Investigation of Non-Premixed Hydrogen-Oxygen Impinged Jet Flame Under Steam Dilution

Yongtao Fan, Taku Tsujimura, N. Iki, O. Kurata, H. Furutani
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Abstract

Large-scale electric power generation with hydrogen-fired gas turbines is key to the realization of zero-emission society. One challenge of premixed hydrogen combustion is the flashback associated with high burning velocity. On the other hand, non-premixed (diffusion) hydrogen-air combustion produces high level of NOx due to the high flame temperature. In order to reduce NOx, a semi-closed gas turbine cycles employing the hydrogen-oxygen combustion has been proposed. In the present study, we developed a non-premixed hydrogen-oxygen burner with sub-millimeter nozzles to form two oxygen jets impinging on the hydrogen jet at an acute angle. Compared to conventional burners with co-flow jets, forced mixing of hydrogen and oxygen occurs due to the impingement. It is expected that the flame holding as well as the combustion efficiency can be improved. High-speed Schlieren and OH* chemiluminescence images of the hydrogen flame with/without the oxygen jet impingement in a pressure vessel were captured to examine the instantaneous flame structure. Flammability and flame structure have been investigated at various jet velocity and pressure conditions. It was found that without the oxygen jet impingement the flame becomes longer with increasing the hydrogen velocity. Lifted flames were observed at the velocity over 200 m/s. The lift position moves gradually downstream with further increasing the velocity. On the other hand, with increasing the velocity of the oxygen jet impinged to the hydrogen jet, a V-shaped flame front stabilized at the impinging position was observed. It was also found that flame holding is improved at high pressure. Based on the impinged jet flame concept, prototype multi-cluster burners with sub-millimeter nozzle arrays were designed and fabricated using the Inconel alloy 3D printing technology.
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蒸汽稀释作用下非预混氢氧碰撞射流火焰的研究
氢能燃气轮机大规模发电是实现零排放社会的关键。预混氢燃烧的一个挑战是高燃烧速度带来的闪回现象。另一方面,由于火焰温度高,非预混(扩散)氢-空气燃烧产生高水平的NOx。为了减少NOx的排放,提出了一种采用氢氧燃烧的半封闭式燃气轮机循环。在本研究中,我们开发了一种非预混氢氧燃烧器,采用亚毫米喷嘴,形成两个氧射流以锐角撞击氢射流。与传统的共流射流燃烧器相比,由于撞击,氢和氧会发生强制混合。预期可以提高火焰的保持度和燃烧效率。利用高速纹影和OH*化学发光图像对压力容器中有/无氧射流撞击的氢火焰进行了分析。研究了在不同喷射速度和压力条件下的可燃性和火焰结构。结果表明,在没有氧气射流冲击的情况下,火焰随着氢气速度的增加而变长。在超过200米/秒的速度下观察到升起的火焰。随着速度的进一步增大,升力位置逐渐向下游移动。另一方面,随着氧射流撞击氢射流速度的增加,在撞击位置观察到一个稳定的v型火焰锋。同时还发现,高压下的保焰性能得到了改善。基于撞击式射流火焰的概念,采用英科乃尔合金3D打印技术,设计并制造了亚毫米喷嘴阵列的多簇燃烧器原型。
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