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Combustion Instability Phenomena Observed During Cryogenic Hydrogen Injection Temperature Ramping Tests for Single Coaxial Injector Elements

机译:单同轴喷射器元件的低温氢注入温度斜坡测试期间观察到的燃烧不稳定性现象

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For LOX/LH_2 shear coaxial injectors, it is well-known that high-frequency combustion instabilities may occur when the injection temperature of hydrogen decreases below a certain value, but the mechanism of the initiation of combustion instability with a coaxial injector is still not clear. In the present study, firing tests were conducted with five types of single shear coaxial injector elements by using LOX and LH2 as propellants to further investigate the mechanism of the initiation of combustion instability during temperature-ramping changes during hydrogen injection. Results showed that unstable combustion was initiated when the hydrogen injection temperature decreased to less than a certain cryogenic temperature. The combustion instabilities observed in the present firing tests are discussed and classified into three different types.
机译:众所周知,对于LOX / LH_2剪切同轴喷射器,当氢的喷射温度降低到一定值以下时,可能会发生高频燃烧不稳定性,但是利用同轴喷射器引发燃烧不稳定性的机制仍不清楚。在本研究中,通过使用LOX和LH2作为推进剂,对五种类型的单剪切同轴喷射器元件进行了点火测试,以进一步研究氢注入过程中温度梯度变化时燃烧不稳定性引发的机理。结果表明,当氢气注入温度降低到低于某个低温温度时,就会引发不稳定的燃烧。讨论了在当前燃烧测试中观察到的燃烧不稳定性,并将其分为三种不同类型。

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