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How does a diesel engine differ from a gasoline engine?

Short Answer

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Question: Briefly explain the differences between diesel engines and gasoline engines in terms of their working principles, fuel used, and efficiency. Answer: Diesel engines work on compression-ignition, using diesel fuel and are generally more fuel-efficient. Gasoline engines work on spark-ignition, using gasoline as fuel, and are typically less fuel-efficient.

Step by step solution

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1. Introduction to Diesel and Gasoline Engines

Diesel and gasoline engines are two types of internal combustion engines commonly used to generate mechanical power for various applications. They work on slightly different principles and involve different types of fuel, as well as varying levels of efficiency.
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2. Working Principle of a Diesel Engine

A diesel engine works on the principle of compression-ignition, where the fuel-air mixture is compressed to a high pressure and temperature which makes it self-ignite. In a diesel engine, only air is drawn into the combustion chamber during the intake stroke. During the compression stroke, the air is compressed, causing its temperature to rise significantly. The fuel is then injected into the hot compressed air, which causes it to ignite and burn, producing mechanical power.
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3. Working Principle of a Gasoline Engine

A gasoline engine, on the other hand, works on the principle of spark-ignition. In a gasoline engine, a fuel-air mixture is drawn into the combustion chamber during the intake stroke. The mixture is then compressed during the compression stroke. Instead of relying on the heat created by the compression to ignite the fuel, a spark plug provides an electrical spark that ignites the compressed fuel-air mixture, producing a controlled explosion that generates mechanical power.
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4. Fuel Used in Diesel and Gasoline Engines

A diesel engine uses diesel fuel, which is heavier and has a higher energy content compared to gasoline. Diesel fuel is less volatile and has a higher flash point, which means it requires higher temperatures to ignite. Gasoline engines use gasoline, a more volatile fuel with a lower energy content and flash point, making it easier to ignite with a spark.
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5. Efficiency

Diesel engines are generally more fuel-efficient than gasoline engines. This is mainly due to their higher compression ratio and the fact that diesel fuel has a higher energy content than gasoline. The higher compression ratio leads to a more efficient combustion process, allowing diesel engines to convert a greater percentage of the fuel's energy into mechanical power. In summary, diesel engines differ from gasoline engines in their working principles, the type of fuel used, and their fuel efficiency. Diesel engines operate on compression-ignition, use diesel fuel, and are generally more fuel-efficient, while gasoline engines operate on spark-ignition, use gasoline as fuel, and are typically less fuel-efficient.

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Key Concepts

These are the key concepts you need to understand to accurately answer the question.

Internal Combustion Engines
Internal combustion engines are remarkable machines that convert chemical energy from fuel into mechanical energy. They power a significant portion of the world’s vehicles, from passenger cars to large trucks. Essential to this process is the combustion of the fuel within the engine's chambers, which pushes pistons and creates motion. These engines come in two distict variants: diesel and gasoline, each with its own operating mechanism and applications.

While both types fall under the internal combustion category, they differ significantly in how they ignite the fuel and utilize air during the combustion cycle. Understanding this distinction is key to grasping the fundamental principles that underlie the operation of each engine type.
Compression-Ignition
Compression-ignition is the trademark of diesel engines. It relies on the principle that when you compress a gas, its temperature rises. In a compression-ignition engine, air is drawn into the combustion chamber and compressed to high pressures, causing the temperature to increase dramatically.

At the peak of compression, diesel fuel is injected into the chamber. As diesel has a high flash point, it doesn't ignite until it reaches the high temperatures caused by compression. This characteristic allows for self-ignition without the need for a spark plug, and the burning fuel forces the piston down, thus powering the engine.
Spark-Ignition
Unlike their diesel counterparts, spark-ignition engines define the operation of gasoline engines. In these engines, a mix of air and gasoline is drawn into the combustion chamber during the intake stroke. This mixture is then compressed, but not to the extent found in diesel engines, as gasoline vapour ignites at lower temperatures.

At the critical moment in the cycle, a spark plug introduces a precisely-timed spark that ignites the compressed mixture. This controlled burn provides the force necessary to drive the piston and consequently, the engine. Spark-ignition systems require a fine balance of fuel-to-air ratios and timing to maximize efficiency and performance.
Fuel Efficiency
Fuel efficiency is a critical factor in engine performance and environmental impact. Diesel engines are typically more fuel-efficient than gasoline engines because of two primary attributes: their higher compression ratios and the higher energy content in diesel fuel.

A diesel engine compresses air to such an extent that the ensuing combustion is more complete, meaning more energy is extracted from each drop of fuel. Moreover, diesel fuel contains more energy per litre than gasoline, which translates to more power and better mileage. This increased efficiency often makes diesel engines a popular choice for heavy-duty applications where torque and range are important.
Combustion Chamber
The combustion chamber is the heart of any internal combustion engine. It's where the magic happens—fuel is converted into the mechanical energy that powers vehicles. For optimal performance and efficiency, the design of the combustion chamber is finely tuned to the type of engine it serves.

In diesel engines, the combustion chamber is designed to withstand high pressures and temperatures needed for compression-ignition. Gasoline engines, conversely, are designed with different priorities such as managing the flow of the fuel-air mix and the timing of the spark. Each type aims to optimize the burn of fuel, reduce emissions, and maximize power output. The chamber's shape, size, and volume are all engineered with these goals in mind.

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Most popular questions from this chapter

An ideal dual cycle has a compression ratio of 15 and a cutoff ratio of \(1.4 .\) The pressure ratio during constantvolume heat addition process is \(1.1 .\) The state of the air at the beginning of the compression is \(P_{1}=14.2\) psia and \(T_{1}=75^{\circ} \mathrm{F}\) Calculate the cycle's net specific work, specific heat addition, and thermal efficiency. Use constant specific heats at room temperature.

Helium gas in an ideal Otto cycle is compressed from \(20^{\circ} \mathrm{C}\) and 2.5 to \(0.25 \mathrm{L},\) and its temperature increases by an additional \(700^{\circ} \mathrm{C}\) during the heat addition process. The temperature of helium before the expansion process is \((a) 1790^{\circ} \mathrm{C}\) (b) \(2060^{\circ} \mathrm{C}\) \((c) 1240^{\circ} \mathrm{C}\) \((d) 620^{\circ} \mathrm{C}\) \((e) 820^{\circ} \mathrm{C}\)

A turbojet is flying with a velocity of \(900 \mathrm{ft} / \mathrm{s}\) at an altitude of \(20,000 \mathrm{ft}\), where the ambient conditions are 7 psia and \(10^{\circ} \mathrm{F}\). The pressure ratio across the compressor is \(13,\) and the temperature at the turbine inlet is 2400 R. Assuming ideal operation for all components and constant specific heats for air at room temperature, determine ( \(a\) ) the pressure at the turbine exit, \((b)\) the velocity of the exhaust gases, and \((c)\) the propulsive efficiency.

A gas-turbine power plant operates on a modified Brayton cycle shown in the figure with an overall pressure ratio of \(8 .\) Air enters the compressor at \(0^{\circ} \mathrm{C}\) and \(100 \mathrm{kPa}\) The maximum cycle temperature is 1500 K. The compressor and the turbines are isentropic. The high pressure turbine develops just enough power to run the compressor. Assume constant properties for air at \(300 \mathrm{K}\) with \(c_{v}=0.718 \mathrm{kJ} / \mathrm{kg} \cdot \mathrm{K}\) \(c_{p}=1.005 \mathrm{kJ} / \mathrm{kg} \cdot \mathrm{K}, R=0.287 \mathrm{kJ} / \mathrm{kg} \cdot \mathrm{K}, k=1.4\) (a) Sketch the \(T\) -s diagram for the cycle. Label the data states. (b) Determine the temperature and pressure at state \(4,\) the exit of the high pressure turbine. (c) If the net power output is \(200 \mathrm{MW}\), determine mass flow rate of the air into the compressor, in \(\mathrm{kg} / \mathrm{s}\)

A Carnot cycle operates between the temperature limits of 300 and \(2000 \mathrm{K},\) and produces \(600 \mathrm{kW}\) of net power. The rate of entropy change of the working fluid during the heat addition process is \((a) 0\) (b) \(0.300 \mathrm{kW} / \mathrm{K}\) \((c) 0.353 \mathrm{kW} / \mathrm{K}\) \((d) 0.261 \mathrm{kW} / \mathrm{K}\) \((e) 2.0 \mathrm{kW} / \mathrm{K}\)

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