TY - JOUR
T1 - Dynamic ignition and combustion characteristics of agglomerated boron-magnesium particles in hot gas flow
AU - Li, Chao
AU - Hu, Chunbo
AU - Deng, Zhe
AU - Hu, Xu
AU - Li, Yue
AU - Wei, Jinjia
N1 - Publisher Copyright:
© 2020 Elsevier Masson SAS
PY - 2021/3
Y1 - 2021/3
N2 - Boron-based fuel is the most attractive energy source for ramjets and scramjets because of its high calorific value. Due to magnesium's excellent combustion performance, adding magnesium as a promoter for boron ignition and combustion was proposed. The combustion mechanisms of boron-based fuel become more complicated after adding magnesium. At the same time, because of the high viscosity B2O3 on boron's surface, fuels always come into combustion in agglomerated state. Therefore, the dynamic ignition and combustion characteristics of agglomerated boron-magnesium particles were investigated experimentally in this paper, which could provide the basic and key parameters for combustor design. The particles investigated here were prepared by drying a mixture of micron sized boron and magnesium slurry. The experiment results indicated that the combustion process of agglomerated boron-magnesium particles can be divided into agglomerated combustion and micro-explosion combustion. The micro-explosion phenomenon is related to the core-shell structure formed during the particle's heating process. With magnesium content being increased, the combustion type will transit from agglomerated combustion to micro-explosion combustion. The transition region of combustion type is the condition that when magnesium content reaches 10-20%. When magnesium content reaches 30%, it has no obvious effect on the combustion of agglomerated boron-magnesium particles. The critical ignition temperature for magnesium containing samples is ranging from 1279 K to 1346 K, and for magnesium free sample is 1670 K. The ignition delay time for samples with magnesium is shortened from 132-164 ms at 1279 K to 26-38 ms at 1673 K, with a reduction of 80%.
AB - Boron-based fuel is the most attractive energy source for ramjets and scramjets because of its high calorific value. Due to magnesium's excellent combustion performance, adding magnesium as a promoter for boron ignition and combustion was proposed. The combustion mechanisms of boron-based fuel become more complicated after adding magnesium. At the same time, because of the high viscosity B2O3 on boron's surface, fuels always come into combustion in agglomerated state. Therefore, the dynamic ignition and combustion characteristics of agglomerated boron-magnesium particles were investigated experimentally in this paper, which could provide the basic and key parameters for combustor design. The particles investigated here were prepared by drying a mixture of micron sized boron and magnesium slurry. The experiment results indicated that the combustion process of agglomerated boron-magnesium particles can be divided into agglomerated combustion and micro-explosion combustion. The micro-explosion phenomenon is related to the core-shell structure formed during the particle's heating process. With magnesium content being increased, the combustion type will transit from agglomerated combustion to micro-explosion combustion. The transition region of combustion type is the condition that when magnesium content reaches 10-20%. When magnesium content reaches 30%, it has no obvious effect on the combustion of agglomerated boron-magnesium particles. The critical ignition temperature for magnesium containing samples is ranging from 1279 K to 1346 K, and for magnesium free sample is 1670 K. The ignition delay time for samples with magnesium is shortened from 132-164 ms at 1279 K to 26-38 ms at 1673 K, with a reduction of 80%.
KW - Agglomerated particle
KW - Boron-magnesium fuel
KW - Dynamic ignition and combustion
KW - Micro-explosion
KW - Solid fuel ramjet/scramjet
UR - https://www.scopus.com/pages/publications/85099184608
U2 - 10.1016/j.ast.2020.106478
DO - 10.1016/j.ast.2020.106478
M3 - 文章
AN - SCOPUS:85099184608
SN - 1270-9638
VL - 110
JO - Aerospace Science and Technology
JF - Aerospace Science and Technology
M1 - 106478
ER -