Engine Cycle
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Engine Cycle

The Carnot cycle is a theoretical ideal thermodynamic cycle proposed by French physicist Sadi Carnot in 1824 and expanded upon by others in the 1830s and 1840s. It provides an upper limit on the efficiency that any classical thermodynamic engine can achieve during the conversion of heat into work, or conversely, the efficiency of a refrigeration system in creating a temperature difference by the application of work to the system. It is not an actual thermodynamic cycle but is a theoretical construct.

Every single thermodynamic system exists in a particular state. When a system is taken through a series of different states and finally returned to its initial state, a thermodynamic cycle is said to have occurred. In the process of going through this cycle, the system may perform work on its surroundings, for example by moving a piston, thereby acting as a heat engine. A system undergoing a Carnot cycle is called a Carnot heat engine, although such a "perfect" engine is only a theoretical construct and cannot be built in practice.[1] However, a microscopic Carnot heat engine has been designed and run.[2]

Essentially, there are two "heat reservoirs" forming part of the heat engine at temperatures and (hot and cold respectively). They have such large thermal capacity that their temperatures are practically unaffected by a single cycle. Since the cycle is theoretically reversible, there is no generation of entropy during the cycle; entropy is conserved. During the cycle, an arbitrary amount of entropy is extracted from the hot reservoir, and deposited in the cold reservoir. Since there is no volume change in either reservoir, they do no work, and during the cycle, an amount of heat energy is extracted from the hot reservoir and a smaller amount of waste heat is given off into the cold reservoir. The net energy is equal to the work done by the engine.

Carnot heat engine as an impractical macroscopic construct

A Carnot heat engine is a heat engine performing the Carnot cycle, and its realizations in a macroscopic scale is impractical. For example, for isothermal expansion as a part of the Carnot cycle, the following conditions are required to be satisfied simultaneously at every step in the expansion to realize it.[3]

  • The hot reservoir temperature TH is infinitesimally higher than the system gas temperature T so heat flow (energy transfer) from the hot reservoir to the gas is made without increasing T (via infinitesimal work on the surroundings by the gas as another energy transfer); if TH is significantly higher than T, then T may be not uniform through the gas so the system is deviated from the thermal equilibrium as well as a reversible process (no more Carnot cycle) or T may increase noticeably so it is no more isothermal process.
  • The force externally applied on the piston (opposite to the internal force on the piston by the gas) needs to be infinitesimally reduced somehow. Without this external assistance, following a gas PV (Pressure-Volume) curve at a constant T downwardly is not possible since following this curve means that the gas-to-piston force decreases (P decrease) as the surroundings expands (the piston moving outwardly). If this assistance is strong so that surroundings expansion is significant, then the system may be deviated from the thermal equilibrium as well as the reversible process (no more Carnot cycle).

These (and other) "infinitesimal" requirements makes the Carnot's cycle to be performed over an infinite amount of time. There are other practical requirements that make the Carnot cycle hard to be realized (e.g., fine control of gas thermal contact with the surroundings including high and low temperature reservoirs), so the Carnot engine should be thought as a theoretical limit of macroscopic scale heat engines rather than a practical achievement goal.

Stages

The Carnot cycle as an idealized thermodynamic cycle performed by a heat engine (Carnot heat engine) consists of the following steps.

  1. Carnot Cycle Figure - Step 1.jpg

    Isothermal expansion. Heat (as an energy) is transferred reversibly from high temperature reservoir at constant temperature TH to the gas at temperature infinitesimally less than TH (to allow heat transfer to the gas without practically changing the gas temperature so isothermal heat addition or absorption). During this step (1 to 2 on Figure 1, A to B in Figure 2), the gas is thermally in contact with the high temperature reservoir and the gas is allowed (by somehow) to expand, doing work on the surroundings by gas pushing up the piston (stage 1 figure, right). Although the pressure drops from points 1 to 2 (figure 1) the temperature of the gas does not change during the process because the heat transferred from the hot temperature reservoir to the gas is exactly used to do work on the surroundings by the gas, so no gas internal energy changes (no gas temperature change for an ideal gas). Heat QH > 0 is absorbed from the high temperature reservoir, resulting in an increase in the entropy of the gas by the amount .

  2. Carnot Cycle Figure - Step 2.png

    Isentropic (reversible adiabatic) expansion of the gas (isentropic work output). For this step (2 to 3 on Figure 1, B to C in Figure 2) the gas in the engine is thermally insulated from both the hot and cold reservoirs, thus they neither gain nor lose heat, an 'adiabatic' process. The gas continues to expand with reduction of its pressure, doing work on the surroundings (raising the piston; stage 2 figure, right), and losing an amount of internal energy equal to the work done. The gas expansion without heat input causes the gas to cool to the "cold" temperature (by losing its internal energy), that is infinitesimally higher than the cold reservoir temperature TC. The entropy remains unchanged as no heat Q transfers (Q = 0) between the system (the gas) and its surroundings, so an isentropic process, meaning no entropy change in the process).

  3. Carnot Cycle Figure - Step 3.png

    Isothermal compression. Heat transferred reversibly to low temperature reservoir at constant temperature TC (isothermal heat rejection). In this step (3 to 4 on Figure 1, C to D on Figure 2), the gas in the engine is in thermal contact with the cold reservoir at temperature TC and the gas temperature is infinitesimally higher than this temperature (to allow heat transfer from the gas to the cold reservoir without practically changing the gas temperature). The surroundings do work on the gas, pushing the piston down (stage 3 figure, right). An amount of energy earned by the gas from this work exactly transfers as a heat energy QC < 0 (negative as leaving from the system, according to the universal convention in thermodynamics) to the cold reservoir so the entropy of the system decreases by the amount .[4] because the isothermal compression decreases the multiplicity of the gas.

  4. Carnot Cycle Figure - Step 4.png

    Isentropic compression. (4 to 1 on Figure 1, D to A on Figure 2) Once again the gas in the engine is thermally insulated from the hot and cold reservoirs, and the engine is assumed to be frictionless and the process is slow enough, hence reversible. During this step, the surroundings do work on the gas, pushing the piston down further (stage 4 figure, right), increasing its internal energy, compressing it, and causing its temperature to rise back to the temperature infinitesimally less than TH due solely to the work added to the system, but the entropy remains unchanged. At this point the gas is in the same state as at the start of step 1.

Figure 1: A Carnot cycle illustrated on a PV diagram to illustrate the work done. 1-to-2 (isothermal expansion), 2-to-3 (isentropic expansion), 3-to-4 (isothermal compression), 4-to-1 (isentropic compression).

In this case, since it is a reversible thermodynamic cycle (no net change in the system and its surroundings per cycle)[5][4]

,

or,

.

This is true as and are both smaller in magnitude and in fact are in the same ratio as .

The pressure-volume graph

When the Carnot cycle is plotted on a pressure-volume diagram (Figure 1), the isothermal stages follow the isotherm lines for the working fluid, the adiabatic stages move between isotherms, and the area bounded by the complete cycle path represents the total work that can be done during one cycle. From point 1 to 2 and point 3 to 4 the temperature is constant (isothermal process). Heat transfer from point 4 to 1 and point 2 to 3 are equal to zero (adiabatic process).

Properties and significance

The temperature-entropy diagram

Figure 2: A Carnot cycle as an idealized thermodynamic cycle performed by a heat engine (Carnot heat engine), illustrated on a TS (temperature T-entropy S) diagram. The cycle takes place between a hot reservoir at temperature TH and a cold reservoir at temperature TC. The vertical axis is the system temperature, the horizontal axis is the system entropy. A-to-B (isothermal expansion), B-to-C (isentropic expansion), C-to-D (isothermal compression), D-to-A (isentropic compression).
Figure 3: A generalized thermodynamic cycle taking place between a hot reservoir at temperature TH and a cold reservoir at temperature TC. By the second law of thermodynamics, the cycle cannot extend outside the temperature band from TC to TH. The area in red, |QC|, is the amount of energy exchanged between the system and the cold reservoir. The area in white, W, is the amount of work energy exchanged by the system with its surroundings. The amount of heat exchanged with the hot reservoir is the sum of the two. If the system is behaving as an engine, the process moves clockwise around the loop, and moves counter-clockwise if it is behaving as a refrigerator. The efficiency to the cycle is the ratio of the white area (work) divided by the sum of the white and red areas (heat absorbed from the hot reservoir).

The behavior of a Carnot engine or refrigerator is best understood by using a temperature-entropy diagram (T-S diagram), in which the thermodynamic state is specified by a point on a graph with entropy (S) as the horizontal axis and temperature (T) as the vertical axis (Figure 2). For a simple closed system (control mass analysis), any point on the graph represents a particular state of the system. A thermodynamic process is represented by a curve connecting an initial state (A) and a final state (B). The area under the curve is:

 

 

 

 

which is the amount of thermal energy (heat) transferred in the process. If the process moves to greater entropy (e.g., moving from a lesser entropy point A to a greater entropy point B in the integral above), the area under the curve is the amount of heat absorbed by the system in that process. If the process moves towards lesser entropy, it is the amount of heat removed or leaving from the system. For any cyclic process, there is an upper portion of the cycle and a lower portion. In T-S diagrams for a clockwise cycle, the area under the upper portion will be the thermal energy absorbed by the system during the cycle, while the area under the lower portion will be the thermal energy removed from the system during the cycle. The area inside the cycle is then the difference between the two (the absorbed net heat energy), but since the internal energy of the system must have returned to its initial value, this difference must be the amount of work done by the system per cycle. Referring to Figure 1, mathematically, for a reversible process, we may write the amount of work done over a cyclic process as:

 

 

 

 

Since dU is an exact differential, its integral over any closed loop is zero and it follows that the area inside the loop on a T-S diagram is equal to the total work performed by the system on the surroundings if the loop is traversed in a clockwise direction, and is equal to the total work done on the system by the surroundings as the loop is traversed in a counterclockwise direction.

Figure 4: A Carnot cycle taking place between a hot reservoir at temperature TH and a cold reservoir at temperature TC.

The Carnot cycle

Figure 5: A visualization of the Carnot cycle

Evaluation of the above integral is particularly simple for the Carnot cycle. The amount of energy transferred as work is

The total amount of thermal energy transferred from the hot reservoir to the system will be

and the total amount of thermal energy transferred from the system to the cold reservoir will be

Due to energy conservation, the net heat transferred, , is equal to the work performed[4]

The efficiency is defined to be:

 

 

 

 

where

W is the work done by the system (energy exiting the system as work),
< 0 is the heat taken from the system (heat energy leaving the system),
> 0 is the heat put into the system (heat energy entering the system),
is the absolute temperature of the cold reservoir, and
is the absolute temperature of the hot reservoir.
is the maximum system entropy
is the minimum system entropy

This definition of efficiency makes sense for a heat engine, since it is the fraction of the heat energy extracted from the hot reservoir and converted to mechanical work. A Rankine cycle is usually the practical approximation.

Reversed Carnot cycle

The Carnot heat-engine cycle described is a totally reversible cycle. That is, all the processes that compose it can be reversed, in which case it becomes the Carnot heat pump and refrigeration cycle. This time, the cycle remains exactly the same except that the directions of any heat and work interactions are reversed. Heat is absorbed from the low-temperature reservoir, heat is rejected to a high-temperature reservoir, and a work input is required to accomplish all this. The P-V diagram of the reversed Carnot cycle is the same as for the Carnot heat-engine cycle except that the directions of the processes are reversed.[6]

Carnot's theorem

It can be seen from the above diagram that for any cycle operating between temperatures and , none can exceed the efficiency of a Carnot cycle.

Figure 6: A real engine (left) compared to the Carnot cycle (right). The entropy of a real material changes with temperature. This change is indicated by the curve on a T-S diagram. For this figure, the curve indicates a vapor-liquid equilibrium (See Rankine cycle). Irreversible systems and losses of energy (for example, work due to friction and heat losses) prevent the ideal from taking place at every step.

Carnot's theorem is a formal statement of this fact: No engine operating between two heat reservoirs can be more efficient than a Carnot engine operating between those same reservoirs. Thus, Equation 3 gives the maximum efficiency possible for any engine using the corresponding temperatures. A corollary to Carnot's theorem states that: All reversible engines operating between the same heat reservoirs are equally efficient. Rearranging the right side of the equation gives what may be a more easily understood form of the equation, namely that the theoretical maximum efficiency of a heat engine equals the difference in temperature between the hot and cold reservoir divided by the absolute temperature of the hot reservoir. Looking at this formula an interesting fact becomes apparent: Lowering the temperature of the cold reservoir will have more effect on the ceiling efficiency of a heat engine than raising the temperature of the hot reservoir by the same amount. In the real world, this may be difficult to achieve since the cold reservoir is often an existing ambient temperature.

In other words, maximum efficiency is achieved if and only if no new entropy is created in the cycle, which would be the case if e.g. friction leads to dissipation of work into heat. In that case, the cycle is not reversible and the Clausius theorem becomes an inequality rather than an equality. Otherwise, since entropy is a state function, the required dumping of heat into the environment to dispose of excess entropy leads to a (minimal) reduction in efficiency. So Equation 3 gives the efficiency of any reversible heat engine.

In mesoscopic heat engines, work per cycle of operation in general fluctuates due to thermal noise. If the cycle is performed quasi-statically, the fluctuations vanish even on the mesoscale.[7] However, if the cycle is performed faster than the relaxation time of the working medium, the fluctuations of work are inevitable. Nevertheless, when work and heat fluctuations are counted, an exact equality relates the exponential average of work performed by any heat engine to the heat transfer from the hotter heat bath.[8]

Efficiency of real heat engines

See also: Heat engine efficiency and other performance criteria

Carnot realized that in reality it is not possible to build a thermodynamically reversible engine, so real heat engines are even less efficient than indicated by Equation 3. In addition, real engines that operate along this cycle are rare. Nevertheless, Equation 3 is extremely useful for determining the maximum efficiency that could ever be expected for a given set of thermal reservoirs.

Although Carnot's cycle is an idealization, the expression of Carnot efficiency is still useful. Consider the average temperatures,

at which heat is input and output, respectively. Replace TH and TC in Equation (3) by ⟨TH⟩ and ⟨TC⟩, respectively.

For the Carnot cycle, or its equivalent, the average value ⟨TH⟩ will equal the highest temperature available, namely TH, and ⟨TC⟩ the lowest, namely TC. For other, less efficient cycles, ⟨TH⟩ will be lower than TH, and ⟨TC⟩ will be higher than TC. This can help illustrate, for example, why a reheater or a regenerator can improve the thermal efficiency of steam power plants--and why the thermal efficiency of combined-cycle power plants (which incorporate gas turbines operating at even higher temperatures) exceeds that of conventional steam plants. The first prototype of the diesel engine was based on the Carnot cycle.

See also

References

Notes
  1. ^ Nicholas Giordano (13 February 2009). College Physics: Reasoning and Relationships. Cengage Learning. p. 510. ISBN 978-0-534-42471-8.
  2. ^ Ignacio A. Martínez; et al. (6 January 2016). "Brownian Carnot engine". Nature Physics. pp. 67-70.
  3. ^ D, Bob (15 January 2020). "In the isothermal expansion phase of a Carnot cycle, why does the gas expand?". StackExchange. Retrieved 2022.{{cite web}}: CS1 maint: url-status (link)
  4. ^ a b c Planck, M. (1945). "equations 39, 40 and 65 in sections §90 & §137". Treatise on Thermodynamics. Dover Publications. pp. 75, 135.
  5. ^ Fermi, E. (1956). "equation 64". Thermodynamics (PDF). Dover Publications. p. 48.
  6. ^ Çengel, Yunus A., and Michael A. Boles. Thermodynamics: An Engineering Approach. 7th ed. New York: McGraw-Hill, 2011. p. 299. Print.
  7. ^ Holubec Viktor and Ryabov Artem (2018). "Cycling Tames Power Fluctuations near Optimum Efficiency". Phys. Rev. Lett. 121 (12): 120601. arXiv:1805.00848. Bibcode:2018PhRvL.121l0601H. doi:10.1103/PhysRevLett.121.120601. PMID 30296120. S2CID 52943273.
  8. ^ N. A. Sinitsyn (2011). "Fluctuation Relation for Heat Engines". J. Phys. A: Math. Theor. 44 (40): 405001. arXiv:1111.7014. Bibcode:2011JPhA...44N5001S. doi:10.1088/1751-8113/44/40/405001. S2CID 119261929.
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