This is a computer drawing of one cylinder of the Wright
1903 aircraft engine.
This engine powered the first, heavier than
air, self-propelled, maneuverable, piloted aircraft; the Wright
The engine consisted of four
like the one shown above, with
each piston connected to a common
which turns the
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. This type of
internal combustion engine
is called a
engine because there are four movements
of the piston before the entire engine firing sequence is repeated.
In the figure, we have colored the
fuel/air intake system
green, and the
blue. We also represent the fuel/air mixture and the exhaust gases by small
colored balls to show how these gases move through the engine.
Since we will be referring to the movement of various engine parts, here is
a figure showing the names of the parts:
At the end of the
the fuel/air mixture has been drawn into the cylinder at low (nearly
atmospheric) pressure by the motion of the piston towards the crankshaft
at the left. From our considerations of the
we designate this condition as Stage 2 of the Otto cycle.
The intake valve is then closed and the piston begins to
move back towards the combustion chamber at the right.
With both valves closed, the combination of the cylinder and combustion chamber
form a completely closed vessel containing the fuel/air mixture. As the piston
is pushed to the right, the volume is reduced and the fuel/air mixture is
compressed. When the piston has moved completely to the right, we designate
the conditions as Stage 3 of the cycle.
During the compression stroke, the electrical contact is kept opened.
When the volume is the smallest,
and the pressure the highest, the contact is closed and current
flows through the completed circuit.
The switch is then quickly opened, producing a spark
ignites the mixture.
During the compression, no
is transferred to the fuel/air mixture.
As the volume is decreased because of the piston's motion,
the pressure in the gas is increased.
In the figure, the mixture has been colored blue at stage 2 and
yellow at stage 3 to denote a moderate increase in pressure.
To produce the increased pressure, we have to do
on the mixture, just
as you have to do work to inflate a bicycle tire using a pump.
There are thermodynamic
which relate the pressure increase and temperature increase to the
change in volume:
p3 / p2 = (V2 / V3) ^ gamma
T3 / T2 = (V2 / V3) ^ (gamma - 1)
where p is the pressure, T is the temperature,
V is the volume of the mixture,
and gamma is the ratio of
specific heats of the mixture.
The numbers indicate the two stages of the cycle.
Since V2 is greater than V3 and gamma is greater than 1 (1.4 for pure air),
p3 is greater than p2 and T3 is greater than T2. Pressure and temperature
of the fuel/air mixture both increase during the compression process, and
the final value (p3 and T3) depends only on a geometric compression ratio
(V2/V3) to some power multiplied by the intial value (p2 and T2).
- Re-Living the Wright Way
- Beginner's Guide to Aeronautics
- NASA Home Page