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Experimental assessment of the lean blow-off in a fully premixed annular combustor

机译:完全预混的环形燃烧器中贫吹灰的实验评估

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摘要

The behaviour of the flame in an annular combustor with multiple bluff-body injectors with swirl was investigated to provide insights into lean blow-off (LBO) mechanisms when flames interact. Two different configurations, with 12 and 18 burners, and various bulk velocities and equivalence ratios were tested. Flame shape and main features were studied by means of 5 kHz OH* chemiluminescence imaging and the stability limits were identified and compiled into stability regime diagrams. As the equivalence ratio of the mixture was reduced the individual flames would first exhibit a transition from a stable "W-shape" state to a stable "V-shape" state before becoming unstable close to extinction. In the 18-burner configuration LBO was characterised by random detachment and re-stabilisation of the flames over multiple burners across the chamber, until complete lift-off. In the 12-burner configuration the flame anchors on a few burners in azimuthally symmetric locations, making the overall flame less prone to global extinction. Finally, the stability curves were computed using a correlation based on the Damkholer (Da) number and compared to single burner configurations. The beginning of the blowoff transient was found to be similar to the LBO condition for a single burner in the 12-burner setup, while the 18-burner configuration was less stable for all the conditions investigated. However, it was found that correlations based on single burner extinction data do not fully work for the extinction of interacting flames. The results provide insights into the blow-off of realistic gas turbine engines and can be used for validating models of such processes.
机译:研究了具有多个凹槽式喷射器的环形燃烧器中的火焰的行为被研究,以在火焰相互作用时向贫吹除(LBO)机制中的见解。测试了两种不同的配置,有12和18燃烧器,以及各种散装速度和等效比率。通过5 kHz OH *化学发光成像研究了火焰形状和主要特征,并识别稳定性限制并编制到稳定性方案图中。随着混合物的等同比减少,各个火焰首先将从稳定的“W形”状态的过渡表现为稳定的“V形”状态,然后在不稳定靠近灭火之前。在18燃烧器配置中,LBO的特征在于随机分离,并在腔室穿过多个燃烧器上重新稳定火焰,直到完全剥离。在12燃烧器配置中,火焰锚在四方称对称位置的几个燃烧器上,使整体火焰不容易产生全局灭绝。最后,使用基于DAMKHOLER(DA)编号的相关性来计算稳定性曲线,并与单刻器配置相比。发现吹气瞬态的开始与12燃烧器设置中的单个燃烧器的LBO条​​件类似,而在调查的所有条件下,18刻器配置较小。然而,发现基于单燃烧器灭绝数据的相关性不会完全用于突出互动火焰的灭绝。结果提供了进入现实燃气轮机发动机的吹气的见解,并且可用于验证这些过程的模型。

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