The Otto engine and the diesel engine are two types of thermal engines. These are two types of endothermic engines that, by thermodynamic reactions, convert the internal energy of the fuel into mechanical work. However, there are certain differences between them.
The most important difference is found in its theoretical cycle. The Otto engine operates according to the Otto cycle by spark ignition while the diesel engine is governed according to the diesel cycle by compression ignition.
The other important difference is in the ignition of the fuel. In the Otto engine the ignition is carried out by means of the spark caused by the spark plug, for this reason it is also known as the spark ignition engine. On the other hand, in the diesel engine, the ignition is carried out by the compression of the fuel; For this reason, the diesel engine is also known as a compression ignition engine.
At the mechanical level there are no major differences between both types of alternative engines. However, it should be noted that the diesel engine, when combusting at a much higher pressure, requires a more robust structure than in the gasoline engine.
The fundamental differences between the two types of engine derive from the differences in their cycles:
- Differences in the entry of fuel into the engine
- Difference in fuel ignition
- Differences in compression ratio
Differences in fuel input
Fuel entry into the diesel engine and the Otto engine is one of the most important differences between both types of thermal engines:
Fuel inlet into the gasoline engine.
Currently, this mixture is generated electronically and its proportions vary depending on different factors such as the temperature of the engine and fuel. In the past, car engines used two types of mechanisms to regulate the entry of fuel at startup: the starter, to increase the amount of gasoline or the air choke that limited air access by increasing the proportion of gasoline,
Fuel inlet in diesel engine
In the diesel engine the air is introduced into the combustion chamber through ducts that go to the suction valve. In this type of thermal engines the fuel (diesel) is introduced directly by means of an injector.
In this type of engine it is important to keep in mind that the pressure inside the cylinder is higher than in the Otto engine. One of the functions of the injector is to print enough pressure to the fuel so that it can enter.
The air-fuel mixture is carried out in the combustion chamber. In the diesel engine there is no regulation of the amount of air, there is only a regulation of the amount of fuel introduced.
Fuel ignition difference
Once the fuel has been introduced into the cylinder, the way it ignites is different between both types of engines. In one case the ignition is carried out by supplying temperature and in the other the ignition of the fuel is carried out by increasing the pressure inside the cylinder. According to the laws of thermodynamics and the law of gases, both state variables ( pressure and temperature) are related. If the volume remains constant, increasing one increases the other.
Ignition of fuel in the gasoline engine
In the Otto engine, the fuel is ignited by a spark. This type of engine requires an ignition system to generate a spark between the spark plug electrodes in the combustion chamber. This spark implies an increase in the temperature of the mixture. This temperature increase is sufficient to allow combustion to start.
Ignition of fuel in the diesel engine
In diesel engine the ignition is done by compression. This type of engine uses the high temperature and pressure obtained by compressing the air in the cylinder to start combustion when the fuel is injected.
In the diesel engine this temperature is achieved by air compression. During the admission cycle the air enters the explosion chamber that will be compressed in the next cycle, that compression generates an increase in air temperature until the autoignition temperature value is passed.
It is at that moment when the injectors put the fuel under pressure, in a pulverized way for a better mixture with the air, and the combustion of the same takes place.
Differences in compression ratio
The compression ratio in an endothermic engine is the number that makes it possible to measure the proportion in which the air-fuel mixture (Otto engine) or air (diesel engine) has been compressed inside the combustion chamber of a cylinder.
In the Otto engine (spark ignition), the upper limit of the compression ratio is essentially determined by the anti-knock quality of the fuel on the market; For Diesel engines, it is determined, above all, by the weight of the engine structure, which increases with increasing compression ratio. This increase is presented in a special way with large displacements.
Difference in weight of the Otto engine with the diesel engine
In this case, the ignition form affects the weight. That is, in the diesel engine, the ignition of the fuel is carried out by compression. As we have mentioned in the mechanical differences, this means that it must be made with a design that can withstand these high pressures. In practice, this means a larger engine, and therefore heavier.
The diesel engine is generally heavier than an Otto engine of equal displacement. If it is the engine of a vehicle, the weight of the engine will also have to be shifted, so the engine will need more power to have similar performance. The amount of work of the vehicle will have to be higher since it displaces more mass per displaced meter.
Another difference that does not affect performance but braking.
In the case of gasoline engines, the engine brake is produced by the air intake system. When we stop accelerating the throttle in an atom mobile, the air flow closes, at that moment the air stops entering the combustion chamber and a vacuum is generated. The force that the piston has to make to generate that vacuum is the energy that is achieved by braking.
In the case of diesel vehicles, and since they do not have an acceleration body, it is not possible to close the air flow to generate that vacuum. The natural process would be as follows: the valves are opened and air enters, the valves are closed and the air is compressed, when the piston reaches the top dead center begins its descent helped by the pressure of the compressed air. In this way there would be hardly any loss of energy.