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A detailed analysis for different heat transfer laws in the Carnot-like model in terms of maximum power efficiency given by the low-dissipation model is also presented. In irreversible Carnot-like HE, the entropy generation of the internal reversible loop is zero and the total entropy output is that generated in the external heat reservoirs (see Figure 1b).

Figure 1. (a) Sketch of a low dissipation heat engine characterized by entropy generation laws ΔS T h and ΔS T c ; (b) Sketch of an irreversible Carnot-like heat engine characterized by generic heat transfers Q h , Q c and Q L .
Figure 1. (a) Sketch of a low dissipation heat engine characterized by entropy generation laws ΔS T h and ΔS T c ; (b) Sketch of an irreversible Carnot-like heat engine characterized by generic heat transfers Q h , Q c and Q L .

Physical Space of the HE Variables

In [41], the region of physical interest in the LD model under maximum power conditions was analyzed. Then, as long as there is a heat leak in the device, the internal hot reservoir cannot reach equilibrium with the external hot reservoir, and the reversible configuration is not achievable.

Figure 3. Possible values of Q  L as a function of the control parameters α and  t. We used the values  Σ c = 0.8 and τ = 0.2.
Figure 3. Possible values of Q L as a function of the control parameters α and t. We used the values Σ c = 0.8 and τ = 0.2.

Maximum-Power Regime

It is well known that, for the Newtonian heat transfer law (k=1),ηPmax =ηCA is independent of theσhc value. Another incompatibility of the two approaches occurs in the Newtonian heat exchange (k =1): meanwhile, the Carnot-like scheme ηCA is independent of any value of σhc, and, in terms of the LD model, ηCA is strictly attached to a symmetric dissipationΣc=1/2(=Σh).

Figure 4. (a) upper and lower bounds of the MP efficiency in terms of the exponent of the heat transfer law k of the Carnot-like heat engine; (b) the  Σ c values that reproduce the upper and lower bounds of the endoreversible engine.
Figure 4. (a) upper and lower bounds of the MP efficiency in terms of the exponent of the heat transfer law k of the Carnot-like heat engine; (b) the Σ c values that reproduce the upper and lower bounds of the endoreversible engine.

Conclusions

Irreversibilities and efficiencies at maximum power of heat engines: The illustrative case of a thermoelectric generator. Phys. Constitutive relation for nonlinear response and universality of efficiency at maximum power for tight-coupled heat engines. Phys.

Figure 7. (a) Physically well behaved region of the α– Σ  c variables. The shaded areas come from the LD model and the dashed curves come from the Carnot-like model; (b) The same for the  t– Σ c variables.
Figure 7. (a) Physically well behaved region of the α– Σ c variables. The shaded areas come from the LD model and the dashed curves come from the Carnot-like model; (b) The same for the t– Σ c variables.

The History and Perspectives of Efficiency at Maximum Power of the Carnot Engine

  • Introduction
  • Finite Time Thermodynamics
  • Steady-State Modelling 1. Heat Transfer Conductance Model
  • Transient Modelling
  • Conclusions and Perspectives

This proves that the Carnot efficiency is the upper bound on the efficiency of the adiabatic and reversible system (two thermostats and the converter). All the previous results are related to the linear form of the heat transfer law (equation (10)).

Figure 1. Extract from Moutier’s book [6] (p. 62).
Figure 1. Extract from Moutier’s book [6] (p. 62).

Global Efficiency of Heat Engines and Heat Pumps with Non-Linear Boundary Conditions

Method

This approach is proposed in Öhman [6] for comparing the global energy efficiency of different real heat engines. For the correlation of global energy efficiency of a real heat engine, it is possible to define a "Fraction of Carnot" (FoC) from Equation (6).

Results

Evaluation of heat pump systems can be made in a similar way to the above by defining Equation (9) as a fraction of Carnot for real heat pumps. The approach of the maximum power cycle, Integrated Local Carnot efficiency and Fraction of Carnot are useful in such studies.

Table 1. Input information for a demonstrational example.
Table 1. Input information for a demonstrational example.

Discussion

QCA Curzon–Ahlborn rate of heat transferred from the hot flow W αH, αL Inverse apparent heat capacity of hot and cold flow K/W. CpH,CpL Constant, linear specific heat capacity of hot and cold flow J/kg·K C(T) Non-constant, complex specific heat capacity J/kg·K.

What Is the Real Clausius Statement of the Second Law of Thermodynamics?

Misunderstanding of the Clausius Statement 1. Carnot’s Theorem

Clausius pointed out that the second law of thermodynamics in his mechanical theory of heat is called the theorem of equivalence of transformations. Therefore, the true Clausius statement of the second law should be the equivalence theorem of transformations. The theorem on equivalence of transformations is a basic theory of classical thermodynamics and it is necessary to be fully aware of it.

In the next section, we will see that Clausius' equality/inequality and the concept of entropy were derived from the equivalence theorem of transformations [24].

Figure 1. p-V diagram of a thermodynamic cycle with three heat reservoirs.
Figure 1. p-V diagram of a thermodynamic cycle with three heat reservoirs.

Alternative Mathematic Expression of the Second Law 1. Clausius Equality / Inequality and Entropy

So the sum of the equivalence values ​​of all transformations in a reversible cycle must be zero. Fortunately, Clausius identified the Carnot function and further obtained the thermal efficiency of a Carnot cycle in terms of the equivalence of transformations theorem. For a Carnot cycle with two different heat source temperatures, the thermal efficiency can also be derived directly from the equivalence of the transformations theorem.

Therefore, it can perhaps be perceived as an alternative mathematical expression of the second law of thermodynamics.

Figure 2. T-S diagram of an infinitesimal Carnot cycle.
Figure 2. T-S diagram of an infinitesimal Carnot cycle.

Conclusions

Fenn, J.B. Engines, Energy and Entropy: An Introduction to Thermodynamics (Global View); Freeman: New York, NY, USA, 1982; pp. The efficiency of compressor heat pumps and refrigerators comes from the second law of thermodynamics. Int.

Performance of a Simple Energetic-Converting Reaction Model Using Linear Irreversible

The Model

In the classical equations of chemical kinetics, which are known to describe a chemical process quite accurately, reaction rates are proportional to concentrations. Thus, this energy may be different for the different stages of the enzymatic reaction, causing the phenomenological coefficients to be different, and the degree of coupling qi to be different in each stage as well, which affects the thermodynamic properties of the system (e.g. power output or entropy production). Furthermore, Figure 2 shows the efficiency plotted as a function of the stoichiometric coefficient for different values ​​of q.

Optimal operating regimes in the context of linear irreversible thermodynamics. A very interesting problem in many biological systems is the transfer of energy, which is essential.

Figure 1. Chemical potential scheme necessary for the reactions in Equation (1) to proceed forward.
Figure 1. Chemical potential scheme necessary for the reactions in Equation (1) to proceed forward.

Optimal Operation Regimes in the Context of the Linear Irreversible Thermodynamics A very interesting problem in many biological systems is the transfer of energy which is of decisive

In the context of linear irreversible thermodynamics, the efficient power function takes the form, . In the context of linear irreversible thermodynamics, the latter is interesting in the sense that we can compare not only the power output but also the cycle efficiency. Characteristic functions (P Maximum Power Output (MPO), Maximum Ecological Function (MEF) and PeMaximum Efficient Power Function (MEPF)) as a function of efficiency.

Later shows how important the parameter q is as it reflects the behavior of the irreversibilities in the system (see Figure 5-7).

Figure 3. This Figure shows the entropy production σ versus the stoichiometric coefficient x
Figure 3. This Figure shows the entropy production σ versus the stoichiometric coefficient x

Concluding Remarks

We can observe how the Power Efficient Function produces loop-like curves as seen in real heat engines. Now, from equations and (35), it is clear that the efficiency that maximizes some of the characteristic functions is related only to q, so in the end, the thermodynamic properties are related to the degree of coupling providing the basis for comparing different types of coupling in a two-flow system. Efficiency at peak power: A solvable analytical model for stochastic heat engines. EPL (Europhys. Lett.

Timed rate controller: optimal efficiency for maximum power output in physical and biological systems. Am.

Progress in Carnot and Chambadal Modeling of Thermomechanical Engine by Considering Entropy

The Chambadal Engine

The temperature difference of the source and sink levels, ΔTS, compared to the cyclic liquid level, ΔTCF, which remains the same, is also relevant for the heat input in the two cases. When the source has a finite heat capacity, there is a temperature variation of the primary fluid in the associated heat exchanger. By following several assumptions one can consider:. i) the presence of Novikov's degree of irreversibility [9], which is expressed by:.

Influence of the working fluid properties on optimized power of an irreversible finite dimensions Carnot engine.Energy Convers.

OTEC Maximum Net Power Output Using Carnot Cycle and Application to Simplify Heat

Exchanger Selection

Description and Analysis

In this study, the comparison of the heat exchangers is based on the net power supplied by the plant per unit of heat exchanger surface. Part of the gross power generated by the power plant is used for water pipes. The heat transfer coefficient of the working fluid is much greater than that of seawater, as the working fluid undergoes a phase change [24].

It was assumed that the working fluid at the exit from the heat exchangers is in a saturated state.

Figure 1. (a) Model of the ocean thermal energy conversion (OTEC) system and (b) temperature–entropy diagram of a Carnot cycle.
Figure 1. (a) Model of the ocean thermal energy conversion (OTEC) system and (b) temperature–entropy diagram of a Carnot cycle.

Optimization Process

In addition, Uehara and Ikegami showed a 44% reduction in the net power output of an OTEC plant for the same temperature change [23]. As for the Carnot cycle, the results for the Rankine cycle show that the temperature change will significantly affect the maximum net power output of the OTEC plant. An objective function of the net power output per unit area of ​​the heat exchanger was defined for the Carnot and Rankine cycles.

The evolution of the output power as a function of the temperature difference was found to follow the same trends as found in other studies.

Table 2. Coefficients for the Nusselt numbers and friction factor correlations.
Table 2. Coefficients for the Nusselt numbers and friction factor correlations.

Energy and Exergy Evaluation of a Two-Stage Axial Vapour Compressor on the LNG Carrier

  • Description and Characteristics of the Analyzed Two-Stage Compressor
  • Measuring Equipment and Measuring Results
  • Thermodynamic Efficiency Analysis
  • Energy and Exergy Analysis Results and Discussion
  • Variation and Optimization of Temperature at the Compressor’s Second Stage Inlet
  • Conclusions

The schematic overview of the two-stage compressor is shown in Figure 1, where p1,t1 is the LNG vapor pressure and temperature at the compressor inlet to the first stage. The energy efficiency of the first stage compressor is higher than that of the second stage and averages around 52%. The exergy efficiency is smoothly increased throughout the range for the second stage of the compressor.

The energy efficiency of the two-phase compressor in the observed range, in the beginning, is 50.7%.

Table 1. Overview of compressor mass flow rate, working medium and assumed efficiencies.
Table 1. Overview of compressor mass flow rate, working medium and assumed efficiencies.

Second Law Analysis for the Experimental

Performances of a Cold Heat Exchanger of a Stirling Refrigeration Machine

Experimental Setup

The displacement piston function is to displace the gas between the hot and cold parts of the machine. The function of the regenerator is to store the heat from the liquid during one of the isochoric transformations of the cycle and to restore it in the other. The lower part of the machine, called the bounce space, contains the connecting rods and the crankshaft.

The main design parameters of the machine are: medium pressure between 15 and 20 bar, nitrogen as the working gas, stainless steel for the cold head and aluminum for the radiator on the hot sink (Table 1).

Mathematical Model

The other fluid is the working gas (Nitrogen) of the Stirling refrigerator and it flows alternately (corresponding to the rotation frequency of the machine) at constant temperatureTC in the inner tube corresponding to the cylinder of the machine (Labels 8 and 10). In this work, the heat capacity rate is the product of the mass flow rate and the specific heat capacity rate of the incompressible fluid. The complex flow field created by the internal geometry of the heat exchanger affects the pressure gradient required to drive the flow.

The two constants sa and b depend on the properties of the fluid, the flow regime and the geometric constraints of the heat exchanger.

Figure 6. Control volume of the cold heat exchanger.
Figure 6. Control volume of the cold heat exchanger.

Results and Discussion

The entropy generation number (NS) increases with the length L of the heat exchanger due to the increase in fluid friction and pressure drop. For each mass flow rate ˙m of the refrigerant liquid, we measured the temperature TC of the cold gas in the expansion chamber of the refrigerator. The heat transfer affects the rate of entropy generation NS, which logically decreases with temperature TC, and the hydraulic diameter Dh, which corresponds to the dominance of the heat transfer irreversibilities over fluid losses (Figure 12).

The cold heat exchanger transfers heat from a gas to a coolant in the temperature range (240–300 K), and the efficiency of this operation is a result of the competition between heat transfer and irreversibilities in the fluid flow.

Figure 8. Variations of entropy generation rate N S as function of cold heat exchange L for different temperatures T C
Figure 8. Variations of entropy generation rate N S as function of cold heat exchange L for different temperatures T C

MDPI

Gambar

Figure 5. Maximum-power efficiency for the symmetric case Σ  c = 1/2, assuming the LD condition that t t c
Figure 6. Influence of the heat leak over the optimized efficiencies appearing in Figure 4
Figure 4. Comparison of efficiency limits at maximum power with the ratio Tmin/TMAX. This result appears more general than the result given in the literature referring to the linear hypothesis of Onsager.
Figure 1. Chemical potential scheme necessary for the reactions in Equation (1) to proceed forward.
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