| 1. | Relatively little effort has been expended in this country to applying two-phase detonation theory to the combustion stability problem .
在把两相爆震理论应用于燃烧稳定性方面，该国家几乎没做过多少工作。 |
| 2. | Since injection density cannot be varied independently, it is difficult to show conclusively its effect on combustion stability .
由于不可能独立地改变喷射密度，要确定地指出喷射密度对燃烧稳定性的影响是很困难的。 |
| 3. | Combustion stability study based on statistic analysis and self - organizing neural network
基于统计分析和自组织神经网络的燃烧稳定性研究 |
| 4. | On base of pure carbon combustion test data , combustion stability parameter r . was proposed to evaluated combustion stability
以纯碳的测试参数为基准，提出了燃烧稳定性的判别指数rw 。 |
| 5. | This model takes the influence of ten key factors to the combustion stability into seriously consideration , and especially realizes self - studying of each factor with neural network
该模型重点考虑了煤质、负荷等10个因素对锅炉燃烧稳定性的影响，特别是利用神经网络实现了燃烧稳定性各影响因素权重的自学习。 |
| 6. | Finally , a online judgement system of boiler combustion stability and operating economy is developed and realized on a 200mw power station in hebei province . li jingtao ( engineering thermalphysics ) directed by prof . yan shunlin and wang jun
以河北南网某电厂200mw机组锅炉为研究对象，开发了电站锅炉燃烧稳定性及运行经济性在线评判系统，实现了燃烧稳定性及运行经济性的在线综合评判。 |
| 7. | On the base of the study of combustion characteristics of large capacity coal - fired boiler , a fuzzy comprehensive judgement model of boiler combustion stability is established . the methods of fuzzy mathematics and neural network are applied to establish the judgement model with self - studying function
本课题在对我国大容量机组锅炉燃烧特性进行研究的基础上，运用模糊数学和神经网络方法建立了具有自学习功能的锅炉燃烧稳定性模糊综合评判模型。 |
| 8. | This paper researched rules of ignition and combustion stability under pressurized environment , discussed how to calculate ignition temperature , and also studied the effects of many factors , such as categories of semi - coke , total pressure , oxygen concentration , particle size , heating rate , on ignition character
研究了加压条件下半焦的着火规律和燃烧稳定性。讨论了着火温度的确定方法，对加压下影响半焦着火特性的各种因素，如半焦种类、总压、氧浓度、粒径、加热速率等进行了试验研究。 |
| 9. | The effect of secondary fuel nozzle location , the mass flow rate of secondary fuel and outlet area of ejectorjet were studied . the main results are : the geometry structure of ejectorjet can be compatible with other rbcc operation modes by secondary combustion organization ; the distribution of secondary fuel on ejectorjet cross section is significant for secondary combustion stability . spi combustion organization method is promising
实验研究了二次燃料喷注位置、二次燃料喷注量、后体出口面积对引射火箭性能的影响，得到的结论为：通过燃烧组织，引射火箭模态可以和其他工作模态(亚燃超燃)共用燃烧室而不需做大的几何变化；二次燃料在引射火箭通道截面上的分布对于引射火箭的稳定工作有重要意义。 |
