内燃机所用的燃料是汽油和空气的混合物。汽油夹着空气，燃烧后产生驱车动力。
It USES a mixture of petrol and air, and this mixture explodes and burns, to produce the energy which propels the car.
这是非常容易引爆的空气和燃料如果是高度压缩之前(或期间)点火过程的混合物。
It is much easier to detonate a mixture of air and fuel if it is highly compressed prior to (or during) the ignition process.
爆燃时会发生什么是刻录在合理的低压力的空气和燃料的混合物。
Deflagration is what happens when you burn a mixture of air and fuel at reasonably low pressure.
本文基于人工神经网络理论及方法，在合理选取影响爆炸威力主要因素的基础上，构建了燃料空气混合物爆炸威力评估模型。
There are many factors affecting explosion power of fuel air mixture, large numbers of them are qualitative and uncertain factors, and the relations between them are very complicated.
当活塞下移时，汽化的燃料和空气的混合物通过进气门进入气缸。
As the piston moves down, the vaporized mixture of fuel and air enters the cylinder through open intake valve.
结果，由节气门(11)控制的混合物包含一部分空气，一部分汽化燃料。
As a result, the mixture controlled by the throttle valve (11) contains partly air and partly vaporised fuel.
气体燃烧器使燃料和夹带的空气完全混合，以便在燃 烧之前形成几乎化学计量的混合物。
The gas burner throughly mixes fuel and entrained air to form a nearly stoichiometric mixture prior to combustion.
燃料-空气混合物的当量比为0.4，燃烧器外壁面与环境采用对流换热边界条件。
Stoichiometric ratio of fuel-air mixture is 0.4. Convection heat exchange has adopted as a boundary condition of external surface.
利用矩形激波管测定了几种碳氢燃料与空气混合物的爆轰极限和临界起爆能。
This paper measured the critical energy and detonation limit of hydrocarbon and air mixtures in the rectangle shock tube.
以燃料和空气混合物为工质的燃烧反应性电弧等离子体在燃烧技术和等离子体技术中都有广泛的应用前景。
Electric arcs in combustible gas mixtures, as a high temperature source in combustion and plasma technology, have a great deal of advantages in comparison with those in noble gases.
如果一个集合点值被超过时，燃料空气混合物进行相应的调整由一个完整的控制器。
If a set point value is exceeded, the fuel-air mixture is adjusted accordingly by an integral controller.
此外，由燃烧驱动激波管产生的高温燃气作为引导火焰点燃激波风洞产生的预混与预热的超声速碳氢燃料——空气混合物。
In addition, a hot, burned gas generated from the shock tube was used as pilot flame for igniting the premixed and preheated supersonic hydrocarbon-air mixture generated in the shock tunnel.
本发明的加热装置(12)包括至少一个用于使得所述待点燃的气态的燃料-空气混合物稳定的机构(17)。
The heating device (12) of the invention comprises at least one organization (17) for stabilizing the to-be ignited gaseous fuel-air mixture.
采用激波风洞-激波管组合设备对预混的碳氢燃料——空气混合物的点火与超声速燃烧进行了研究。
A combination facility, which consists of a shock tunnel and a shock tube, was used for studying ignition and supersonic combustion of premixed hydrocarbon fuel-air mixture.
采用激波风洞-激波管组合设备对预混的碳氢燃料——空气混合物的点火与超声速燃烧进行了研究。
A combination facility, which consists of a shock tunnel and a shock tube, was used for studying ignition and supersonic combustion of premixed hydrocarbon fuel-air mixture.
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