The Wright brothers used a
gasoline powered, four-stroke,
internal combustion engine to power their
aircraft. In an internal combustion engine, fuel and air are
ignited inside a
cylinder. The hot exhaust gas pushes a piston in the cylinder which is connected to a
crankshaft to produce power. The burning of fuel is not a continuous process, but occurs very quickly at regular time intervals. Between ignitions, the engine parts move in a repeated sequence called a
cycle. The engine is called a four-stroke engine because there are four movements
(strokes) of the piston during one cycle. The brothers' design was based on early automobile engine designs which used the
Otto cycle, developed by the German, Dr. N. A. Otto, in 1876.
The brothers' design is very simple by today's standards, so it is a good engine for students to study to learn the fundamentals of engine operation. There are two main parts to engine operation: the
mechanical operation of the engine parts, and the thermodynamics through which the engine produces
work and
power. On this page we will discuss the basic thermodynamic principles and on a separate page we present the
thermodynamic analysis that allows you to design and predict engine performance.
Thermodynamics is a branch of physics which deals with the energy and work of a system. It was born in the 19th century as scientists were first discovering how to build and operate steam engines. Thermodynamics deals only with the large scale response of a system which we can observe and measure in experiments. The basic ideas of thermodynamics are taught in high school physics classes, so the Wright brothers knew and used these concepts, particularly in their
engine design.
We have broken the Otto cycle into six numbered stages based on the
mechanical operation of the engine. At each stage, we show a cut through the cylinder to reveal the movement of the piston and the amount of the gas volume created by the head of the piston and the cylinder to the right of the piston head. On the figure we show a plot of
pressure versus gas
volume throughout one cycle. The cycle begins at the lower left with
Stage 1 being the beginning of the
intake stroke of the engine. The pressure is near atmospheric pressure and the gas volume is at a minimum with the piston far to the right in the cylinder. Between Stage 1 and Stage 2 the piston is moved to the left, the pressure remains constant, and the gas volume increases as fuel/air mixture is drawn into the cylinder through the intake valve (red).
Stage 2 begins the
compression stroke of the engine with the closing of the intake valve. Between Stage 2 and Stage 3, the piston moves back to the right, the gas volume decreases, and the pressure increases because
work is done on the gas by the piston.
Stage 3 is the beginning of the
combustion of the fuel/air mixture. The combustion occurs very quickly and the volume remains constant.
Heat is released during combustion which increases both the
temperature and the pressure, according to the
equation of state.
Stage 4 begins the
power stroke of the engine. Between Stage 4 and Stage 5, the piston moves back to the left, the volume in increased, and the pressure falls as
work is done by the gas on the piston. At
Stage 5 the exhaust valve (blue) is opened and the residual heat in the gas is
exchanged with the surroundings. The volume remains constant and the pressure adjusts back to atmospheric conditions.
Stage 6 begins the
exhaust stroke of the engine during which the piston moves back to the right, the volume decreases and the pressure remains constant. At the end of the exhaust stroke, conditions have returned to Stage 1 and the process repeats itself.
During the cycle,
work is done on the gas by the piston between stages 2 and 3. Work is done by the gas on the piston between stages 4 and 5. The difference between the work done by the gas and the work done on the gas is shown in yellow and is the work produced by the cycle. The work times the rate of the cycle (cycles per second) is equal to the
power produced by the engine. The area enclosed by the cycle on a p-V diagram is proportional to the work produced by the cycle. On this page we have shown an
ideal Otto cycle in which there is no heat entering (or leaving) the gas during the compression and power strokes, no friction losses, and instantaneous burning occurring at constant volume. In reality, the ideal cycle does not occur and there are many losses associated with each process. These losses are normally accounted for by efficiency factors which multiply and modify the ideal result. For a real cycle, the shape of the p-V diagram is similar to the ideal, but the area (work) is always less than the ideal value.