首页> 外文会议>ASME(American Society of Mechanical Engineers) Turbo Expo vol.1; 20060506-11; Barcelona(ES) >PERFORMANCE OF PREFILMING AIRBLAST ATOMIZERS IN UNSTEADY FLOW CONDITIONS
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PERFORMANCE OF PREFILMING AIRBLAST ATOMIZERS IN UNSTEADY FLOW CONDITIONS

机译:非定常流动条件下预吹塑空气雾化器的性能

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Within the context of lean premixed prevaporized combustion (LPP) which is considered as most promising technology for the next generation of low emission combustors for aero engines, combustion instabilities are a major issue. These combustion instabilities may compromise the pollutant emissions and even cause damage to the combustion chamber structure. In the literature, numerous phenomenological studies on combustion oscillation are available, but a comprehensive theory is still missing. One potential excitation mechanism is the interaction of strong air velocity fluctuations and pressure oscillations with the airblast atomizer leading to temporal fluctuations of the spray characteristics. This phenomenon was investigated experimentally at the Institute of Thermal Turbomachinery (ITS) within a parametric study. A duct with a prefilming surface was set up as an abstraction of a prefilming airblast atomizer. A mean air velocity up to 65 m/s can be reached, and periodic oscillations can be superimposed by means of a siren with a frequency up to 570 Hz. The disintegration process of the liquid fuel was studied downstream the atomizing edge of a plain airblast nozzle. Several optical diagnostics like phase resolved LDV (Laser Doppler Velocimetry) and an improved PTV technique (Particle Tracking Velocimetry) were used. The mean air velocity, the film load, the kinematic viscosity and the surface tension of the fluid as well as the pulsation frequency and amplitude of the siren were varied, and their effect on the temporal evolution of the droplet size and droplet rate was studied. It was found that the amplitude of fluctuations of the droplet size and the droplet rate is almost proportional to the air velocity fluctuations at low frequencies. At higher frequencies, however, both are nearly unaffected. In addition, the fluctuations of droplet diameter and rate increase strongly if the mean air velocity is increased. The phase shift between particle diameter, particle rate and air velocity fluctuations was found to increase at higher excitation frequencies.
机译:在被认为是下一代航空发动机低排放燃烧器最有希望的技术的稀薄预混预蒸发燃烧(LPP)的背景下,燃烧不稳定性是一个主要问题。这些燃烧不稳定性可能会损害污染物排放,甚至会损坏燃烧室结构。在文献中,关于燃烧振荡的许多现象学研究是可用的,但是仍然缺少综合理论。一种潜在的激励机制是强空气速度波动和压力振荡与鼓风雾化器的相互作用,从而导致喷雾特性随时间波动。此现象已在热力涡轮机械研究所(ITS)的参数研究中进行了实验研究。建立了具有预成膜表面的管道,作为预成膜鼓风雾化器的抽象形式。可以达到最高65 m / s的平均风速,并且可以通过频率高达570 Hz的警报器叠加周期性的振荡。研究了普通喷气喷嘴雾化边缘下游液体燃料的分解过程。使用了几种光学诊断技术,例如相位分辨LDV(激光多普勒测速仪)和改进的PTV技术(粒子跟踪测速仪)。改变了平均风速,薄膜载荷,流体的运动粘度和表面张力以及警报器的脉动频率和幅度,并研究了它们对液滴尺寸和液滴速率随时间变化的影响。已经发现,液滴尺寸和液滴速率的波动幅度几乎与低频处的空气速度波动成比例。但是,在较高的频率下,两者几乎都不受影响。另外,如果平均风速增加,则液滴直径和速率的波动会大大增加。发现在较高的激发频率下,粒径,粒径和空气流速波动之间的相移会增加。

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