TY - JOUR
T1 - Ignition and Combustion Behavior of Sintered-B/MgB2 Combined with KNO3
AU - Sun, Yalun
AU - Ren, Hui
AU - Jiao, Qingjie
AU - Li, Yongnan
AU - Xu, Heming
AU - Yu, Xusheng
AU - Zhang, Wei
AU - Lu, Qingchuan
N1 - Publisher Copyright:
© 2020 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim
PY - 2020/6/1
Y1 - 2020/6/1
N2 - To further enhance the performance of B/KNO3 (BPN) igniter, sintered B/MgB2 (s-B/MgB2) powder was proposed to be used as a boron substitute. The amount of heat release was tested by oxygen bomb and thermogravimetry/differential scanning calorimetry (TG/DSC). s-B/MgB2/KNO3 (sBPN) igniter could not release as much heat as BPN igniter in the oxygen bomb due to the reduced calorific value of the s-B/MgB2. However, calculations show that s-B/MgB2 reached an over 90 % heat release efficiency in oxygen bomb, compared to that of 53.34 % for boron. At heating rate of 10 K min−1 in TG/DSC experiment, 19.5 % sBPN (sBPN with 19.5 wt. % s-B/MgB2 powder) has a heat release of 1815 J g−1 and experienced an exothermic span of 2.10 min, whereas it took 24.5 % BPN (BPN with 24.5 wt. % boron powder) 3.45 min to release 1465 J g−1. The pressure-time curve (P-t curve), burning rate and combustion temperature were determined. The P-t curve indicates that the combustion pressure was more readily established with the sBPN than with the BPN. The maximum pressure rise of sBPN was 362.0 Pa ms−1, whereas the figure for BPN is 77.2 Pa ms−1. Coupled with infrared radiation (IR) temperature thermometer, the distribution of the flame temperature field during combustion was obtained. It is shown that the combustion temperature of 19.5 % sBPN igniter is approximately 800 K higher than that of 24.5 % BPN. IR images of the combustion process show that the temperature difference of the 19.5 % sBPN flame is smaller than that of the 24.5 % BPN. 19.5 % sBPN also produces more hot residue, which contains KMgF3, resulting in a longer high-temperature duration. The higher combustion pressure and temperature and more residue may enable the sBPN to readily ignite the following charge.
AB - To further enhance the performance of B/KNO3 (BPN) igniter, sintered B/MgB2 (s-B/MgB2) powder was proposed to be used as a boron substitute. The amount of heat release was tested by oxygen bomb and thermogravimetry/differential scanning calorimetry (TG/DSC). s-B/MgB2/KNO3 (sBPN) igniter could not release as much heat as BPN igniter in the oxygen bomb due to the reduced calorific value of the s-B/MgB2. However, calculations show that s-B/MgB2 reached an over 90 % heat release efficiency in oxygen bomb, compared to that of 53.34 % for boron. At heating rate of 10 K min−1 in TG/DSC experiment, 19.5 % sBPN (sBPN with 19.5 wt. % s-B/MgB2 powder) has a heat release of 1815 J g−1 and experienced an exothermic span of 2.10 min, whereas it took 24.5 % BPN (BPN with 24.5 wt. % boron powder) 3.45 min to release 1465 J g−1. The pressure-time curve (P-t curve), burning rate and combustion temperature were determined. The P-t curve indicates that the combustion pressure was more readily established with the sBPN than with the BPN. The maximum pressure rise of sBPN was 362.0 Pa ms−1, whereas the figure for BPN is 77.2 Pa ms−1. Coupled with infrared radiation (IR) temperature thermometer, the distribution of the flame temperature field during combustion was obtained. It is shown that the combustion temperature of 19.5 % sBPN igniter is approximately 800 K higher than that of 24.5 % BPN. IR images of the combustion process show that the temperature difference of the 19.5 % sBPN flame is smaller than that of the 24.5 % BPN. 19.5 % sBPN also produces more hot residue, which contains KMgF3, resulting in a longer high-temperature duration. The higher combustion pressure and temperature and more residue may enable the sBPN to readily ignite the following charge.
KW - Energy Release Efficiency
KW - Flame Temperature
KW - Igniter
KW - Ignition Capability
KW - Modified Boron
UR - http://www.scopus.com/inward/record.url?scp=85080040173&partnerID=8YFLogxK
U2 - 10.1002/prep.201900367
DO - 10.1002/prep.201900367
M3 - Article
AN - SCOPUS:85080040173
SN - 0721-3115
VL - 45
SP - 997
EP - 1004
JO - Propellants, Explosives, Pyrotechnics
JF - Propellants, Explosives, Pyrotechnics
IS - 6
ER -