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arXiv 2604.08035physics.flu-dyn

圆环腔体稳定旋转火焰在圆形海勒-沙瓦燃烧器中的研究

Cavity-Stabilized Rotating Flames in a Circular Hele-Shaw Burner

SKLTCS, CAPT, School of Mechanics and Engineering Science, Peking University(北京大学力学与工程科学学院)

Xiangyu Nie, Shengkai Wang

AI总结:

研究通过实验观察了在圆形海勒-沙瓦燃烧器中稳定的旋转火焰,揭示了低流速下火焰自组织现象及燃烧模式转变机制,为微通道燃烧器设计提供理论支持。

摘要:

我们报告了在配备环形腔体火焰持火器的开放圆形海勒-沙瓦燃烧器中,甲烷和空气预混火焰的直接实验观测。这些火焰在足够低的流速下自发形成,其中火焰回火被热淬灭所抵消,导致局部火焰速度与流速之间的动态平衡。与在封闭微通道中传播的火焰不同,这些火焰表现出稳定的行波模式,其头部沿腔体前缘滑动,快速膨胀形成低速区,从而促进火焰稳定。在低流速下,旋转火焰为单头,其旋转频率大致与层流火焰速度成正比,表明火焰前沿以近似恒定形状的方式传播。随着流速增加,旋转火焰分裂为多个等间距头部,头部数量和旋转频率随流速增加而增加,直至这些旋转火焰转变为稳定环形火焰,其锚定在腔体前缘。在足够高的流速下,火焰前沿被推离腔体后侧,导致熄灭。参数测量覆盖了广泛的等效比和流速范围,从而获得了不同火焰模式及其转变边界的大致图谱。此外,还进行了丙烷和二甲醚的额外实验。发现旋转-稳定火焰转变边界的关键总质量流率对等效比、间隙距离和燃料类型不敏感。这些结果不仅对理解微通道中火焰动力学的基础理论有帮助,也对微燃烧器的实际设计和微燃烧技术的应用有实用价值。

英文摘要:

We report direct experimental observations of self-organized rotating flames of premixed CH4 and air in an open circular Hele-Shaw burner equipped with an annulus cavity flame holder. These flames formed spontaneously at sufficiently low flow rates, where flame flashback was counteracted by thermal quenching, resulting in a dynamic balance between the local flame speed and flow velocity. Unlike flames propagating in closed micro-channels, these flames exhibited stable traveling-wave patterns with heads gliding along the leading edge of the cavity, where rapid expansion created a low-speed zone that facilitated flame stabilization. At low flow rates, the rotating flames were single-headed, with their rotation frequencies roughly proportional to the laminar flame speeds, suggesting that the flame fronts traveled in a nearly constant-shape fashion. As the flow rate increased, the rotating flames split into multiple heads at approximately equal spacing, and the number of heads and rotation frequency increased with the flow rate, until these rotating flames transitioned into steady ring-shaped flames anchored at the cavity leading edge. Blow-off or extinction occurred at sufficiently high flow rates, where the flame front was pushed out of the rear side of the cavity. Parametric measurements were conducted over a wide range of equivalence ratios and flow rates, from which a regime diagram of different flame modes and their transition boundaries was obtained. Additional experiments were conducted on C3H8 and DME. It was found that the critical total mass flow rate at the rotating-steady flame transition boundary is insensitive to equivalence ratio, gap distance, and fuel type. These results should be useful not only for the fundamental understanding of flame dynamics in micro-channels but also for the practical design of micro-combustors and the application of micro-combustion technologies.

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