摘要
采用Fluent软件模拟了50t转炉四孔变角和非变角氧枪气体射流,研究了喷孔倾角对氧气射流流场和流股融合距离的影响。结果表明,在距喷头出口距离较近时,各流股独立为自由射流,随着距喷头出口距离的增加,各流股不断扩张,并在一定距离时融合成单股射流;非变角喷头A的流股融合距离为1.3m,与冷态水模实验得出枪位1.3m时炉口溅出量最大是一致的;变角氧枪B至I的对角喷孔倾角不同,射流流股融合了两次,大大降低了炉口溅出量;变角氧枪对角喷孔倾角相差0.5°较对角喷孔倾角相差1°时更有利于射流融合距离的增加;在研究喷孔倾角10.5°~11.5°/12.5°的9个喷头中,倾角11°/11.5°的喷头H射流融合距离最长,其理论炉口喷溅量最少。
The gas jets of variable and non-variable angle four-hole oxygen lances for 50 t BOF have been numerically simulated by using Fluent software to study the effect of inclining angle of jet nozzles on oxygen jet flow field and syncreti- zing length of jet-flows. Results show that in distance near the outlet of jet-nozzle the each jet-flow is independent free-flow, with increasing distance from outlet of jet nozzle the each jet-flow continuously spreads out and merges each other into one jet-flow (stream) at certain distance; the syncretizing distance of jet-flows of non-variable angle jet nozzle A is 1.3 m that is consistent with the cold water simulated test results in which at situation of lance level 1.3 m the spitting amount from furnace is maximum; the inclining angles of opposite angles jet hole of variable angle oxygen lances vary from lance B to lance I, and the jet-flows of these lances syneretize for two times led to abruptly reduce the furnace spitting amount; compared with difference 1° of inclining angles, the variable angle oxygen lances with difference 0, 5 o of inclining angles of opposite angles jet hole is more favorable to increase the syncretizing distance ; among the studied nine jet nozzle with inclining angles 10. 5° - 11.5°/12. 5°, the jet nozzle H with inclining angle 11°/11.5° has maximum jet flow syncretizing distance, its theoretical furnace mouth spitting amount is lowest.
出处
《特殊钢》
北大核心
2014年第4期8-11,共4页
Special Steel
基金
河北省自然科学基金资助项目(No.E2012401063)
关键词
50
t转炉
变角氧枪
射流
融合距离数值模拟
50 t Converter, Variable Angle Oxygen Lance, Jet-Flow, Syncretizing Distance, Numerical Simula- tion