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Hot Surface Ignition Temperatures of Hydrocarbon Fuels

机译:碳氢燃料的热表面着火温度

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Hot surface ignition temperatures are measured for n-heptane, turbine engine based fuels namely Jet-A, JP-8, JP-5 and piston-engine based fuel 100 low lead aviation gasoline (Avgas) using a newly developed apparatus. Hot surface ignition is defined as the process of a flammable liquid coming in contact with a hot surface and evaporating, mixing and reacting with the surrounding oxidizer with self-supporting an exothermic heat release process (combustion). If all the conditions are adequate, the fuel completely turns into the combustion products following the ignition process. The ignition and combustion processes depend on vaporization rate, heat of vaporization, mixing rate with the oxidizer, a critical balance between the energy release during the initiation reactions and the rate of heat transfer to the surrounding mixture and the boundaries. Under most practical circumstances, the ignition process is probabilistic because of small variations in key parameters. One of the most important parameters determining die probability of successful ignition is the temperature of the hot surface. A test apparatus is established to reproducibly observe the hot surface ignition process by dispensing ~25 µL drops of fuel on an electrically heated surface with a temperatu re uniformity within ±5°C. Ignition and flame propagation events are recorded using regular and high speed visible cameras. The ignition event is transient and initiates at randomly distributed locations on the hot surface. Initial tests confirmed that the experimental variations in the drop size, drop velocity, plume characteristics, surface properties including temperature changes, and the nonlinear dependence of temperature of the initial reaction rate lead to the probabilistic nature of the ignition event Ignition probability is defined as a ratio of the number of ignitions and the number of dispensed drops, 20 drops are dispensed at each defined hot surface temperature for each fuel. The number of ignitions is counted by visual observation of a luminous flame. Curve fits are plotted in which the probabilities of ignition are graphed as a function of the hot surface temperature using Logistic functions whose two parameters are evaluated using the lowest maximum and the highest minimum temperatures for ignition.
机译:使用新开发的设备测量正庚烷,涡轮发动机基燃料(即Jet-A,JP-8,JP-5和活塞发动机基燃料100低铅航空汽油)的热表面着火温度。热表面着火是指易燃液体与热表面接触并与周围的氧化剂蒸发,混合并起反应并自支撑放热过程(燃烧)的过程。如果所有条件都满足,则在点火过程之后,燃料会完全变成燃烧产物。点火和燃烧过程取决于汽化速率,汽化热,与氧化剂的混合速率,引发反应过程中释放的能量与向周围混合物和边界的热传递速率之间的关键平衡。在大多数实际情况下,由于关键参数的微小变化,点火过程是概率性的。决定成功点火可能性的最重要参数之一是热表面的温度。建立了一种测试设备,可通过在电加热的表面上分配温度均匀性在±5°C之内的〜25 µL燃料滴来可重复地观察热表面着火过程。使用常规和高速可见摄像机记录点火和火焰传播事件。点火事件是短暂的,并在热表面上随机分布的位置开始。初始测试证实了液滴尺寸,液滴速度,羽流特性,包括温度变化在内的表面特性以及初始反应速率的温度与温度的非线性相关性导致点火事件概率性质的实验变化点火概率定义为点火次数与分配的液滴数之比为20,则在每种定义的热表面温度下为每种燃料分配20滴。通过目视观察发光火焰来计数点火次数。绘制了曲线拟合,其中使用Logistic函数绘制了点火概率与灼热表面温度的函数关系图,该函数的两个参数使用点火的最低最高温度和最高最低温度进行评估。

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