Scientists Probe the Source of Stochastic Occurrence of Super-Knock in Engines Running on Hydrogen/Methane Fuels

Scientists analyzed detonation formation in hydrogen/methane air mixtures, quantifying the effect of non-thermal reactions on the mechanism of detonation.

Image credit: Sandia National Laboratories

The Science

Small-displacement turbocharged internal combustion engines can experience “knock” without suffering lasting damage. Knock happens when the fuel ignites earlier than expected. Much more damaging is “super-knock.” Unlike normal knock, super-knock is caused by a detonation wave due to a feedback loop between the heat release associated with the flame and pressure inside an engine cylinder. One alternative fuel, hydrogen, is at higher risk of super-knock than other fuels because of the ways engines must operate to run efficiently on hydrogen. One solution is fuels made of a mix of hydrogen and methane. Adding methane to hydrogen fuel can smooth combustion and reduce some types of emissions. Combustion in engines is extremely complex, so researchers need to study hydrogen/methane fuel reactions to aid in engine design.

The Impact

Using blends of hydrogen and methane as fuels in internal combustion engines is one of the most promising strategies for reducing carbon dioxide emissions. One concern when burning these fuels in spark-ignited engines is the transition from a “desirable” mechanism of combustion to the formation of a detonation wave. In desirable combustion, the wave of fuel combustion (called deflagration) propagates away from the spark ignition source. Under the wrong conditions, this combustion can instead lead to the formation of a detonation wave. This wave rapidly consumes all the fuel and results in a strong pressure spike called “super-knock” in engines. To avoid “super-knock,” scientists studied the causes of the shift from deflagration-to-detonation. This research will help pave the way to the use of viable alternatives to fossil fuels in internal combustion engines.

Summary

The researchers investigated the impact of non-thermal reaction chemistry on the propagation of combustion fronts for a H₂-CH₄ fuel mixture burning in air within a bounded domain, representing an idealized engine cylinder. Previous work has shown that in some combustion environments, the H + CH₃ and H + OH radical-radical recombination and the H + O₂ radical-molecule association reactions can form long-lived excited-state intermediates (such as CH₄*, H₂O*, HO₂*) that can undergo subsequent reactions with H, O, OH, and O₂ before undergoing collisional stabilization (to CH₄, H₂O, HO₂). The international team led by Sandia National Laboratories included non-thermal ”termolecular” reactions in the model, studying in particular the effects of such radical-radical recombination and radical-molecule association reactions. The team used the S3D direct numerical simulation (DNS) code, with 1 micrometer spatial resolution, showing that inclusion of non-thermalized reaction chemistry influences chemical reaction fluxes during high-pressure H₂-CH₄ combustion and the transition of deflagration fronts to high-pressure, fast-moving detonation fronts.

On the other hand, the inclusion of chemical explosive mode analysis (CEMA), a reliable computational flame diagnostic tool to systematically detect important species and reactions formed during combustion, indicated that, irrespective of the presence of non-thermal reactivity, temperature and oxygen concentration remain the two most dominant variables affecting detonation formation in H₂/CH₄-air mixtures under engine relevant conditions. The researchers note that this particular observation might change with different H₂/CH₄ blending ratios. The researchers’ proposed model appears in the image above. First, a spark-triggered flame propagates outwards at speed ‘S_f’ accompanied by a pressure wave travelling at speed ‘a,’ where a is much larger than S_f (a >> S_f). Without termolecular reactions, the unburned gas near the cylinder wall spontaneously ignites before being consumed by the spark-triggered flame. Subsequently, the emerging ignition front propagates outward with speed ‘SSp’ such that it remains decoupled from the pressure wave (SSp >> a), thereby leading to the formation of normal knock. However, in the presence of termolecular reactions, coalescence between the spark-triggered flame front and the pressure wave occurs with ‘a’ being approximately as large as ‘S_f.’ The perfect synchronization between the pressure wave and the spark-triggered flame front results in the deflagration-to-detonation transition i.e., super-knock without any spontaneous ignition in the unburned end-gas. The researchers propose that their non-thermal reaction chemistry needs to be included when modelling the combustion of H₂-CH₄ mixtures to accurately predict important aspects of flame behavior.

Contact

Jacqueline Chen
Sandia National Laboratories
[email protected]

Funding

The work at Sandia National Laboratories was supported by the Department of Energy (DOE) Office of Science, Basic Energy Sciences, Division of Chemical Sciences, Geosciences, and Biosciences as well as by the Exascale Computing Project, a collaborative effort of the DOE Office of Science and the National Nuclear Security Administration. The work at Argonne National Laboratories was supported by the DOE Office of Science, Office of Basic Energy Sciences, Division of Chemical Sciences, Geosciences, and Biosciences. Two of the researchers were supported as part of the Argonne-Sandia Consortium on High-Pressure Combustion Chemistry. One of the researchers also acknowledges the support from the Natural Science Foundation of Jiangsu Province. The work at the University of Connecticut was supported by the Exascale Computing Project.