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Feasibility of 'intermittent' active control of combustion instabilities in liquid fueled combustors using a 'smart' fuel injector

机译:使用“智能”燃料喷射器的“间歇”主动控制液体燃料燃烧器中的燃烧型燃烧装置的可行性

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This paper describes an experimental investigation of the feasibility of an "intermittent" active control approach for suppressing combustion instabilities in liquid fueled combustors. The developed controller employs a "smart" fuel injector that can modify the spray properties in response to changes in combustor operating conditions. This action weakens or breaks up the coupling between the combustion process and combustor acoustic modes oscillations, thus preventing the excitation of large amplitude instabilities. This approach differs significantly from previously proposed active control methods, both in concept and implementation, as it requires only "intermittent" modification of the combustion process by a single control action as opposed to the continuous action required by most other active control methods. The "smart" fuel injector used in this study consisted of a double-staged, air-assisted atomizer in which counter swirling, primary (inner stage) and secondary (outer stage) air streams were supplied to the injector through separate sets of tangentially oriented orifices. Control of the ratio of air mass flow rates supplied to these two stages, by use of a diverter valve, resulted in significant changes in the spray shape and its axial, tangential, and radial velocity components. This variation in spray properties of the "smart" injector was characterized for different values of the inner to outer air flow rate ratio in cold flow tests with a PDPA system. These results were then correlated with the characteristics of the "intermittently" controlled combustor. Measured quantities included the instability amplitudes, axial dependence of the mean and oscillatory heat release amplitudes, and the characteristics of the recirculation zones, which were all shown to depend on the fuel spray properties. The results of this study demonstrate the feasibility of using "smart" fuel injectors with capabilities for varying the combustion process characteristics to reduce the amplitudes of detrimental combustion instabilities in real engines to acceptable levels.
机译:本文介绍了抑制液体燃料燃烧器中抑制燃烧燃烧能力的“间歇性”主动控制方法的可行性的实验研究。开发控制器采用“智能”燃料喷射器,其可以响应于燃烧器操作条件的变化而改变喷射性能。该动作削弱或破坏燃烧过程与燃烧器声学模式振荡之间的耦合,从而防止激发大的幅度不稳定性。这种方法与先前提出的主动控制方法有显着不同,无论是在概念和实现中,因为它只需要通过单个控制动作的“间歇”修改燃烧过程,而不是大多数其他主动控制方法所需的连续动作。本研究中使用的“智能”燃料喷射器由双分阶段的空气辅助雾化器组成,其中通过单独的切向定向器将计数器旋转,初级(内级)和次级(外级)空气流供应到注射器中孔。通过使用转向阀,控制提供给这两个阶段的空气质量流量比率,导致喷雾形状和轴向,切向和径向速度分量的显着变化。 “智能”喷射器的喷射特性的这种变化特征在于具有PDPA系统的冷流检测中的内部空气流量比的不同值。然后将这些结果与“间歇”控制燃烧器的特性相关。测量量包括不稳定性幅度,平均和振荡释放幅度的轴向依赖性,以及再循环区域的特性,所有这些都被证明取决于燃料喷雾性能。本研究的结果表明使用“智能”燃料喷射器具有功能,以改变燃烧过程特性,以减少真正的发动机中有害燃烧稳定性的幅度。

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