/ / Article

Research Article | Open Access

Volume 2014 |Article ID 890713 | 7 pages | https://doi.org/10.1155/2014/890713

# Work Criteria Function of Irreversible Heat Engines

Accepted17 Jul 2014
Published05 Aug 2014

#### Abstract

The irreversible heat engine is reconsidered with a general heat transfer law. Three criteria known in the literature—power, power density, and efficient power—are redefined in terms of the work criteria function (WCF), a concept introduced in this study. The formulation enabled the suggestion and analysis of a unique criterion—the efficient power density (which accounts for the efficiency and power density). Practically speaking, the efficient power and the efficient power density could be defined on any order based on the WCF. The applicability of the WCF is illustrated for the Newtonian heat transfer law () and for the radiative law (). The importance of WCF is twofold: it gives an explicit design and educational tool to analyze and to display graphically the different criteria side by side and thus helps in design process. Finally, the criteria were compared and some conclusions were drawn.

#### 2. The Work Criteria Function

The irreversible heat engine, as considered earlier, in , was assumed to follow law of radiative heat transfer. It was analyzed to determine the maximum efficient power. In this section, the irreversible heat engine is reconsidered based on laws of general heat transfer, and criteria known in the literature (maximum power, maximum power density, and maximum efficient power) are reviewed and recast in terms of the work criteria function (WCF). The WCF allows the definition of a new criterion, the maximum efficient power density, as suggested from the result obtained. The analysis relies upon applying the first and second laws of thermodynamics written as equality, which is a common exercise that is well documented in the literature available in finite-time thermodynamics research. The schematics of the engine are given in Figure 1, and the schematics of its temperature entropy diagram are depicted by Figure 2. The irreversible heat engine under consideration works between two heat reservoirs at high and low temperatures. The rate of heat input to the engine, , is given by In this equation, exponent represents well-known heat transfer rates: the Newtonian heat transfer rate (), the radiative heat transfer rate (), and so on; is the thermal conductance at the hot side of the engine; is the temperature of the hot reservoir; and is the temperature of the working fluid at the hot side of the engine. Similarly, the cooling rate or the rate of heat rejection from the heat engine, , is given by In this equation, is the thermal conductance at the cold side of the heat engine, is the temperature of the working fluid at the cold side of the engine, and is the temperature of the cold reservoir. The net power rate, , extracted by the heat engine, follows the first law of thermodynamics for a cyclic process and is given by The second law of thermodynamics, accounting for internal irreversibilities, is given by In (4) is the irreversibility factor; its value falls in the range.

The efficiency of the heat engine is defined as the ratio between net power extracted from the heat engine and the rate of heat absorbed by it. In mathematical symbols the efficiency is given by where is the efficiency of the endoreversible heat engine ().

Equations (1) to (4) are manipulated and rearranged in the following calculations in order to explicitly progress to the work criteria function formulation. Equation (1) is rearranged to give the temperature at the hot side of the engine by Similarly, based on (2), the temperature at the cold side of the engine is given by The efficiency of the endoreversible heat engine () is a convenient choice to relate the ratio of the heat engine temperature; thus (4) could be rearranged as given by Equations (6)–(8) are used to derive the explicit expression for the rate of heat input to the engine, given by In this equation is the ratio between the temperatures of the reservoirs, , and is the ratio between the thermal conductance ratio .

As stated earlier, there are different criteria that are commonly used to describe the performance of heat engines. In this study the following criteria are considered:(i)the net power extracted from the heat engine (given by (3));(ii)the net power density defined as the net power extracted divided by the maximum volume (see  for more details);(iii)the net efficient power defined as the efficiency multiplied by the net power;(iv)the net efficient power density defined as the net efficient power divided by the maximum volume of the working fluid;(v)Results being valid for ideal gas  (10).The maximum volume of the working fluid, (expressed in SI units), is adopted from  and is given by In this equation is the mass of the working fluid, is the ideal gas coefficient (assuming ideal gas as the working fluid), and is the minimum pressure in the cycle. It is interesting to note that the criteria summarized in the previous page by (i)–(iv) could be addressed by the work criteria function, which is given by In this equation and are integers to represent the criteria considered in the study. The study uses to give the expression of the heat input to the heat engine (see (1) and (9)). The power output extracted by the heat engine is given when and . The power density criterion is defined when and . The efficient power criterion is defined using and . From the suggested formalism (see (11)), one could consider the criterion defined by to mean the efficient power density extracted by the heat engine. The WCF, therefore, provides a general statement to define efficient power and efficient power density of any order.

The WCF could be viewed as a one-dimensional function for a specific choice of variables or parameters involved. In this study, the parameter was chosen to be variable; its value spans the range from zero up to Carnot efficiency (). The other parameters are each chosen to define a specific criterion. The general criteria suggested by the work function is given by To facilitate the generation of the plots given in the next section, the temperatures at both sides of the heat engine, as derived in explicit form, are shown for the convenience of the reader. The temperature of the working fluid at the hot side of the engine is given by The temperature of the working fluid at the cold side of the engine (using (8)-(9) and (13)) is given by In the next section the WCF is considered numerically and sample plots are given for illustrating its usage in analyzing different criteria for the irreversible heat engine.

#### 3. Numerical Considerations

In this section the work criteria function is used to illustrate the different criteria aforementioned earlier. The Newtonian heat transfer law is used in the illustration, but other cases could be presented, following the same procedure.

##### 3.1. Newtonian Heat Transfer Law ()

The following figures (Figures 39) are given for the case of the Newtonian heat transfer law, with (a typical value of Rankine cycle or steam turbines, for which  K and  K). Figure 3 shows the power output of the endoreversible heat engine relative to its maximum value. The plot shows curves of the power for different values of the irreversibility factor, , in the 0.85–1 range.

By consulting Figure 3 two points should be explained in some detail. First, the maximum efficiency is reduced from the Carnot efficiency to values given by (5). Second, the maximum power is reduced and its efficiency is shifted to the left. If we consider the extreme case, or , one could observe that the maximum efficiency and the efficiency at maximum power were reduced by approximately 20%, while the maximum power was reduced by 42%. Similar behavior is observed when considering the other performance characteristic curves, such as power density (Figure 4), efficient power (Figure 5), and efficient power density (Figure 6). It is important to note that the criteria considered in the plots, in ascending order, show a shift to the right in the location of the maximum value of the criterion under consideration. One could conclude that, for a higher order of the efficient power or the efficient power density, a higher shift to the right in the efficiency value is produced.

The effect of thermal conductance is reported in Figures 7 and 8, for which inclusive values of in the 1–10 range are shown on the plots. The reasonable general conclusion is depicted, as the value of changes drastically, of the efficiency at maximum criteria changed approximately by 3%. For comparison purposes, power, power density, efficient power, and efficient power density criteria for the case are shown on the plots given by Figure 9. The conclusions stated above are now shown explicitly, as could be noticed in this figure.

##### 3.2. Radiative Heat Transfer Law ()

The work criteria function could be used to easily analyze different values for different values of (the exponent power found in the heat transfer rate expressions). For demonstrating its use, the radiative heat transfer law is considered. Figure 10 shows the criteria (similar to Figure 9) with one exception—the typical value of is 0.3 (a typical value of the gas turbine dictated by  K and  K). Although the location of the efficiency at the maximum criteria considered is changed, conclusions similar to those drawn for the case of are nevertheless valid.

#### 4. Summary and Conclusions

In the current study three criteria of the irreversible heat engine in finite time are reconsidered for a more general heat transfer law (as given by (1) and (2)). Power, power density, and efficient power were cast in a functional form called the work criteria function (WCF—see (11)-(12)). This formulation enabled the introduction of the efficient power density, a new criterion used for describing the performance characteristics of heat engines. The WCF suggests efficient power and efficient power density of different orders, represented by the exponents and .

Sample plots are given in Section 3 illustrating the simplicity of the WCF. The Newtonian heat transfer law () served as a working example to present and compare the criteria mentioned above. The conclusions from these plots for the arbitrarily chosen value of (ideally the value of should approach 1) were as follows: (1) the maximal efficiency is reduced according to (5) by approximately 20%; (2) the maximum criteria were reduced by 42%; (3) the locations of the efficiency at maximum criteria were shifted to the left, similar to the shift in the maximal efficiency; (4) the smaller the value of the heat conductance ratio, the more power that could be extracted from the engine; and (5) the location of the efficiency at maximum criteria is shifted to the right while comparing the criteria considered above in their order of presentation.

The radiative heat transfer law was considered briefly in Figure 10. Similar conclusions are drawn as for the Newtonian heat transfer law with the following exceptions: the value of the efficiency at maximum criteria is different and the reservoirs temperature is 0.3, which is a typical value representing gas turbine.

Comparing the plots given in Section 3 with what was observed by previous studies, the following conclusion could be derived regarding the practical efficiency of real heat engines.

The efficiencies of any criteria of any order always fall between two extremes—the Carnot efficiency and the Curzon-Ahlborn efficiency.

#### Conflict of Interests

The author declares that there is no conflict of interests regarding the publication of this paper.

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