部分裂解氨火焰放大的旋流数及喷嘴设计试验分析

IF 5 Q2 ENERGY & FUELS
Jordan Davies , Daisuke Sato , Syed Mashruk , Agustin Valera-Medina
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引用次数: 0

摘要

由于其易于储存和现有的全球分销网络,对使用可再生生产的氨用于脱碳能源系统的兴趣正在增长。部分裂解氨可以克服这种燃料的火焰稳定性挑战,但具有可接受排放的大功率氨基漩涡火焰的演示尚未实现。因此,本研究考察了不同的旋流数和喷嘴设计对20%(体积)裂纹氨旋流火焰的静态稳定性和排放的影响,其等效比范围很广(0.3 <;Φ& lt;2.2)和热功率分别为5,10和15kw。此外,在化学计量条件下测试了100 kW热电的参考案例。虽然火焰的形态变化很大,但稳定的火焰显示在广泛的等效比,涡流数和喷嘴几何形状范围内。值得注意的是,1.75的几何旋流数与长喷嘴配对,使其能够在0.6和0.7的等效比下过渡到平坦的康达射流火焰。当几何旋流数为1.45时,缩短喷嘴会产生更短、更宽的v形火焰,并大大提高了丰富的排气极限。这被发现是一个理想的特性,以达到高热功率与恒定的喷嘴喉道直径-即倾倒平面速度-作为一个扩大的火焰刷防止射流状火焰,这是容易被掐掉。这也可以通过增加旋涡数来实现,尽管在较小程度上。然而,在加宽火焰刷时,必须仔细考虑约束直径,以避免火焰撞击,这可能会增加局部热损失,从而降低燃烧效率,导致未燃烧的NH3排放量增加。在相同几何旋流数为1.45的情况下,较短的喷嘴结构导致更高的NO排放,这可能是由于较短的喷嘴形成的火焰更短、更宽,这意味着NH2在火焰区域消耗NO的停留时间更短。在丰富的条件下,这种差异不太明显,所有配置的NO排放量都达到可忽略不计Φ = 1.15
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Experimental analysis of swirl number and nozzle design for scale-up of partially cracked ammonia flames
Due to its ease of storage and existing global distribution network, interest in the use of renewably produced ammonia for decarbonising energy systems is growing. Partially cracking ammonia can overcome the flame stability challenges of this fuel, but demonstrations of high-power ammonia-based swirl flames with acceptable emissions have yet to be realised. Therefore, the present study examines the effects of varying swirl number and nozzle design on the static stability and emissions from 20 % (vol.) cracked ammonia swirl flames for a wide range of equivalence ratios (0.3 < Φ < 2.2) and thermal powers of 5, 10 and 15 kW. Additionally, a reference case of 100 kW thermal power at stoichiometric conditions was tested. Stable flames were shown across a broad range of equivalence ratios, swirl numbers and nozzle geometries although flame morphologies varied greatly. Of note was a geometric swirl number of 1.75 paired with a long nozzle, which enabled the transition to a flat, Coanda jet flow flame at equivalence ratios of 0.6 and 0.7. For a geometric swirl number of 1.45, shortening the nozzle resulted in significantly shorter, wider V-shape flames with greatly improved rich blowoff limits. This was found to be a desirable characteristic for reaching high thermal power with a constant nozzle throat diameter – i.e. dump plane velocity – as a widened flame brush prevents jet-like flames, which are susceptible to pinching off. This can also be achieved by increasing the swirl number, although to a lesser extent. However, with a widened flame brush, careful consideration must be given to confinement diameter to avoid flame impingement which has potential to increase local heat loss and hence reduce combustion efficiency, resulting in an increase in unburned NH3 emissions. With the same geometric swirl number of 1.45, the shorter nozzle configuration resulted in higher NO emissions, potentially due to the shorter nozzle forming shorter, wider flames, meaning there was less residence time for NH2 to consume NO in the flame zone. This difference was less noticeable at rich conditions, with all configurations reaching negligible NO emissions by Φ = 1.15
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