A Contemporary View on Carnot’s Réflexions
<p>Visibly boiling water is poured into a beaker filled with crushed ice. After stirring, the mixture is ice-cold. The result cannot be explained by temperature alone because the temperature in the beaker remains constant at 0 °C.</p> "> Figure 2
<p>Conception of the physical quantity of entropy based on the preliminary term caloric (caloricum, calorique) and the general term irreversibility.</p> "> Figure 3
<p>(<b>a</b>) Carnot separates the flow of calorique from a hot reservoir (red) to a cold reservoir (blue) into two fundamentally different channels: reversible flow through the reversible engine and irreversible flow through direct contact. (<b>b</b>) Replacing calorique with entropy requires a change in the irreversible flow, and entropy is generated. (<b>c</b>) For the sake of simplicity, only the upper part of (<b>b</b>) is often shown in textbooks. This obscures the intelligent separation of reversible from irreversible entropy flow.</p> "> Figure 4
<p>Waterfall analogy. The shaft of a water mill is driven by the mass of water falling from a height of <math display="inline"><semantics> <msub> <mi>h</mi> <mn>1</mn> </msub> </semantics></math> to a lower height (<math display="inline"><semantics> <msub> <mi>h</mi> <mn>2</mn> </msub> </semantics></math>). In the same way, the fall of entropy from temperature <math display="inline"><semantics> <msub> <mi>T</mi> <mn>1</mn> </msub> </semantics></math> to a lower temperature (<math display="inline"><semantics> <msub> <mi>T</mi> <mn>2</mn> </msub> </semantics></math>) drives the shaft of a heat engine.</p> "> Figure 5
<p>Idealized water mill process for a wheel height of <span class="html-italic">h</span>. The bucket is filled at maximum height from state A to state B; then, the water descends (B–C) and pours out of the bucket at a minimum height (C–D). The empty bucket is raised again (D–A). For Carnot’s idealized heat engine, there is isothermal heating from A to B, adiabatic expansion (B–C), isothermal cooling (C–D), and adiabatic compression (D–A). The motive power of a reversible water mill is proportional to the mass flow and the height difference. Therefore, the area in the <math display="inline"><semantics> <mrow> <mi>h</mi> <mo>,</mo> <mi>m</mi> </mrow> </semantics></math> diagram is proportional to the motive power. Similarly, the area in the <math display="inline"><semantics> <mrow> <mi>T</mi> <mo>,</mo> <mi>S</mi> </mrow> </semantics></math> diagram is proportional to the motive power of a reversible heat engine.</p> "> Figure 6
<p>Definition of isentropic efficiency (<math display="inline"><semantics> <msub> <mi>η</mi> <mi>S</mi> </msub> </semantics></math>). The heat reservoirs contain a mixture of liquid and solids, for example, tin (505 K, red) and water (273 K, blue). The amount of entropy entering the heat engine can be determined by the mass of the solidified substance in the hot reservoir. Note that Carnot did not demand infinite reservoirs—only constant temperatures. Our suggestion of finite reservoirs based on phase mixtures is a valid development of Carnot’s concept.</p> "> Figure 7
<p>The diffusion of hot flame gases after touching the inlet of a heat engine, such as a Stirling engine, is an obvious loss. The fall of entropy is reduced when the flame gases are cooled due to more efficient entropy transfer at the hot end of the heat engine.</p> "> Figure 8
<p>Gas turbine cycle. (<b>a</b>) Flow in a hypothetical closed-cycle gas turbine. The compressor is driven by the expander turbine on the same shaft in a real turbine. (<b>b</b>) Temperature and pressure as a function of the path through the closed tube.</p> "> Figure 9
<p>Countercurrent heat exchange. The upper fluid stream on the right and the lower fluid stream on the left cannot mix but are in contact with thin metal sheet (gray). At each point of the sheet, the temperature is slightly higher in the upper stream than in the lower stream. Therefore, entropy flows from top to bottom (white arrows).</p> "> Figure 10
<p>(<b>a</b>) Water and steam flow in an idealized steam turbine. (<b>b</b>) Corresponding Clausius–Rankine cycle in the <math display="inline"><semantics> <mrow> <mi>T</mi> <mo>,</mo> <mi>S</mi> </mrow> </semantics></math> diagram. At point D, water is at low pressure and low temperature. The feed pump raises the pressure with a barely noticeable increase in temperature at point A. The water temperature increases by absorption of entropy in the countercurrent heat exchanger until the boiling temperature is reached at A’. Further entropy is absorbed during evaporation until the fully gaseous state is reached at B. Adiabatic expansion lowers the temperature to near ambient temperature (C) without changing the entropy. Entropy is discharged to a river or cooling tower at ambient temperature until the cycle is completed in D.</p> "> Figure 11
<p>Clausius–Rankine cycle in the <math display="inline"><semantics> <mrow> <mi>T</mi> <mo>,</mo> <mi>s</mi> </mrow> </semantics></math> diagram at 1 MPa pressure. (<b>a</b>) A cycle based on steam at the boiling temperature does not work because after adiabatic expansion to point C, the the water-droplet content in the wet steam is much too high. (<b>b</b>) After heating the steam the maximum temperature of 850 K, the steam contains sufficient entropy to reach the phase boundary after adiabatic expansion to 310 K. The unit of entropy is named Carnot (Ct) [<a href="#B3-entropy-26-01002" class="html-bibr">3</a>,<a href="#B11-entropy-26-01002" class="html-bibr">11</a>]. Energy is not introduced yet; therefore, the common unit of J/K is not appropriate, and kgm<sup>2</sup>s<sup>−2</sup>K<sup>−1</sup> seems too complicated for a basic quantity. As in the technical literature, the specific entropy (<span class="html-italic">s</span>) in Ct/mol is used on the axis of abscissas.</p> "> Figure 12
<p>Clausius–Rankine cycle at 25 MPa pressure. (<b>a</b>) Compared to the situation in <a href="#entropy-26-01002-f011" class="html-fig">Figure 11</a>b, the maximum temperature is reached at lower specific entropy. Therefore, the same problem of excessive liquid water content in the cold steam arises. (<b>b</b>) Intermediate expansion to the vicinity of the phase boundary and subsequent heating to the maximum temperature, again, shift the vertical line to a higher entropy value. During adiabatic expansion, the phase line is crossed. Whether such a small proportion of liquid water is tolerable or a second intermediate heating becomes necessary is decided by real steam turbine experts.</p> "> Figure 13
<p><math display="inline"><semantics> <mrow> <mi>T</mi> <mo>,</mo> <mi>s</mi> </mrow> </semantics></math> diagram for the gas turbine (light gray) and steam turbine (dark gray) of a combined cycle engine. Minimizing the gap between the two areas in the figure is an obvious requirement.</p> "> Figure 14
<p>Fall of entropy of a reversible heat engine (arrow down) and heat pump (arrow up). The temperature values of 310 K (37 °C) and 280 K (7 °C) are theoretical values for room heating and ambient temperature, respectively, not technical values. (<b>a</b>) A heat pump is driven by a reversible heat engine. (<b>b</b>) The current of the entropy fall, represented by the width of the rectangle, is increased to the current of the reverse entropy fall of the heat pump. The reversible heat engine supplies additional electricity to the power distribution network. The entropy flow of the engine is divided into an upper part and a lower part. We imagine a high-temperature turbine and a low-temperature turbine for the temperature interval pf 310 K to 280 K, but this is not mandatory for the argument. The low-temperature part of the entropy flow of the engine is used to pump the entropy back to the temperature of 310 K. (<b>c</b>) Since all machines are reversible, the low-temperature engine/pump combination can be removed. Instead, an entropy flow of the same magnitude can be fed directly into the space heating system. This is the principle of cogeneration.</p> "> Figure 15
<p>Different energy influxes (<math display="inline"><semantics> <mrow> <mi>d</mi> <msub> <mi>E</mi> <mn>1</mn> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>d</mi> <msub> <mi>E</mi> <mn>2</mn> </msub> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <mi>d</mi> <msub> <mi>E</mi> <mn>3</mn> </msub> </mrow> </semantics></math>) into an open system (dashed line) are balanced by an energy outflux (<math display="inline"><semantics> <mrow> <mi>d</mi> <msub> <mi>E</mi> <mn>4</mn> </msub> </mrow> </semantics></math>). The amount of energy within the open system is constant if the sum of energy fluxes is zero: <math display="inline"><semantics> <mrow> <msub> <mo>∑</mo> <mi>i</mi> </msub> <mrow> <mi>d</mi> <msub> <mi>E</mi> <mi>i</mi> </msub> <mo>=</mo> <mn>0</mn> </mrow> </mrow> </semantics></math>. Many elementary physics books formulate a special case in which energy is constant in a closed system, as shown on the right. This case is more convenient for physicists who have the freedom to define a sufficiently large enclosure but less useful for engineers, who have to deal with open systems in reality.</p> "> Figure 16
<p>A thermal resistor is assumed as a cause of irreversible temperature reduction. The entropy produced in the thermal resistor increases the entropy current into the engine, ass represented by an increased width of area <math display="inline"><semantics> <msub> <mi>A</mi> <mn>1</mn> </msub> </semantics></math>.</p> ">
Abstract
:1. Introduction
2. Entropy as Quantity of Heat
2.1. Difference to Energy
2.2. Latent Heat
2.3. Irreversible Process
2.4. Conceptual Change Towards Entropy
3. Foundation of Carnot’s Réflexions
3.1. Calorique as a Precursor of Entropy
3.2. Waterfall Analogy
3.3. Statement on Efficiency Without Energy
4. Combustion Engines
- Flame reaction;
- Thermal diffusion of hot flame gases;
- Thermal diffusion of hot exhaust gasses;
- Heat conduction at the inlet;
- Heat conduction at the outlet;
- Friction due to the viscosity of the medium;
- The turbulence of the medium;
- Leakage of the medium, mainly in turbines;
- Mechanical friction;
- Turbulence of the exhaust gas;
- General operation of the engine.
4.1. Stirling Engine
4.2. Gas Turbine as Prototype of a Combustion Engine
4.3. Steam Turbine
4.4. Combined Cycle Turbine
5. Heat Pump
6. Energy
6.1. Quantitative Comparison
6.2. Energy Conservation
6.3. Energy Consumption or Degradation
6.4. Energy Supply
7. Energy Analysis of Heat Engines
7.1. Physical Origin of Non-Unity Efficiency
7.2. Utilization of Entropy Generated by Diffusion
7.3. Endoreversible Engines
8. Discussion
Funding
Institutional Review Board Statement
Data Availability Statement
Conflicts of Interest
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Meyn, J.-P. A Contemporary View on Carnot’s Réflexions. Entropy 2024, 26, 1002. https://doi.org/10.3390/e26121002
Meyn J-P. A Contemporary View on Carnot’s Réflexions. Entropy. 2024; 26(12):1002. https://doi.org/10.3390/e26121002
Chicago/Turabian StyleMeyn, Jan-Peter. 2024. "A Contemporary View on Carnot’s Réflexions" Entropy 26, no. 12: 1002. https://doi.org/10.3390/e26121002
APA StyleMeyn, J.-P. (2024). A Contemporary View on Carnot’s Réflexions. Entropy, 26(12), 1002. https://doi.org/10.3390/e26121002