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富氧推火燃烧技术在减压蒸馏装置加热炉上的应用
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作者 魏伯卿 《石油炼制与化工》 CAS CSCD 北大核心 2014年第6期82-85,共4页
介绍了富氧推火燃烧技术在中国石油大港石化分公司5Mt/a原油减压蒸馏装置加热炉上应用的结果。根据该炉的情况,设计了一套用于炼油装置减压加热炉的富氧推火燃烧技术方案,实施该方案后,减压炉燃料能耗降低了5.95%,排烟氧体积分数降低了5... 介绍了富氧推火燃烧技术在中国石油大港石化分公司5Mt/a原油减压蒸馏装置加热炉上应用的结果。根据该炉的情况,设计了一套用于炼油装置减压加热炉的富氧推火燃烧技术方案,实施该方案后,减压炉燃料能耗降低了5.95%,排烟氧体积分数降低了52.8%;富氧推火燃烧技术投资少、效益高,年节能净收益为215.6万元,投资回收期不到10个月。 展开更多
关键词 加热炉 富氧 助燃 局部增氧 燃烧 推火燃烧
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富氧推火燃烧对烯烃加热炉火焰改变的影响
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作者 魏伯卿 《节能》 2014年第3期28-31,共4页
在烯烃装置2台加氢加热炉上实施富氧引火燃烧技术助燃后效果良好,但其中有一个燃烧器的火苗烧及氢气加热管,造成极大的安全隐患。通过对该燃烧器使用富氧推火燃烧技术助燃,改变了该燃烧器的燃烧火焰分布,确保了其燃烧安全稳定,但牺牲了... 在烯烃装置2台加氢加热炉上实施富氧引火燃烧技术助燃后效果良好,但其中有一个燃烧器的火苗烧及氢气加热管,造成极大的安全隐患。通过对该燃烧器使用富氧推火燃烧技术助燃,改变了该燃烧器的燃烧火焰分布,确保了其燃烧安全稳定,但牺牲了一定的节能效率。 展开更多
关键词 加热炉 富氧 助燃 局部增氧 燃烧 推火燃烧
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加热炉富氧推火与引火燃烧的火焰变化规律分析
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作者 魏伯卿 《石油工程建设》 2014年第5期12-16,共5页
文章介绍了富氧推火燃烧技术和富氧引火燃烧技术的原理,以及该技术首次在炼油装置和烯烃装置加热炉改造中的成功应用情况。通过对加热炉富氧推火与引火燃烧应用对比、扁形与圆形富氧喷嘴实验,分析得出:富氧推火燃烧使燃烧火焰向富氧气... 文章介绍了富氧推火燃烧技术和富氧引火燃烧技术的原理,以及该技术首次在炼油装置和烯烃装置加热炉改造中的成功应用情况。通过对加热炉富氧推火与引火燃烧应用对比、扁形与圆形富氧喷嘴实验,分析得出:富氧推火燃烧使燃烧火焰向富氧气体喷射的水平分量方向偏移的距离,要比富氧引火燃烧使燃烧火焰向富氧气体喷射的水平分量反方向偏移的距离大;富氧扁形喷嘴推火燃烧和引火燃烧改变燃烧火焰的程度,要比富氧圆形喷嘴推火燃烧和引火燃烧改变燃烧火焰的程度大。 展开更多
关键词 加热炉 富氧 助燃 局部增氧 推火燃烧 燃烧
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Ignition characteristics and combustion performances of a LO_2/GCH_4 small thrust rocket engine 被引量:2
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作者 ZHANG Jia-qi LI Qing-lian SHEN Chi-bing 《Journal of Central South University》 SCIE EI CAS CSCD 2018年第3期646-652,共7页
A 500 N model engine filled with LO2/GCH4 was designed and manufactured.A series of ignition attempts were performed in it by both head spark plug and body spark plug.Results show that the engine can be ignited but th... A 500 N model engine filled with LO2/GCH4 was designed and manufactured.A series of ignition attempts were performed in it by both head spark plug and body spark plug.Results show that the engine can be ignited but the combustion cannot be sustained when head spark plug applied as the plug tip was set in the gaseous low-velocity zone with thin spray.This is mainly because flame from this zone cannot supply enough ignition energy for the whole chamber.However,reliable ignition and stable combustion can be achieved by body spark plug.As the O/F ratio increases from 2.61 to 3.49,chamber pressure increases from 0.474 to 0.925 MPa and combustion efficiency increases from 57.8%to 95.1%.This is determined by the injector configuration,which cannot produce the sufficiently breakup of the liquid oxygen on the low flow rate case. 展开更多
关键词 LO2/GCH4 small thrust rocket engine ignition characteristic combustion performance
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The Use of Fractal for Prediction of Burning Rate of Composite Solid Propellants 被引量:2
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作者 Manouchehr Nikazar,Mohammad B. Bagherpour,Bahram Dabir (Chem. Eng. Dept., Amirkabir University of Technology (Tehran Polytechnic), No.424, Hafez Ave., Tehran, Iran.) 《Journal of Thermal Science》 SCIE EI CAS CSCD 2000年第4期361-364,共4页
By using the fractal geometry it is possible to calculate the actual AP (Ammonium Perchlorate) surface area and oxidizer-binder interface fractal dimension in the prediction of burning rate of composite solid propella... By using the fractal geometry it is possible to calculate the actual AP (Ammonium Perchlorate) surface area and oxidizer-binder interface fractal dimension in the prediction of burning rate of composite solid propellants. In this investigation, the fractal dimension was determined by a procedure known as the "Box Counting Method". Using this dimension, surface area relations were developed for the rough particles. This method was implemented in the PEM (Petite Ensemble Model) burning rate model. The comparison of burning rates for a typical propellant by the PEM and fractal model shows that the burning rates obtained by using the fractal geometry are slightly less than those obtained by the PEM model. 展开更多
关键词 PEM model composite solid propellant burning rate fractal.
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