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武颖韬1(), 费立涵1, 孔祥东1, 王帜2, 汤成龙1(), 黄佐华1
收稿日期:
2024-01-22
修回日期:
2024-03-24
出版日期:
2024-03-27
通讯作者:
汤成龙
作者简介:
武颖韬(1993—),男,博士,讲师,wuyingtao@xjtu.edu.cn
基金资助:
Yingtao WU1(), Lihan FEI1, Xiangdong KONG1, Zhi WANG2, Chenglong TANG1(), Zuohua HUANG1
Received:
2024-01-22
Revised:
2024-03-24
Online:
2024-03-27
Contact:
Chenglong TANG
摘要:
利用落滴法对比了三种咪唑二氰胺离子液体分别掺混糠醇的自燃特性,使用高速相机和红外相机同步获得了燃料自燃过程的宏观、微观及红外图像;从液面下方拍摄了液滴与液池的混合反应过程。实验观察到了典型的三阶段自燃现象:铺展混合、气相产物生成及火核出现-火焰传播,使用着火延迟时间对燃料的自燃活性进行了定量表征,并计算了糠醇比例对混合燃料推进性能的影响。结果表明,糠醇添加可以显著降低混合燃料黏度,促进燃料与氧化剂的混合,加速自燃过程高温气雾产物的出现。混合燃料的着火延迟时间随糠醇添加比例非单调变化,着火延迟最短的掺混比随液滴速度的增加而增大;混合燃料推进性能受糠醇添加的影响较小。本研究可为自燃离子液体推进剂的开发及利用提供参考。
中图分类号:
武颖韬, 费立涵, 孔祥东, 王帜, 汤成龙, 黄佐华. 咪唑二氰胺离子液体掺混糠醇的自燃及推进性能[J]. 化工学报, DOI: 10.11949/0438-1157.20240102.
Yingtao WU, Lihan FEI, Xiangdong KONG, Zhi WANG, Chenglong TANG, Zuohua HUANG. Hypergolic ignition characteristics and propulsion performance of imidazolium dicyanamide ionic liquids blended with furfuryl alcohol[J]. CIESC Journal, DOI: 10.11949/0438-1157.20240102.
燃料 | 分子结构 | ρ /gcm-3 | 黏度/mPas | σ (mN/m) | ΔHf (kJ/mol) |
---|---|---|---|---|---|
[AMIM][DCA] | 1.1 | 11.2 | 52.8 | 382.0 | |
[BMIM][DCA] | 1.1 | 36.0 | 42.1 | 266.5 | |
[EMIM][DCA] | 1.1 | 16.0 | 49.7 | 258.6 | |
FA | 1.1 | 5.3 | 38.0 | -179.8 |
表 1 燃料分子结构及室温下物性参数[16, 25, 28]
Table 1 Fuel molecular structures and physical properties at room temperature[16, 25, 28]
燃料 | 分子结构 | ρ /gcm-3 | 黏度/mPas | σ (mN/m) | ΔHf (kJ/mol) |
---|---|---|---|---|---|
[AMIM][DCA] | 1.1 | 11.2 | 52.8 | 382.0 | |
[BMIM][DCA] | 1.1 | 36.0 | 42.1 | 266.5 | |
[EMIM][DCA] | 1.1 | 16.0 | 49.7 | 258.6 | |
FA | 1.1 | 5.3 | 38.0 | -179.8 |
图5 纯[BMIM][DCA]与Vf = 0.5的[BMIM][DCA]/FA混合燃料自燃前期液面下图像
Fig. 5 Morphology of pure [BMIM][DCA] and 50%FA/50%[BMIM][DCA] blend in the early stage of hypergolic ignition beneath the liquid surface
燃料 | C* / m·s-1 | CF | Ivac / m·s-1 | Isp / m·s-1 |
---|---|---|---|---|
[AMIM][DCA], Vf =0.00 | 1534.7 | 1.8236 | 2893.0 | 2798.8 |
[AMIM][DCA], Vf =0.25 | 1529.2 | 1.8260 | 2887.4 | 2792.3 |
[AMIM][DCA], Vf =0.50 | 1523.6 | 1.8284 | 2881.6 | 2785.7 |
[AMIM][DCA], Vf =0.75 | 1517.7 | 1.8310 | 2875.7 | 2778.9 |
[BMIM][DCA], Vf =0.00 | 1539.5 | 1.8257 | 2905.9 | 2810.8 |
[BMIM][DCA], Vf =0.25 | 1533.3 | 1.8275 | 2897.7 | 2802.0 |
[BMIM][DCA], Vf =0.50 | 1526.6 | 1.8294 | 2889.0 | 2792.7 |
[BMIM][DCA], Vf =0.75 | 1519.4 | 1.8314 | 2879.7 | 2782.7 |
[EMIM][DCA], Vf =0.00 | 1531.3 | 1.8243 | 2887.7 | 2793.6 |
[EMIM][DCA], Vf =0.25 | 1526.6 | 1.8266 | 2883.4 | 2788.4 |
[EMIM][DCA], Vf =0.50 | 1521.8 | 1.8288 | 2878.9 | 2783.1 |
[EMIM][DCA], Vf =0.75 | 1516.8 | 1.8312 | 2874.4 | 2777.6 |
FA | 1511.7 | 1.8336 | 2869.6 | 2771.9 |
表 2 不同混合燃料的推进性能参数
Table 2 Propulsion performance parameters of different fuel blends
燃料 | C* / m·s-1 | CF | Ivac / m·s-1 | Isp / m·s-1 |
---|---|---|---|---|
[AMIM][DCA], Vf =0.00 | 1534.7 | 1.8236 | 2893.0 | 2798.8 |
[AMIM][DCA], Vf =0.25 | 1529.2 | 1.8260 | 2887.4 | 2792.3 |
[AMIM][DCA], Vf =0.50 | 1523.6 | 1.8284 | 2881.6 | 2785.7 |
[AMIM][DCA], Vf =0.75 | 1517.7 | 1.8310 | 2875.7 | 2778.9 |
[BMIM][DCA], Vf =0.00 | 1539.5 | 1.8257 | 2905.9 | 2810.8 |
[BMIM][DCA], Vf =0.25 | 1533.3 | 1.8275 | 2897.7 | 2802.0 |
[BMIM][DCA], Vf =0.50 | 1526.6 | 1.8294 | 2889.0 | 2792.7 |
[BMIM][DCA], Vf =0.75 | 1519.4 | 1.8314 | 2879.7 | 2782.7 |
[EMIM][DCA], Vf =0.00 | 1531.3 | 1.8243 | 2887.7 | 2793.6 |
[EMIM][DCA], Vf =0.25 | 1526.6 | 1.8266 | 2883.4 | 2788.4 |
[EMIM][DCA], Vf =0.50 | 1521.8 | 1.8288 | 2878.9 | 2783.1 |
[EMIM][DCA], Vf =0.75 | 1516.8 | 1.8312 | 2874.4 | 2777.6 |
FA | 1511.7 | 1.8336 | 2869.6 | 2771.9 |
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