aluminum oxide (Al2O3) and unreacted aluminum (Al), respectively. In contrast to those from S-n, the quenched agglomerates from S-OF were spherical and much smaller (5-20 mu m), with uniform dispersal of Al, O, and F on their surfaces. The solid agglomerate products from complete combustion of the propellants in an oxygen bomb were collected and further analysed by TEM, selected area electron diffraction (SAED), and XRD. The results indicated that the propellant S-n tended to form solid combustion products with a dense crystalline structure, whereas the propellant S-OF tended to form solids with a more irregular inner structure of low crystallinity. The above results suggested that the ignition/agglomeration/combustion process of Al in S-OF did not obey the prototypical model for aluminised solid propellants. The effect of fluoridation on Al particles during the combustion process of the solid propellant containing organic fluoride has been confirmed and is considered to be a crucial factor in giving rise to the observed phenomena.
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