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Vortex Burner—A Useful Tool for Studying the Flame Stability of Gaseous Fuels and Fuel Mixtures

机译:涡流燃烧器—研究气态燃料和燃料混合物的火焰稳定性的有用工具

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摘要

A vortex burner has been developed that permits direct comparison of flame stability of fast‐burning and of slow‐burning gaseous fuels and their mixtures. In this burner, air is introduced tangentially into a chamber to generate a vortex. The vortex is then accelerated by means of a converging nozzle which directs the air into a throat section where fuel is injected radially from ports in the periphery of the throat. The flame is stabilized in space in a divergent, pressure‐recovery section and burns as a whirling inverted cone. Flame stability is independent of tangential velocity at any given air rate. However, changes in other parameters, such as throat diameter and length of the pressure‐recovery section, do have an effect on flame stability. The results of these investigations with the vortex burner suggest that further studies with longer recovery sections are of interest. Likewise, the effect of gas temperature on flame stability will be studied.
机译:已经开发出一种涡流燃烧器,可以直接比较快速燃烧和缓慢燃烧的气态燃料及其混合物的火焰稳定性。在该燃烧器中,空气被切向引入腔室以产生涡流。然后通过一个会聚喷嘴将涡流加速,该喷嘴将空气引导到喉部,在该处从喉部周边的端口向径向注入燃料。火焰在发散的压力恢复区中稳定在空间中,并以旋转的倒锥燃烧。在任何给定的空气速率下,火焰稳定性与切向速度无关。但是,其他参数的变化(例如,喉管直径和压力恢复段的长度)确实会影响火焰稳定性。用涡流燃烧器进行的这些研究的结果表明,对具有更长回收段的进一步研究是有意义的。同样,将研究气体温度对火焰稳定性的影响。

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