富燃料

含硼HTPB富燃料推进剂工艺恶化机理研究

Mechanism of the deteriorated processability in boron - fuel - rich HTPB propellants

燃料云雾的临界起爆能和爆轰胞格尺寸均与当量比成一U形曲线关系，并且云雾爆轰最敏感点并不是对应于等化学当量的混合物而是偏向于富燃料；

Results demonstrate that the relationship of critical initiation energy and equivalence ratio shows an " U " shape curve , the cell size is also .

采用微测温和火焰照相及SEM研究了含硼富燃料推进剂燃烧波温度分布、火焰结构及熄火表面；

The combustion wave temperature profiles , the flame structure and extinguished surface of boron-based fuel-rich propel-lant are investigated by means of temperature measuring , flame photograph and SEM .

Fenton试剂法处理有机废水的技术进展富燃料推进剂的燃烧成气率测试研究

The Study of Fenton Reagent Degradation Organic Waste-water Investigation on measuring gas generation rate for fuel-rich propellant during combustion process

热力学平衡以及均相动力学计算结果表明富氧贫燃料条件下CO2浓度的变化对烟气中硫的组分和浓度几乎无影响，富燃料条件下CO2的存在于一定程度上促进了SO2的析出。

The results of thermal-equilibrium method and homogeneous kinetic indicate that under oxygen-rich conditions , the change of CO2 concentration has no impact on sulfur concentration and composition in smoke .

用最小自由能法计算了镁铝富燃料推进剂一次燃烧室产物的成分，分析了凝聚相C、Mg和Al产物含量的变化对燃烧残渣的影响；

The product compositions of magnesium-aluminum fuel-rich propellant in primary chamber were calculated by using minimum free energy method . The effects of condensed phase product content including carbon , magnesium and aluminum on combustion residue were analyzed .

实验结果表明：含硼富燃料推进剂各组分含量相同时，在硼粒子表面包覆AP提高了推进剂的爆热，其中凝相放热量增加，气相放热量减少；

The results showed : When the propellants ' formations are the same , coating boron with AP can increase the explosive heat . Condensed-phase releasing heat is increased and gas-phase releasing heat is decreased .

结果表明，多孔介质内的富燃料燃烧同样可以实现超绝热火焰温度，燃烧产物中H2含量很高，验证了富燃制氢的可行性。

It was concluded that , rich combustion in porous media can also achieve superadiabatic temperature . H2 product is quite rich after combustion , so rich combustion can be used to hydrogen production .

AP/KP/GAP富燃料推进剂的热分解特性

Thermal decomposition characteristics of AP / KP / GAP fuel-rich propellant

提高含硼富燃料推进剂能量的技术途径

Technical Approaches of Enhancing the Energy of Boron Based Fuel-rich Propellant

初步确定了该类推进剂的燃烧过程，为建立含硼富燃料推进剂燃烧物理模型提供了依据。

Meanwhile , the combustion course of the propellant was confirmed preliminary .

团聚硼对富燃料推进剂燃速的影响

The Influence of Agglomerated Boron on Burning Rate of Fuel-rich Solid Propellant

低压下镁铝富燃料固体推进剂燃烧性能研究

Study on combustion properties of magnesium-aluminized fuel-rich solid propellants under low pressure

含硼富燃料推进剂配方初步优化

Preliminary Optimization Formulation of Fuel - rich Solid Propellant Based on Boron

氟化物对Mg/NaNO3富燃料推进剂燃烧性能的影响

Influence of Fluorides on Combustion Characteristics of Mg / NaNO_3 Fuel-rich Propellants

含硼富燃料推进剂燃烧表面沉积层研究

Study on burning surface sedimentary deposit of boron-based fuel-rich propellant

富燃料推进剂的燃烧成气率测试研究

Investigation on measuring gas generation rate for fuel-rich propellant during combustion process

氟橡胶/镁/硝酸钠富燃料体系的热分析

Thermal Analysis of Viton A / Mg / NaNO_3 Fuel Rich System

包覆及团聚硼对富燃料推进剂燃烧性能的影响

Effect of coated and agglomerated boron on combustion characteristics of boron-based fuel-rich propellants

镁铝富燃料推进剂燃烧残渣影响因素理论分析

Theoretical analysis on combustion residue of magnesium - aluminum fuel - rich propellant

含硼富燃料推进剂各组分对其低压燃速的影响

Effect of Components of Fuel-rich Boron-based Solid Propellant on the Burning Rate in Low Pressure

硼粒子表面包覆对富燃料推进剂热分解特性的影响

The Effects of Boron Particle Surface Coating on the Thermal Decomposition of Fuel rich Propellant

镁铝富燃料推进剂热值的均匀性和稳定性及不确定度分析

Uniformity and Stability of Combustion Heat and Its Uncertainty Analyses for Mg / Al Fuel-rich Propellant

贫燃料与富燃料爆炸气体中，由管道底部向上，其电导性是逐渐增大的。

But in the fuel lean and fuel rich explosive gas , the electrical conductivity increases gradually from bottom to top .

气浮台冷气推力测试装置的系统设计富燃料推进剂的燃烧成气率测试研究

Design and Test Studies on Cold Gas Propulsion System of Five Degrees of Freedom Air-bearing Test-bed Investigation on measuring gas generation rate for fuel-rich propellant during combustion process

在小型流动反应器中研究了不同煤粉及其煤焦对富燃料再燃区NO异相还原的影响。

The effect of different pulverized coals and chars on NO heterogeneous reduction in the fuel rich stage of reburning was studied in a bench scale flow reactor .

通过燃气发生器法测试含硼富燃料推进剂一次燃烧喷射效率，分析推进剂组分和喷射装置对一次燃烧喷射效率的影响。

Influences of composition of propellant and ejection device on ejection efficiency of primary combustion of boron-based fuel-rich propellant were studied by measuring the ejection efficiency in a gas generator .

采用推进剂静态燃速测试仪和氧弹式量热器的试验方法，研究了各组分对含硼富燃料推进剂低压燃速和爆热的影响。

Effects of components of fuel-rich boron-based solid propellant on burning rate in low pressure and explosive heat were investigated by measuring its burning rate with standard burner method and explosive heat with calorie meter of oxygen bomb .

火旋风火焰体内富燃料核对连续火焰区的径向温度分布有重要影响，且火焰体可用圆柱与圆锥的结合体描述。

The fuel-rich core in the flame body of fire whirl significantly affects the radial temperature distribution in the continuous flame region , and the flame body can be described by the combination of a cylinder and a cone .

膏体富燃料推进剂一次燃烧处于非平衡条件下，本文建立了非平衡条件下热力计算的理论模型以及不同热力学状态下求解平衡组分和燃烧温度的控制方程组。

The primary combustion of fuel-rich pasty propellant is under the chemical non-equilibrium condition . This paper presents the theoretical model of thermodynamic calculation under the chemical non-equilibrium condition and equations solving equilibrium compositions and temperature in the different thermodynamic states .