燃气轮机模型燃烧室湍流流场测量

Daniele Contini, Marco Ruggiero, Giampaolo Manfrida
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引用次数: 1

摘要

本文介绍了燃气轮机燃烧室缩尺(1∶3)模型中反应流动的研究结果。在常压下对贫预混料燃烧室模型进行了试验;采用双通道光纤激光多普勒风速仪在气流上播种Al2O3,对反应流进行了测量。测量覆盖了轴对称燃烧室的广泛区域,在不同的播种条件和数据速率下,包括火焰发展和再循环区域。本文详细分析了流速的波动分量;平均流动特性是一个先决条件。报道和讨论了湍流的频域和时域特征,包括功率密度谱、自相关系数和时间积分尺度,并尝试对反应湍流流场进行物理描述。
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Turbulent flow field measurements in a model gas turbine combustion chamber

The results of the investigation of the reactive flow in a scaled-down (≅1:3) model of a gas turbine combustion chamber are presented. The lean-premix combustion chamber model was tested at atmospheric pressure; measurements in the reactive flow were taken by using a two-channel fibre-optic laser Doppler anemometer with Al2O3 seeding on the air flow. Measurements cover a wide region of the axial-symmetric combustion chamber at points characterised by different seeding conditions and data rates, including the flame development and recirculating zones. This work presents a detailed analysis of the fluctuating components of flow velocity; mean flow properties are presented as a prerequisite. Frequency and time domain characteristics of turbulence including power density spectra, autocorrelation coefficients and time integral scales are reported and discussed, and a physical description of the reacting turbulent flow field is attempted.

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