Effect of hardware geometry on gas and drop behavior in a radial mixer spray

A. Ateshkadi, V.G. McDonell, G.S. Samuelsen
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引用次数: 25

Abstract

The demands on current and future aero gas turbine combustors are requiring a greater insight into the role of the injector/done design and manufacturing tolerances. This paper systematically isolates manufacturing tolerances and focuses on hardware design. The target is the structure of the two-phase flow and combustion performance associated with practical injector/dome hardware. A spray injector with two radial inflow swirlers was custom designed to (1) maintain tight tolerances and strict assembly protocol and (2) thereby isolate the sensitivity of performance to hardware design. Although it represents practical hardware, the custom set is a unique modular design that (1) accommodates parametric variation in geometry, (2) retains symmetry, and (3) maintains effective area. Swirl sense and the presence of a venturi were found to be the most influential. The venturi acts as a fuel prefilming surface and constrains the highest fuel mass concentration to an annular ring near the centerline. Coswirl enhances the radial dispersion of the continuous phase, and counterswirl increases the level of mixing that occurs in the downstream region of the mixer. The combined effect of the two parameters (swirl sense and venturi) revealed that the largest drop sizes, which penetrate the continuous phase flow, are formed with coswirl and without venturi. The smallest drop size distributions were found to occur for the counterswirl configuration with venturi. In the case of counterswirl without venturi, the high concentration of fluid mass is found in the center region of the flow. The lean blowout (LBO) equivalence ratio was lower for counterswirl configurations for reasons that involved the coupling of the centerline recirculation zone with the location of high fuel concentration emanating from smaller droplets. In the coswirl configuration, a lack of fuel drops exists in the reaction anchoring region, thereby leading to poor stability characteristics.

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硬件几何形状对径向混合器喷雾中气滴行为的影响
当前和未来对航空燃气轮机燃烧器的需求需要更深入地了解喷油器/已完成设计和制造公差的作用。本文系统地分离了制造公差,重点研究了硬件设计。目标是两相流结构和与实际喷油器/穹窿硬件相关的燃烧性能。带有两个径向流入旋流器的喷射器的定制设计(1)保持严格的公差和严格的装配协议,(2)从而隔离性能对硬件设计的敏感性。虽然它代表了实用的硬件,但定制集是一种独特的模块化设计,可以(1)适应几何参数变化,(2)保持对称性,(3)保持有效面积。旋感和文丘里腔的存在被发现是最具影响力的。文丘里管充当燃料预膜表面,并将最高燃料质量浓度限制在靠近中心线的环形环上。共旋增强了连续相的径向分散,而反旋增加了混合器下游区域的混合水平。两个参数(旋流感和文丘里)的综合作用表明,在有共旋流和文丘里流的情况下,穿透连续相流的液滴尺寸最大。在文丘里管的反旋结构中,液滴尺寸分布最小。在没有文丘里腔的反旋情况下,流体质量的高浓度出现在流动的中心区域。由于中心线再循环区与由小液滴产生的高燃料浓度位置的耦合,反旋结构的稀爆等效比较低。在共旋构型中,反应锚固区缺少燃料滴,稳定性特性较差。
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