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Heat Engines

Thermodynamics was invented, almost by accident, in 1825, by a young French engineer called Sadi Carnot, who was investigating the theoretical limitations on the efficiency of steam engines. Although, nowadays, we are not particularly interested in steam engines, it is still highly instructive to review some of Carnot's arguments. We know, by observation, that it is possible to do mechanical work $ w$ upon a device $ M$ , and then to extract an equivalent amount of heat $ q$ , which goes to increase the internal energy of some heat reservoir. (Here, we use the small letters $ w$ and $ q$ to denote intrinsically positive amounts of work and heat, respectively.) An good example of this process is Joule's classic experiment by which he verified the first law of thermodynamics. A paddle wheel is spun in a liquid by a falling weight, and the work done by the weight on the wheel is converted into heat, and absorbed by the liquid. Carnot's question was the following. Is it possible to reverse this process, and build a device, called a heat engine, that extracts heat energy from a reservoir, and converts it into useful macroscopic work? For instance, is it possible to extract heat from the ocean, and use it to run an electric generator?

There are a few caveats to Carnot's question. First of all, the work should not be done at the expense of the heat engine itself, otherwise the conversion of heat into work could not continue indefinitely. We can ensure that this is the case by demanding that the heat engine perform some sort of cycle, by which it periodically returns to the same macrostate, but, in the meantime, has extracted heat from the reservoir, and done an equivalent amount of useful work. A cyclic process seems reasonable, because we know that both steam engines and internal combustion engines perform continuous cycles. The second caveat is that the work done by the heat engine should be such as to change a single parameter of some external device (e.g., by lifting a weight), without doing it at the expense of affecting the other degrees of freedom, or the entropy, of that device. For instance, if we are extracting heat from the ocean to generate electricity, we want to spin the shaft of the electrical generator without increasing the generator's entropy--that is, without causing the generator to heat up, or fall to bits.

Let us examine the feasibility of a heat engine using the laws of thermodynamics. Suppose that a heat engine, $ M$ , performs a single cycle. Because $ M$ has returned to its initial macrostate, its internal energy is unchanged, and the first law of thermodynamics tell us that the work done by the engine, $ w$ , must equal the heat extracted from the reservoir, $ q$ , so that

$\displaystyle w = q.$ (6.191)

The previous condition is certainly a necessary condition for a feasible heat engine. But, is it also a sufficient condition? In other words, does every device that satisfies this condition actually work? Let us think a little more carefully about what we are actually expecting a heat engine to do. We want to construct a device that will extract energy from a heat reservoir, where it is randomly distributed over very many degrees of freedom, and convert it into energy distributed over a single degree of freedom associated with some parameter of an external device. Once we have expressed the problem in these terms, it is fairly obvious that what we are really asking for is a spontaneous transition from a probable to an improbable state, which we know is forbidden by the second law of thermodynamics. So, unfortunately, we cannot run an electric generator off heat extracted from the ocean, because this is equivalent to expecting all of the molecules in the ocean, which are moving in random directions, to all suddenly all move in the same direction, so as to exert a force on some lever, say, that can then be converted into a torque on the generator shaft. We know, from our investigation of statistical thermodynamics, that such a process--although, in principle, possible--is fantastically improbable.

The improbability of the scenario just outlined is summed up in the second law of thermodynamics, which says that the total entropy of an isolated system can never spontaneously decrease, so

$\displaystyle {\mit\Delta} S \geq 0.$ (6.192)

For the case of a heat engine, the isolated system consists of the engine, the reservoir from which it extracts heat, and the outside device upon which it does work. The engine itself returns periodically to the same state, so its entropy is clearly unchanged after each cycle. We have already specified that there is no change in the entropy of the external device upon which the work is done. On the other hand, the entropy change per cycle of the heat reservoir, which is held at absolute temperature $ T_1$ , say, is given by

$\displaystyle {\mit\Delta} S_{\rm reservoir} = \oint  \frac{{\mathchar'26\mkern-11mud}Q}{T_1} = -\frac{q}{T_1},$ (6.193)

where $  {\mathchar'26\mkern-11mud}Q$ is the infinitesimal heat absorbed by the reservoir, and the integral is taken over a whole cycle of the heat engine. The integral can be converted into the expression $ -q/T_1$ because the amount of heat extracted by the engine is assumed to be too small to modify the temperature of the reservoir (which is the definition of a heat reservoir), so that $ T_1$ is a constant during the cycle. The second law of thermodynamics reduces to

$\displaystyle \frac{-q}{T_1} \geq 0$ (6.194)

or, making use of the first law of thermodynamics,

$\displaystyle \frac{q}{T_1} = \frac{w}{T_1} \leq 0.$ (6.195)

Because we wish the work, $ w$ , done by the engine to be positive, the previous relation clearly cannot be satisfied, which proves that an engine that converts heat directly into work is thermodynamically impossible.

A perpetual motion device, which continuously executes a cycle without extracting heat from, or doing work on, its surroundings, is possible according to Equation (6.195). In fact, such a device corresponds to the equality sign in Equation (6.192), which implies that the device must be completely reversible. In reality, there is no such thing as a completely reversible engine. All engines, even the most efficient, have frictional losses that render them, at least, slightly irreversible. Thus, the equality sign in Equation (6.192) corresponds to an asymptotic limit that reality can closely approach, but never quite attain. It follows that a perpetual motion device is thermodynamically impossible. Nevertheless, the US patent office receives about 100 patent applications a year regarding perpetual motion devices. The British patent office, being slightly less open-minded that its American counterpart, refuses to entertain such applications on the basis that perpetual motion devices are forbidden by the second law of thermodynamics.

According to Equation (6.195), there is no thermodynamic objection to a heat engine that runs backwards, and converts work directly into heat. This is not surprising, because we know that this is essentially what frictional forces do. Clearly, we have, here, another example of a natural process that is fundamentally irreversible according to the second law of thermodynamics. In fact, the statement

It is impossible to construct a perfect heat engine that converts heat directly into work
is called Kelvin's formulation of the second law.

We have demonstrated that a perfect heat engine, that converts heat directly into work, is impossible. But, there must be some way of obtaining useful work from heat energy, otherwise steam engines would not operate. The reason that our previous scheme did not work was that it decreased the entropy of a heat reservoir, held at some temperature $ T_1$ , by extracting an amount of heat $ q$ per cycle, without any compensating increase in the entropy of anything else, so the second law of thermodynamics was violated. How can we remedy this situation? We still want the heat engine itself to perform periodic cycles (so, by definition, its entropy cannot increase over a cycle), and we also do not want to increase the entropy of the external device upon which the work is done. Our only other option is to increase the entropy of some other body. In Carnot's analysis, this other body is a second heat reservoir held at temperature $ T_2$ . We can increase the entropy of the second reservoir by dumping some of the heat that we extracted from the first reservoir into it. Suppose that the heat per cycle that we extract from the first reservoir is $ q_1$ , and the heat per cycle that we reject into the second reservoir is $ q_2$ . Let the work done on the external device be $ w$ per cycle. The first law of thermodynamics implies that

$\displaystyle q_1 = w + q_2.$ (6.196)

Note that if $ q_2 < q_1$ then positive (i.e., useful) work is done on the external device. The total entropy change per cycle is a consequence of the heat extracted from the first reservoir, and the heat dumped into the second, and must be positive (or zero), according to the second law of thermodynamics. So,

$\displaystyle {\mit\Delta} S = \frac{-q_1}{T_1} + \frac{q_2}{T_2} \geq 0.$ (6.197)

We can combine the previous two equations to give

$\displaystyle \frac{-q_1}{T_1} + \frac{q_1 - w}{T_2} \geq 0,$ (6.198)


$\displaystyle \frac{w}{T_2} \leq q_1\left(\frac{1}{T_2} - \frac{1}{T_1}\right).$ (6.199)

It is clear that the engine is only going to perform useful work (i.e., $ w$ is only going to be positive) if $ T_2<T_1$ . So, the second reservoir must be colder than the first if the heat dumped into the former is to increase the entropy of the universe more than the heat extracted from the latter decreases it. It is useful to define the efficiency, $ \eta$ , of a heat engine. This is the ratio of the work done per cycle on the external device to the heat energy absorbed per cycle from the first reservoir. The efficiency of a perfect heat engine is unity, but we have already shown that such an engine is impossible. What is the efficiency of a realizable engine? It is clear, from the previous equation, that

$\displaystyle \eta \equiv \frac{w}{q_1} \leq 1 - \frac{T_2} {T_1} = \frac{T_1 - T_2}{T_1}.$ (6.200)

Note that the efficiency is always less than unity. A real engine must always reject some energy into the second heat reservoir, in order to satisfy the second law of thermodynamics, so less energy is available to do external work, and the efficiency of the engine is reduced. The equality sign in the previous expression corresponds to a completely reversible heat engine (i.e., one that is quasi-static). It is clear that real engines, which are always irreversible to some extent, are less efficient than reversible engines. Furthermore, all reversible engines that operate between the two temperatures $ T_1$ and $ T_2$ have the same efficiency,

$\displaystyle \eta = \frac{T_1 - T_2}{T_1},$ (6.201)

irrespective of the manner in which they operate.

Let us consider how we might construct a reversible heat engine. Suppose that we have some gas in a cylinder equipped with a frictionless piston. The gas is not necessarily a perfect gas. Suppose that we also have two heat reservoirs held at temperatures $ T_1$ and $ T_2$ (where $ T_1 > T_2$ ). These reservoirs might take the form of large water baths. Let us start off with the gas in thermal contact with the first reservoir. We now pull the piston out, very slowly, so that heat energy flows reversibly into the gas from the reservoir. Let us now thermally isolate the gas, and slowly pull out the piston some more. During this adiabatic process, the temperature of the gas falls (because there is no longer any heat flowing into it to compensate for the work it does on the piston). Let us continue this process until the temperature of the gas falls to $ T_2$ . We now place the gas in thermal contact with the second reservoir, and slowly push the piston in. During this isothermal process, heat flows out of the gas into the reservoir. We next thermally isolate the gas a second time, and slowly compress it some more. In this process, the temperature of the gas increases. We stop the compression when the temperature reaches $ T_1$ . If we carry out each step properly then we can return the gas to its initial state, and then repeat the cycle ad infinitum. We now have a set of reversible processes by which a quantity of heat is extracted from the first reservoir, and a quantity of heat is dumped into the second. We can best evaluate the work done by the system during each cycle by plotting out the locus of the gas in a $ p$ -$ V$ diagram. The locus takes the form of a closed curve. See Figure 6.3. The net work done per cycle is the ``area'' enclosed within this curve, because $  {\mathchar'26\mkern-11mud}W = p  dV$ [if $ p$ is plotted vertically, and $ V$ horizontally, then $ p  dV$ is clearly an element of area under the curve $ p(V)$ ]. The engine we have just described is called a Carnot engine, and is the simplest conceivable device capable of converting heat energy into useful work.

Figure 6.3: An ideal-gas Carnot engine.
\epsfysize =3in

For the specific case of an ideal gas, we can actually calculate the work done per cycle, and, thereby, verify Equation (6.201). Consider the isothermal expansion phase of the gas. For an ideal gas, the internal energy is a function of the temperature alone. The temperature does not change during isothermal expansion, so the internal energy remains constant, and the net heat absorbed by the gas must equal the work it does on the piston. Thus,

$\displaystyle q_1 = \int_a^b p  dV,$ (6.202)

where the expansion takes the gas from state $ a$ to state $ b$ . Because $ p V= \nu  R T$ , for an ideal gas, we have

$\displaystyle q_1 = \int_a^b \nu R  T_1\frac{ dV}{V} = \nu  R  T_1  \ln\left(\frac{V_b}{V_a}\right).$ (6.203)

Likewise, during the isothermal compression phase, in which the gas goes from state $ c$ to state $ d$ , the net heat rejected to the second reservoir is

$\displaystyle q_2 = \nu  R  T_2  \ln\left(\frac{V_c}{V_d}\right).$ (6.204)

Now, during adiabatic expansion, or compression,

$\displaystyle T  V^{ \gamma -1} = {\rm constant}.$ (6.205)

It follows that, during the adiabatic expansion phase, which takes the gas from state $ b$ to state $ c$ ,

$\displaystyle T_1  V_b^{ \gamma -1} = T_2  V_c^{ \gamma -1}.$ (6.206)

Likewise, during the adiabatic compression phase, which takes the gas from state $ d$ to state $ a$ ,

$\displaystyle T_1  V_a^{ \gamma -1}= T_2  V_d^{ \gamma -1}.$ (6.207)

If we take the ratio of the previous two equations then we obtain

$\displaystyle \frac{ V_b}{V_a} = \frac{V_c}{V_d}.$ (6.208)

Hence, the work done by the engine, which we can calculate using the first law of thermodynamics,

$\displaystyle w = q_1 - q_2,$ (6.209)


$\displaystyle w = \nu  R   (T_1 - T_2) \ln\left(\frac{V_b}{V_a}\right).$ (6.210)

Thus, the efficiency of the engine is

$\displaystyle \eta = \frac{w}{q_1} = \frac{T_1 - T_2}{T_1}$ (6.211)

which, not surprisingly, is identical to Equation (6.201).

The engine described previously is very idealized. Of course, real engines are far more complicated than this. Nevertheless, the maximum efficiency of an ideal heat engine places severe constraints on real engines. Conventional power stations have many different ``front ends'' (e.g., coal fired furnaces, oil fired furnaces, nuclear reactors), but their ``back ends'' are all very similar, and consist of a steam driven turbine connected to an electric generator. The ``front end'' heats water extracted from a local river (say), and turns it into steam, which is then used to drive the turbine, and, hence, to generate electricity. Finally, the steam is sent through a heat exchanger, so that it can heat up the incoming river water, which means that the incoming water does not have to be heated so much by the ``front end.'' At this stage, some heat is rejected to the environment, usually as clouds of steam escaping from the top of cooling towers. We can see that a power station possesses many of the same features as our idealized heat engine. There is a cycle that operates between two temperatures. The upper temperature is the temperature to which the steam is heated by the ``front end,'' and the lower temperature is the temperature of the environment into which heat is rejected. Suppose that the steam is only heated to $ 100^\circ$ C (or 373K), and the temperature of the environment is $ 15^\circ$ C (or 288K). It follows from Equation (6.200) that the maximum possible efficiency of the steam cycle is

$\displaystyle \eta = \frac{373-288}{373} \simeq 0.23.$ (6.212)

So, at least 77% of the heat energy generated by the ``front end'' goes straight up the cooling towers. Not surprisingly, commercial power stations do not operate with $ 100^\circ$ C steam. The only way in which the thermodynamic efficiency of the steam cycle can be raised to an acceptable level is to use very hot steam (clearly, we cannot refrigerate the environment). Using $ 400^\circ$ C steam, which is not uncommon, the maximum efficiency becomes

$\displaystyle \eta = \frac{673-288}{673} \simeq 0.57,$ (6.213)

which is more reasonable. In fact, the steam cycles of modern power stations are so well designed that they come surprisingly close to their maximum thermodynamic efficiencies.

next up previous
Next: Refrigerators Up: Classical Thermodynamics Previous: Joule-Thompson Throttling
Richard Fitzpatrick 2016-01-25