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First Law of Thermodynamics
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C.Mascolini, Daliento, C.Del Plato (*) - I.Ionita (**)
(*) Istituto Alfano I - (**)
University of Galati
Thermodynamics
Summary
Thermodynamics is the science of the relationship between
heat,
work, and
systems that analyze
energy processes. The energy processes that convert heat energy from available
sources such as chemical
fuels
into mechanical work are the major concern of this science. Thermodynamics consists
of a number of analytical and theoretical methods which may be applied to machines
for energy conversion.
First Law of Thermodynamics
The first law of thermodynamics is the application of the conservation
of energy principle to heat and thermodynamic processes:
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Change in internal energy =
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Heat added to the system
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- Work done by the system
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The first law makes use of the key concepts of internal
energy, heat,
and system
work. It is used extensively in the discussion of heat
engines.
It is typical for chemistry texts to write the first law as
ΔU=Q+W. It is the same law, of course - the thermodynamic expression of
the conservation of energy principle. It is just that W is defined as the work
done on the system instead of work done by the system. In the context of physics,
the common scenario is one of adding heat to a volume of gas and using the expansion
of that gas to do work, as in the pushing down of a piston in an internal combustion
engine. In the context of chemical reactions and process, it may be more common
to deal with situations where work is done on the system rather than by it.
Enthalpy
Four quantities called "thermodynamic
potentials" are useful in the chemical thermodynamics of reactions
and non-cyclic processes. They are internal
energy, the enthalpy, the Helmholtz
free energy and the Gibbs
free energy. Enthalpy is defined by
H = U + PV
where P and V are the pressure and volume, and U
is internal energy. Enthalpy is then a precisely measurable state
variable, since it is defined in terms of three other precisely definable
state variables. It is somewhat parallel to the first
law of thermodynamics for a constant pressure system
Q = ΔU + PΔV since in this case Q=ΔH
It is a useful quantity for tracking chemical reactions. If as a result of an
exothermic reaction some energy is released to a system, it has to show up in
some measurable form in terms of the state variables. An increase in the enthalpy
H = U + PV might be associated with an increase in internal energy which could
be measured by calorimeter, or with work done by the system, or a combination
of the two.
The internal energy U might be thought of as the
energy required to create a system in the absence of changes in temperature
or volume. But if the process changes the volume, as in a chemical reaction
which produces a gaseous product, then work
must be done to produce the change in volume. For a constant pressure process
the work you must do to produce a volume change ΔV is PΔV. Then the
term PV can be interpreted as the work you must do to "create room"
for the system if you presume it started at zero volume.
System Work
When work
is done by a thermodynamic system, it is usually a gas that is doing the work.
The work done by a gas at constant pressure is:
The line from a to b represents an expansion
of a gas at constant pressure. The work done is the area under the curve.
For non-constant pressure, the work can be visualized as the area under the
pressure-volume curve which represents the process taking place. The more general
expression for work done is:
The integral gives the exact area under
the curve which is equal to the work.
Work done by a system decreases the internal energy
of the system, as indicated in the First Law of Thermodynamics.
System work is a major focus in the discussion of heat engines.
Second Law of Thermodynamics
The second law of thermodynamics is a general principle which places constraints
upon the direction of
heat transfer
and the attainable efficiencies of
heat engines.
In so doing, it goes beyond the limitations imposed by the
first
law of thermodynamics.
The maximum efficiency which can be achieved is the Carnot
efficiency.
Second Law: Heat Engines
Second Law of Thermodynamics: It is impossible to
extract an amount of heat QH from a hot reservoir and use it all
to do work W. Some amount of heat QC must be exhausted to a cold
reservoir. This precludes a perfect heat
engine.
This is sometimes called the "first form"
of the second law, and is referred to as the Kelvin-Planck statement of the
second law.
Second Law: Entropy
Second Law of Thermodynamics: In any cyclic process the entropy will either
increase or remain the same:
Entropy:
a state variable whose change is defined for a reversible process at T where
Q is the heat absorbed.
Entropy: a measure of the amount of energy which is unavailable to do work.
Entropy:
a measure of the disorder of a system.
Entropy:
a measure of the multiplicity of a system.
Since entropy gives information about the evolution of an isolated system with
time, it is said to give us the direction of "time's
arrow" . If snapshots of a system at two different times shows one
state which is more disordered, then it could be implied that this state came
later in time. For an isolated system, the natural course of events takes the
system to a more disordered (higher entropy) state.
Heat Engine Processes
Heat engine processes are shown on a PV diagram.
Besides constant pressure,
volume
and temperature
processes, a useful process is the adiabatic
process where no heat
enters or leaves the system.
The Diesel Engine
The diesel internal combustion engine differs from the gasoline powered Otto
cycle by using a higher compression of the fuel to ignite the fuel rather
than using a spark plug ("compression ignition" rather than "spark
ignition").
In the diesel engine, air is compressed adiabatically
with a compression ratio typically between 15 and 20. This compression raises
the temperature to the ignition temperature of the fuel mixture which is formed
by injecting fuel once the air is compressed.
The ideal air-standard cycle is modeled as a reversible adiabatic
compression followed by a constant
pressure combustion process, then an adiabatic expansion as a power stroke
and an iso-volumetric
exhaust. A new air charge is taken in at the end of the exhaust, as indicated
by the processes a-e-a on the diagram.
Since the compression and power strokes of this
idealized cycle are adiabatic, the efficiency can be calculated from the constant
pressure and constant volume processes. The input and output energies and the
efficiency can be calculated from the temperatures and specific heats:
It is convenient to express this efficiency in terms
of the compression ratio rC = V1/V2 and the
expansion ratio rE = V1/V3. The efficiency
can be written
Now using the ideal gas law PV= n R T and g= CP/CV, this
can be written
Now using the fact that Va = Vd = V1 and Pc=Pb
from the diagram
Dividing the numerator and denominator by V1Pc
Now making use of the adiabatic condition PVg= constant,
the efficiency can be written
The Otto Engine
cv – Specific Heat constant volume γ – Specific Heat Ratio
p – pressure T – temperature
V – volume f – fuel/air ratio
Q – Fuel heating value Cps –cycles per secomd
P – power
Compression stroke: Combustion:
Power Stroke:
Work per cycle:
Engine Power:
Ideal Otto Cycle
On the figure we show a plot
of pressure
versus gas volume
throughout one cycle. We have broken the cycle into six numbered
stages based on the mechanical operation of the engine. For the ideal four
stroke engine, the intake
stroke (1-2) and exhaust
stroke (6-1) are done at constant pressure and do not contribute to the
generation of power by the engine. During the compression
stroke (2-3), work is done on the gas by the piston. If we assume that no
heat enters the gas during the compression, we know the relations
between the change in volume and the change in pressure and temperature from
our solutions of the entropy
equation for a gas. We call the ratio of the volume at the beginning of
compression to the volume at the end of compression the compression ratio,
r. Then
where p is the pressure, T is the
temperature, and γ is the ratio of specific
heats. During the combustion
process (3-4), the volume is held constant and heat is released. The change
in temperature is given
by
where Q is the heat released per pound of
fuel which depends on the fuel, f is the fuel/air ratio for combustion
which depends on several factors associated with the design and temperature
in the combustion chamber, and cv is the specific heat at constant volume.
From the equation
of state, we know that:
During the power
stroke (4-5), work is done by the gas on the piston. The expansion ratio
is the reciprocal of the compression ratio and we can use the same relations
used during the compression stroke:
Between stage 5 and stage 6, residual heat is transferred
to the surroundings so that the temperature and pressure return to the initial
conditions of stage 1 (or 2).
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. We can calculate the work by determining the area enclosed by
the cycle on the p-V diagram. But since the processes 2-3 and 4-5 are curves,
this is a difficult calculation. We can also evaluate the work W by the
difference of the heat into the gas minus the heat rejected by the gas. Knowing
the temperatures, this is an easier calculation.
The work times the rate of the cycle (cycles per
second cps) is equal to the power
P produced by the engine.
The efficiency is:
Links
http://hyperphysics.phy-astr.gsu.edu/hbase/heacon.html#heacon
http://www.grc.nasa.gov/WWW/K-12/airplane/ottoa.html
http://www.egr.msu.edu/~lira/supp/pg160expanded.pdf
http://www.tpub.com/content/engine/14037/css/14037_93.htm
http://www.engr.colostate.edu/~allan/thermo/page1/page1f.html
http://www.taftan.com/thermodynamics/
http://hyperphysics.phy-astr.gsu.edu/hbase/thermo/heatengcon.html#c1
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