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How do internal and external combustion engines differ?

Short Answer

Expert verified
Internal combustion engines burn fuel inside the engine, like in car engines. External combustion engines burn fuel externally, like in steam engines.

Step by step solution

01

- Definition of Combustion Engines

First, understand what a combustion engine is. A combustion engine is a complex machine that converts fuel into mechanical energy, typically to power vehicles.
02

- Internal Combustion Engine

Define internal combustion engines (ICE). In an ICE, the combustion of fuel occurs inside the engine itself. The chemical energy of the fuel is converted into thermal energy through combustion, which then produces mechanical work.
03

- External Combustion Engine

Define external combustion engines (ECE). In an ECE, the combustion of fuel happens outside the engine. The produced thermal energy is then transferred to the engine to do work, commonly via a working fluid like water or air.
04

- Comparison of Fuel Combustion Location

Compare the location of combustion. For an internal combustion engine, the fuel burns inside the engine’s cylinders. For an external combustion engine, the fuel combusts externally in a separate part of the system and the energy is transferred into the engine.
05

- Examples for Each Engine Type

Provide examples. A common internal combustion engine example is the gasoline or diesel engine used in most cars today. A common external combustion engine example is the steam engine used in old locomotives.

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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 (ICEs) are fascinating devices widely used in vehicles today. In these engines, the combustion of fuel takes place within the engine itself, typically in cylinders. This process converts the chemical energy of the fuel into thermal energy through combustion.
The generated thermal energy then transforms into mechanical work, driving the pistons and thus the vehicle.
Common examples of internal combustion engines include gasoline engines and diesel engines.

These engines are popular due to their efficiency, compact size, and powerful output, making them ideal for cars, motorcycles, and even airplanes.
External Combustion Engines
External combustion engines (ECEs) work differently from internal combustion engines. In an ECE, fuel combustion occurs outside the engine in a separate compartment.
The generated heat energy is then transferred to the engine to produce mechanical work.
This is often accomplished using a working fluid like water or air. An excellent example is the steam engine.

The steam created by heating water outside the engine then moves into the engine, causing mechanical motion.
Although less common today, external combustion engines were crucial during the industrial revolution for powering locomotives and factories.
Thermal Energy Conversion
Converting thermal energy into mechanical work is a core function of combustion engines.
In both internal and external combustion engines, fuel combustion releases thermal energy.

For internal combustion engines, this thermal energy directly impacts the engine's internal components, causing expansion that moves the pistons.
For external combustion engines, the thermal energy heats a working fluid that then drives the engine.
This process of transforming thermal energy into motion is fundamental to both types of engines' operation.
Mechanical Work
Mechanical work is the movement or force produced by an engine. In combustion engines, mechanical work is derived from the energy released during fuel combustion.
In internal combustion engines, the expanding gases push the pistons, creating motion. This motion can be used to power various applications like vehicle wheels or machinery parts.

In external combustion engines, thermal energy heats a fluid that expands and moves within the engine, generating mechanical work.
This is a key principle behind the operation of engines, whether they are powering a car or driving a factory machine.
Engine Types Comparison
Comparing internal and external combustion engines reveals several key differences.
For internal combustion engines, fuel burns inside the engine's cylinders, and the conversion of thermal energy to mechanical work happens in one place.
These engines are generally more efficient and compact.

In contrast, external combustion engines burn fuel outside the engine, and the heat energy is transferred via a working fluid. This separation can lead to larger engine sizes and greater simplicity in design.
Common examples are: cars and motorcycles for internal combustion engines, and steam engines for external combustion engines.
Understanding these differences helps you appreciate the diverse applications and historical significance of each engine type.

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Most popular questions from this chapter

An air-standard Brayton cycle has a compressor pressure ratio of 10 . Air enters the compressor at \(p_{1}=100 \mathrm{kPa}\), \(T_{1}=20^{\circ} \mathrm{C}\) with a mass flow rate of \(11 \mathrm{~kg} / \mathrm{s}\). The turbine inlet temperature is \(1222 \mathrm{~K}\). Calculate the thermal efficiency and the net power developed, in \(\mathrm{kW}\), if (a) the turbine and compressor isentropic efficiencies are each \(100 \%\). (b) the turbine and compressor isentropic efficiencies are 88 and \(84 \%\), respectively. (c) the turbine and compressor isentropic efficiencies are 88 and \(84 \%\), respectively, and a regenerator with an effectiveness of \(80 \%\) is incorporated.

A converging-diverging nozzle operating at steady state has a throat area of \(3 \mathrm{~cm}^{2}\) and an exit area of \(6 \mathrm{~cm}^{2}\). Air as an ideal gas with \(k=1.4\) enters the nozzle at 8 bar, \(400 \mathrm{~K}\), and a Mach number of \(0.2\), and flows isentropically throughout. If the nozzle is choked, and the diverging portion acts as a supersonic nozzle, determine the mass flow rate, in \(\mathrm{kg} / \mathrm{s}\), and the Mach number, pressure, in bar, and temperature, in \(\mathrm{K}\), at the exit. Repeat if the diverging portion acts as a supersonic diffuser.

Air enters the compressor of a gas turbine at \(100 \mathrm{kPa}\), \(300 \mathrm{~K}\). The air is compressed in two stages to \(900 \mathrm{kPa}\), with intercooling to \(300 \mathrm{~K}\) between the stages at a pressure of \(300 \mathrm{kPa}\). The turbine inlet temperature is \(1480 \mathrm{~K}\) and the expansion occurs in two stages, with reheat to \(1420 \mathrm{~K}\) between the stages at a pressure of \(300 \mathrm{kPa}\). The compressor and turbine stage efficiencies are 84 and \(82 \%\), respectively. The net power developed is \(1.8 \mathrm{MW}\). Determine (a) the volumetric flow rate, in \(\mathrm{m}^{3} / \mathrm{s}\), at the inlet of each compressor stage. (b) the thermal efficiency of the cycle. (c) the back work ratio.

Helium gas is flowing through a duct. At a particular location it is at \(150 \mathrm{kPa}\) and \(300 \mathrm{~K}\), and it has a velocity of \(280 \mathrm{~m} / \mathrm{s}\). Assume that Helium behaves as an ideal gas. Determine (a) the Mach number. (b) the stagnation temperature in \(\mathrm{K}\). (c) the stagnation pressure in kPa.

Air enters the compressor of a simple gas turbine at \(p_{1}=96 \mathrm{kPa}, T_{1}=298 \mathrm{~K}\). The isentropic efficiencies of the compressor and turbine are 85 and \(89 \%\), respectively. The compressor pressure ratio is 13 and the temperature at the turbine inlet is \(1340 \mathrm{~K}\). The net power developed is \(1450 \mathrm{~kW}\). On the basis of an air-standard analysis, calculate (a) the volumetric flow rate of the air entering the compressor, in \(\mathrm{m}^{3} / \mathrm{s}\). (b) the temperatures at the compressor and turbine exits, each in \(\mathrm{K}\). (c) the thermal efficiency of the cycle.

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