1. Introduction: A New Concept of Hydrogen Combustion
For many years, research on internal combustion (IC) engines has been aimed at reducing their harmfulness to the natural environment [
1]. In many countries, scientists are conducting research to check the emission of conventional fuels in typical or less typical applications of self-ignition (SI) and compression ignition (CI) engines [
2,
3]. However, it seems that the greatest interest in recent years has been the research on modern alternative fuels such as, e.g., alcohols [
4,
5,
6]. Within the group of alternative fuels, hydrogen is probably the most popular and forward-looking fuel. Considering the use of hydrogen in conventional internal combustion engines, it can be noticed that most of the work focuses on hydrogen use in spark-ignition engines. Much less work is devoted to compression-ignition engines, especially considering that hydrogen may not be the main volumetric share in the fuel but only an addition to conventional fuel. The addition of hydrogen to diesel fuel, often referred to as “mixing hydrogen with diesel” or “hydrogen enrichment”, has become of interest due to its potential to improve combustion properties and reduce emissions [
7,
8]. Hydrogen is considered to be a clean fuel and, when mixed with diesel fuel, it can affect various engine performance parameters. Here is the potential impact on engine parameters (
Figure 1).
Research on the addition of hydrogen to liquid hydrocarbon fuels has been ongoing since the 1990s, especially in the case of supersonic combustion. The work of Gruenig et al. [
9] shows that the high temperature of the burner entrance allows the stabilization of the supersonic flame through self-ignition of hydrogen. The effectiveness of this process depends on establishing a flammable hydrogen–air mixture and ensuring thermal self-ignition conditions. Diagonal waves play an important role in raising the temperature of the fuel–air mixture, which can accelerate the self-ignition process by reactions on the surfaces of the whirling fuel. There is a close link between gas dynamics and chemical kinetics in responsive supersonic flow. Changes in temperature and pressure caused by the diagonal wave structure affect the local starting reactions on the surfaces of the whirling fuel, which also affects the reaction rates in the main combustion zone. Additionally, the emitted combustion heat may affect the flow structure, forming a diagonal wave structure extending back to the combustion zones.
The paper [
10] presents experimental and computational studies of supersonic flow and hydrogen combustion in the LAPCAT-II chamber, using ramjet/scramjet. The chamber was divided into four sections with increasing cross-sectional area. The research included experiments and simulations using the large vortices (LES) method for various values of total temperature, total pressure, and equivalence coefficient. Changing the chamber temperature led to different combustion behaviors. For lower temperatures, combustion took place only in a separated area, for medium temperatures—between the first and second sections and for higher temperatures—earlier. The results of LES and the experiments showed consistent pressure increases on the chamber walls. Both LES and the experiments showed the sensitivity of the chamber to changes in the total temperature, which resembled turbulent supersonic combustion of hydrogen and air.
In work [
11], the effect of hydrogen admixture on self-ignition of homogeneous and hybrid mixtures of heavy hydrocarbons in air was carried out with a detailed mechanism of n-decane oxidation reaction. It turned out that the reactivity of mixtures containing hydrogen is not always higher than the reactivity of pure hydrocarbon–air mixtures. At temperatures below about 1050 K, the addition of hydrogen to such mixtures increases the self-ignition delay, so it acts as an inhibitor. As the hydrogen content increases, the duration of the blue flame reaction becomes shorter and may even degrade. This is due to the reaction of hydrogen with intermediate products of hydrocarbon oxidation, which leads to the formation of less active forms, hindering the chain branching processes. However, at temperatures exceeding 1050 K, the addition of hydrogen reduces the overall self-ignition delay, indicating its role as a promoter.
However, it is generally accepted that hydrogen requires shorter ignition delays due to low ignition energy and high flame velocity. Wide range of flammability of hydrogen means that it can ignite and burn in a wide range of concentrations in the air (from about 4% to 75% by volume). In order to achieve a high concentration of hydrogen in diesel fuel, mix proportions must be carefully managed and controlled to optimize combustion without exceeding safety limits. Hydrogen and diesel fuel differ significantly in terms of combustion properties due to different chemical properties and combustion behavior. Hydrogen is highly flammable and has a low demand for ignition energy. It may ignite at low energy levels and wide concentration ranges. Diesel fuel, on the other hand, is less flammable and requires higher temperatures or a constant heat source to ignite in comparison to hydrogen [
12].
Hydrogen tends to reduce emissions of carbon monoxide (CO), particulate matters (PM), and unburnt hydrocarbons due to its cleaner combustion properties. Additionally, it can potentially reduce nitrogen oxide (NO
x) emissions by changing combustion conditions. Improving combustion efficiency through the addition of hydrogen has the potential to increase fuel economy [
13] by obtaining more energy from the fuel and achieving a better output with a given amount of diesel fuel. The use of hydrogen in a CI engine can positively affect its power due to a more efficient combustion process. As a result, this can increase torque and power, providing additional efficiency benefits. The presence of hydrogen in diesel fuel may affect engine components and materials. The lubricating properties change, which can affect the wear characteristics and the durability of the engine. Therefore, modifications may be necessary to ensure compatibility and durability. The use of hydrogen admixture can positively affect the performance of the engine when starting cold due to its properties, by facilitating ignition especially in colder climate conditions.
As already mentioned, the combustion of diesel fuel typically involves a longer ignition delay and burning time compared to hydrogen. However, it should be remembered that hydrogen, due to its unique properties, can under certain conditions potentially extinguish the flame in a CI engine; it has a high flame speed and a wide range of flammability, but it also has a high demand for ignition energy. Hydrogen, if added to a CI engine, can change the combustion characteristics and affect the spread of flame [
14,
15].
During combustion, hydrogen releases a significant amount of heat per unit mass. The high energy content results in efficient combustion, contributing to higher thermal efficiency in properly optimized systems. Diesel fuel has a lower energy content per unit mass compared to hydrogen. CI engines operate with lower thermal efficiency compared to hydrogen-powered engines due to factors such as incomplete combustion and heat loss.
The comparison of both fuels presented in the above summary shows how big the differences between them are. Modifications to the engine’s fuel system may be required to ensure proper mixing, injection, and combustion in order to effectively utilize hydrogen–diesel mixtures. Therefore, several factors seem to be crucial, including the percentage of hydrogen content, engine design, operating conditions, and control systems used. Research and development in this area is ongoing, with the aim of optimizing the proportions of mixtures and engine modifications to achieve the best performance and emission reductions. As with any modification to the fuel composition, thorough testing, adherence to engine manufacturer guidelines, and consideration of safety and performance implications are essential before hydrogen–diesel blends can be used in engines.
All this prompted the authors of this article to propose a new concept of improving combustion by dissolving hydrogen in diesel fuel. This approach focuses on the fuel injection and atomization process, which is one of the most important factors affecting the combustion efficiency of CI engines. It largely determines the efficiency of the engine and the emission of toxic exhaust components.
In currently used injection systems, the dispersion of the fuel stream into droplets occurs under the influence of only one physical stimulus. This is the velocity of the fuel flow in the atomizer holes, caused by the difference in pressure between the atomizer and the combustion chamber. The dispersion of the fuel stream initiated by this stimulus is facilitated by a secondary factor, which is the inertial and discrete medium into which the fuel is injected. It is believed that due to the low compressibility of the fuel, the expansion process does not play an important role in the atomization mechanism. In order to achieve an environmentally friendly spraying mechanism, not only is it necessary to apply a very high pressure but also to control this pressure according to the operating conditions of the engine. There are some physical implications that allow us to believe that the observed tendency in the development of injection systems is not necessarily the only possibility. The spray mechanism can be improved by increasing the injection pressure or modifying the fuel stream dispersion process.
In order to improve the combustion process, it is proposed to enrich the already existing spray mechanism with an additional physical stimulus, which is the spontaneous release of hydrogen from the liquid solution in the non-equilibrium phase. This process is volumetric. The concept of improving combustion consists in obtaining a fuel–gas solution by dissolving an appropriate amount of hydrogen in the diesel fuel. The equilibrium phase of the solution can be achieved at the assumed injection pressure. During the injection, a rapid pressure drop can be observed, which consequently reduces the thermodynamic potential of the solution in the equilibrium phase. As a result, the equilibrium phase is significantly disturbed, and the dissolved hydrogen is released from the entire volume of the solution. It can be expected that the kinetics of hydrogen release, if combined with the kinetics of the stimulus inducing the imbalance phase, may be significant.
The gas atoms in the solution are uniformly dispersed throughout the volume of the liquid. By releasing themselves simultaneously from the entire volume, they form diffuse microbubbles that expand and tend to aggregate. If the pressure drop is carried out dynamically, the microbubbles will not be able to accumulate in one volume and the expansion of hydrogen will take place in micro areas dispersed in the liquid. The energy generated during the gas release, and thus the work performed during hydrogen decompression, is absorbed by the solution. Thus, the release of hydrogen from the liquid induces additional internal forces that exceed the binding forces of the liquid particles and consequently ruptures the microbubble environment.
In the case of supplying the gas–fuel solution to the injector, there are physical premises that hydrogen can spontaneously release from the solution due to a sudden decrease in thermodynamic potential during fuel injection into the combustion chamber and thus due to a strong disturbance of the equilibrium state. As a result, the described mechanism should rupture the fuel droplets from the inside. Therefore, it will be an additional factor facilitating the fuel atomization mechanism and, as a result, improving the combustion process. This concept is illustrated in
Figure 2.
3. Results
During the tests, three measurement series were performed. The first for a conventional injection system equipped with a standard Bosch CP3 pump, which is a reference for further measurements. The two following measurements were carried out on a dedicated high-pressure pump enabling the dissolution of hydrogen in diesel fuel.
The fuel pressure during the measurements was regulated by an external controller based on the reading from the pressure sensor in the Common Rail tank and by regulating the operation of the electronic fuel dose valve on the pump and the pressure regulator on the CR tank. In order to demonstrate the favorable features of gas dissolution in the fuel, the injection pressure in each measurement series was 40 MPa.
In
Figure 5, a significant reduction in NOx emissions when supplied with a solution of diesel fuel with hydrogen indicates that the temperature of the medium has decreased during combustion, in particular the maximum values. However, the decrease in temperature due to the increasing combustion rate means that an additional factor must have appeared, which consequently accelerated combustion. The decrease in temperature could not have been caused by a change in the amount of fuel fed, because in both cases the same injection time and the same pressure in the tank were set. The acceleration of combustion must therefore have resulted from changes in the structure of the H
2 injection dissolved in diesel fuel.
A reduction in NOx emissions of up to 21% for a diesel blend containing 0.3% hydrogen suggests that changes in combustion dynamics due to the presence of hydrogen have led to fuller and more controlled combustion, thereby limiting the formation of nitrogen oxides. This result highlights the potential of hydrogen enrichment to reduce NOx emissions in internal combustion engines. The reduction of NOx emissions from hydrogen enrichment in a diesel engine is associated with complex combustion reactions.
The following are simplified reactions illustrating the potential impact of hydrogen on the reduction of NOx emissions. In a typical combustion process without hydrogen enrichment, nitrogen oxides (NOx) are formed as a result of high temperatures:
N2 + O2 → NO (Nitric oxide formation)
NO + O2 → NO2 (Conversion of NO to nitrogen dioxide)
High temperatures during combustion cycles in the engine promote the formation of nitrogen oxides. The addition of hydrogen to the fuel mixture affects the combustion process, leading to a reduction in NOx emissions due to the changed combustion dynamics:
H2 + O2 → H2O (Combustion of hydrogen with steam generation)
H2 + O2 → H2O2 (Formation of hydrogen peroxide)
The hydrogen–air mixture exhibits combustion in a wide range from 4 to 75% by volume of air, which represents a particularly wide combustion spectrum. Such a wide range ensures fuel savings because combustion is possible even with a lean mixture. The reduction of NOx content is facilitated by a slight increase in temperature at the end of combustion when using a lean mixture [
17,
18]. Taking into account that the self-ignition temperature of hydrogen (584.4 °C) exceeds the temperature of gasoline and natural gas, it becomes necessary to use an internal source [
19,
20] when using hydrogen in internal combustion engines. It is worth noting that a key aspect of internal combustion engines is to increase efficiency by increasing the compression ratio. The increased self-ignition temperature of hydrogen allows for the improvement in engine efficiency by achieving a higher compression ratio. Nevertheless, the shorter flame extinguishing distance for hydrogen, compared to gasoline and natural gas, increases the likelihood of flame reflection. In addition, the combustion rate of hydrogen under stoichiometric conditions and at atmospheric pressure is 2.83 m/s, while for gasoline, it is 0.3 m/s. Given the faster hydrogen combustion, adjustments to the existing system should take into account more rapid ignition time of hydrogen.
The presence of hydrogen can alter the formation pathways of nitrogen oxides during combustion. In the conventional combustion process, based on hydrocarbon fuels such as diesel fuel, the formation of NOx is intermediated with various nitrogen-containing radicals (e.g., NH, NH2, and N). However, in the case of hydrogen enrichment, reactions involving these intermediates may be disrupted or altered.
The chemical kinetics of the combustion reaction plays a key role in determining the formation of nitrogen oxides (NOx) in combustion engines [
21]. Hydrogen introduced into the combustion process significantly affects chemical kinetics, affecting the pathways and rate of formation of NOx intermediates.
The dynamics of rich combustion includes the combustion of fuel with a fuel–air equivalence ratio greater than 1. Compared to lean combustion conditions, total combustion requires more oxygen or oxygen atoms. As a result, the concentration of the OH radical decreases. At the same time, the share of hydrogen in OH radicals increases, which leads to hydrogen enrichment and an increase in the tendency of NHx radicals (x = 1, 2, 3) to combine with hydrogen and undergo oxidation.
One common example of a chain-termination reaction is the reaction between a radical and a stable molecule to form non-radical products. For instance, in the context of hydrocarbon combustion, the reaction of a hydroxyl radical (OH•) with a hydrocarbon molecule can be a chain-termination step:
OH• + Hydrocarbon → Products
In this reaction, the hydroxyl radical (OH•) reacts with a hydrocarbon, leading to the formation of stable products. The removal of the radical terminates the chain reaction because the radical is no longer available to initiate further propagation steps.
Chain-termination reactions play a crucial role in controlling the overall kinetics and dynamics of various chemical processes, including combustion reactions and polymerization reactions.
Within a certain temperature and oxygen concentration range, the reduction of NOx in the flames can be improved, in a process known as thermal DeNOx [
22,
23]. The main route of NO reduction, especially through reactions R1 and R2 (listed in
Table 3) [
24,
25], which are key elements of thermal DeNOx. The self-sufficient nature of the DeNOx mechanism results from the direct or indirect production of O and OH from R1 at a rate controlled by the branching ratio α = k
1/(k
1 + k
2). In addition, R1 exhibits high sensitivity to flame velocity and NO generation. When mixed with hydrogen, the increase in O/H radicals and the importance of the H
2/O
2 reaction make R1 with the NH
2 radical even more important [
26,
27]. R1 is considered a chain-branching reaction, whereas R2 is a chain-termination reaction. When the reaction reaches R2, N
2 + H
2O is terminated and formed. A low branching coefficient indicates that R1 is slower than R2, which makes the formation of O/H radicals difficult. R2 in a larger proportion allows for the continuous production of NO in the reaction. The large branching coefficient suggests that R1 produces a significant amount of NNH, promoting the production of OH and O in the subsequent steps:
NNH = N2 + H,
- (1)
H + O2 = O + OH
- (2)
O + H2O = OH + OH.
The lifespan of NNH radicals ranges from 10−11 to 10−8 s. During this period, NH2 radicals react with O/H radicals to form NO, replacing the reduction reaction. This gives
NH2 + OH = NH +H2O,
NH2 + O = HNO + H
and finally
An interesting observation concerns the effect of pressure on NOx emission in the mixture of NH
3/H
2/air. Below 1 atm, the increase in pressure reduces NO emission [
29,
30,
31]. Similarly, NOx emissions at a high pressure show a significant decrease compared to emissions at 1 atm, at levels below 5 and 1 ppm, and when the pressure exceeds 10 and 20 atm, respectively. Moreover, the addition of steam to the NH
3/H
2 mixture showed increased energy generation potential while mitigating Zeldovich’s NOx emissions and introducing O/H radicals into the system. The benefits include reductions in both NOx and unburnt NH
3, particularly with lower equivalence factors, φ [
32].
Another harmful compound analyzed during this research was carbon monoxide. Under these conditions, the CO concentration was higher by approx. 100% (
Figure 6). The presence of CO in the exhaust gas signals a local shortage of oxygen necessary for combustion. The main cause of oxygen deficiencies is the improper matching of vortexes occurring in the combustion chamber with the jet of sprayed fuel. The shortage also depends on the atomization structure of the fuel but to a lesser extent. Therefore, it is treated as a secondary indicator when assessing the preparation of fuel for combustion.
The occurrence of increased CO emissions suggests a disturbance of the ideal balance of fuel and oxygen in the combustion chamber. In a properly functioning combustion process, the fuel is expected to mix evenly with oxygen, facilitating full and efficient combustion, resulting in lower CO emissions. However, the observed increase in CO levels indicates that, under certain conditions, this balance can be disturbed. The basic factor contributing to these deficiencies is the improper matching of vortexes in the combustion chamber to the sprayed dose of fuel. The vortexes play a key role in creating a well-mixed air–fuel mixture, ensuring optimal combustion efficiency. When the vortexes are not properly aligned in the fuel stream, this leads to uneven mixing, resulting in local insufficiency of oxygen. This oxygen deficiency hinders the combustion process, resulting in increased carbon monoxide production. Although the fuel atomization structure is considered a contributing factor, its influence is considered secondary to the key role played by the vortexes. The complicated relationship between the vortexes and the setting of the fuel stream is necessary to obtain an optimal air–fuel mixture and, consequently, to minimize CO emissions. The noticeable increase in CO emissions observed under these conditions highlights the importance of fine adjustments in the combustion chamber to ensure efficient mixing of fuel and air. Solving the problem of vortex–fuel misalignment is essential to alleviate local oxygen deficiencies, thereby increasing combustion efficiency and reducing carbon monoxide emissions.
Compared to the diesel fuel supply system (
Figure 7 and
Figure 8), in all measurements carried out on the solution supply system, the concentration of PM in the exhaust gas decreased significantly (in some cases up to 20%). PM emission indicates, to a large extent, the soot content in the exhaust gas. If the mechanism of soot formation is simplified to cracking, it can be concluded that the liquid fuel phase causes soot formation. The amount of soot produced depends on the physical conditions under which the airless liquid hydrocarbon phase is maintained.
The pressure and temperature values in both cases are approximate (the analysis was performed for the same torque values). Therefore, time must play a significant role. The duration of the liquid phase depends on the rate of evaporation and, thus, on the size of the droplets (the conditions of movement of the medium in the chamber are similar), resulting from the operation of the fuel-atomizing mechanism. According to the described soot formation mechanism, PM occurs due to the shortening of the liquid phase time. This means that the droplets in the solution supply systems should have had smaller diameters than the droplets in the diesel supply systems. Although the injection pressure was the same, it can be concluded on the basis of PM emissions that the atomization of diesel fuel with H2 must be preceded by significant changes in the fuel atomization mechanism to decrease droplets’ diameters, which consequently would allow for more favorable fuel atomization at the combustion site compared to a conventional diesel fuel system. The factor causing this change is the physical release effect that occurs when gas is released from the liquid in which it is dissolved and whenever an imbalance occurs, i.e., when the thermodynamic potential of the solution is higher than the thermodynamic potential of the environment into which the ON solution with H2 is injected.
Despite the identical injection pressure, the particulate matter (PM) emission test indicates that the process of hydrogen atomization of diesel fuel (H2) requires significant changes in the fuel atomization mechanism. These modifications lead to the formation of droplets with a smaller diameter, which seems to play a key role in obtaining more favorable fuel atomization at the combustion point compared to a conventional diesel fuel system. The observed differences in particulate emissions between hydrogen and conventional diesel fuel systems highlight the complex relationship between fuel atomization and combustion efficiency. Although the injection pressure remained constant, the introduction of hydrogen appears to cause changes in the atomization process, possibly affecting the droplet size distribution. The formation of smaller-diameter droplets in the case of hydrogen diesel suggests a change in microstructure and an evenly distributed stream of fuel. This finer atomization may have several combustion benefits, such as increased oxygen interaction area, improved evaporation, and a more homogeneous air–fuel mixture. These factors contribute to improving combustion efficiency and can potentially lead to a reduction in particulate emissions. The conclusions drawn from particulate emissions emphasize the importance of understanding and optimizing the fuel atomization mechanism when introducing hydrogen into diesel fuel. Tuning this process seems to play a key role in achieving more efficient combustion, highlighting the potential of cleaner and more efficient power systems. Further investigation of specific changes in the fuel atomization mechanism will provide valuable insights to improve the integration of hydrogen in CI engines, with the ultimate goal of reducing emissions and increasing overall system performance.
The general trend observed for the combustion of fuels with the addition of hydrogen indicates that the flame temperature increases with the increase in the share of hydrogen in the fuel mixture, and it can be illustrated as two curves of the flame temperature [
33,
34]. The rate of increase in flame temperature is particularly noticeable when the proportion of H
2 exceeds 90%, indicating the dominance of H
2 for the second curve. For all tested equivalence coefficients, it was observed that the normalized rate of heat release increases with the addition of H
2. The maximum rate of heat release occurs at the same temperature in the fuel-rich area but shifts to a lower temperature in stoichiometric and fuel-poor areas as the proportion of hydrogen increases. In general, the rate of heat release remains higher in fuel-rich and stoichiometric areas [
35].
Theoretically, the maximum power in a hydrogen engine depends on the selected air–fuel ratio and fuel injection method. Some studies indicate that the stoichiometric air-to-fuel ratio for hydrogen is 34:1. At this particular ratio, hydrogen occupies 29% of the combustion chamber, leaving only 71% for air. As a result, the energy content of this mixture is lower compared to diesel fuel. This is due to the fact that diesel fuel, being a liquid, occupies a minimum volume in the combustion chamber, allowing more air to enter and thus increasing the energy content [
36,
37,
38].
Calculating the engine’s thermal energy when burning a mixture of hydrogen and diesel fuel involves several factors, including the energy content of each fuel and the combustion efficiency. The calculation is as follows:
Energy Content of Hydrogen: The lower heating value (LHV) of hydrogen is approximately 120 MJ/kg.
Energy Content of Diesel Fuel: The LHV of diesel fuel can vary, but it is assumed to be around 45 MJ/kg in this case.
Combustion Efficiency: The combustion efficiency varies based on engine design and operating conditions. A typical range for internal combustion engines might be from 20% to 30%.
The formula for calculating thermal energy (Q) is
where
Q is the thermal energy;
m is the mass of the fuel burned;
LHV is the lower heating value of the fuel;
η is the combustion efficiency (expressed as a decimal).
The share of hydrogen energy in the fuel mixture can be calculated according to the following equation:
In the analyzed case, with the parameters set to a fuel pressure of 400 bar, fuel consumption of 1.21 kg/h, and a hydrogen pressure of 2.5 bar at the entrance to the pump, the following is obtained:
Assuming a certain mass of hydrogen (mH
2) and diesel fuel (mdiesel) burned in the engine, the thermal energy for each fuel can be calculated and then summed up.
It has to be kept in mind that the actual energy obtained from the combustion process can be influenced by factors such as the combustion efficiency, engine design, and the air–fuel ratio. The actual engine performance may vary, and the values provided here are for illustrative purposes.
The equilibrium constant (K) expression along with the van’t Hoff equation can be used to represent the effect of a decrease in temperature on the chemical equilibrium of the reaction involving the production of NO. Assuming a simple reaction
where a, b, c, and d are the stoichiometric coefficients.
The Equilibrium Constant Expression is given as
And the Van’t Hoff Equation is given as
Now, for the specific reaction involving the production of NO, the appropriate stoichiometric coefficients can be substituted, and the signs can be adjusted according to the direction of the reaction. The generic reaction N2 + O2 ⇌ 2NO will be used for simplicity.
Equilibrium constant expression for NO formation:
Van’t Hoff Equation for Temperature Decrease (T2 < T1):
The negative sign in the exponent indicates that a decrease in temperature (T2 < T1) leads to a decrease in the equilibrium constant (K(T2) < K(T1)), favoring the production of lower concentrations of NO. The equilibrium constant reflects the ratio of product concentrations to reactant concentrations at equilibrium, and a lower equilibrium constant suggests a shift towards lower product concentrations.