ASHRAE 4711-2004 Coefficient of Performance of Fluorinatied Ether and Fluorinated Ether Mixtures《氟化醚和氟化醚混合物的性能系数》.pdf
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1、471 1 Coefficient of Performance of Fluorinated Ether and Fluorinated Ether Mixtures Ismail Kul, Ph.D. Darryl D. DesMarteau, Ph.D. Adolph Beyerlein, Ph.D. Member ASHRAE ABSTRACT The coejcient ofperformance (COP) is estimatedfrom thermodynamic literature data using methods of Morrison andMcLinden (I
2、986) and reportedfor the ether R-E125 and the ether mixtures R-E218(50%)/R-E143a(50%), R-E218/ R- I34a/R-I 61, R-E125(75%)/R- I61 (25%), R-EI25/R-32/ R-l52a, and R-E125/R-32/R-I34a. The chemical formulae for the ethers R-E218, R-E143a, and R-E125 are CF30CF2CF3, CF30CH3, and CF30CF2H, respectively.
3、The binary mixtures are azeotropic mixtures with the azeo- tropic compositions given in mole fraction, and the ternary mixtures are equimolar mixtures. The calculated COP of the mixtures rangedfrom 80% to 90% of thatfor R-22 except for the azeotropic mixtures R-E125(75%)/R-l61(25%) and R- E218(50%)/
4、R-E143A, whose calculated COPS are lower. The calculations show that R-EI25 and mixtures containing R-E2I8 would require superheat on the suction line to elim- inate “wet compression.“ INTRODUCTION The search for R-22 alternatives is complicated because it is difficult to match the wide spread betwe
5、en the boiling point (-40.1“C -40.2“F) and critical temperature (96C 204.8“F) of R-22. The leading class of compounds that provide us refrigerant alternatives that do not harm the strato- spheric ozone are the hydrofluorocarbons (HFC). Some of the HFC compounds (such as fluoroethane R-1611) with the
6、 highest critical temperatures and low boiling points that approach the boiling point of R-22 have a low fluorine content and tend to be flammable. Because of the difficulties in identifying an ideal HFC alternative, the search for R-22 alternatives has been extended to mixtures (Calm and Didion 199
7、8). This has led to the discovery of a number of mixture alternatives, and two of the leading HFC mixture alternatives that are currently being marketed, are R-410A (McLinden et al. 1998) and R-407C (Nagel and Bier 1995). However when comparing the cycle performance calculations of R-41 OA and R-407
8、C with R-22 some shortcomings are evident and the search for R-22 alter- natives continues. The low critical temperature of R-41 OA (72.5“C 162.5“F) results in higher volumetric capacity but reduced efficiency. Higher heat capacities of the more complex alternatives (particularly fluorinated propane
9、 deriv- atives) also lower rehgerant efficiencies. Methods for improving efficiencies by addition of a liquid-line/suction- line heat exchanger have been investigated by Domanski et al. (1 994a). Liquid-line/suction-line heat exchanger will super- heat the suction gas and may at first appear to incr
10、ease the cooling capaciy or refrigerating effect. However, this must be balanced against the lowered volume capacity and increased compression work associated with the superheated vapor. Domanski et al. (1994a) have found that the overall effect on refrigeration capacity and efficiency is usually sm
11、all and may be either positive or negative depending on a combination of factors with heat capacity being the most influential property. In view of the limitations of HFC refrigerant alternatives, the authors have measured the vapor pressure, liquid density, and critical properties of fluorinated et
12、hers, fluorinated sulfur compounds (CF,SF5 and CF3SCF3) and mixtures of these compounds (Ku1 2001; Beyerlein et al 1998). Although the heat capacity of these compounds is high, these compounds yield mixtures with high critical temperatures for improved refrigerant efficiency and at the same time hav
13、e boiling points approaching that of R-22. Ismail Ku1 is an assistant professor of chemistry at Widener University, Chester, Penn. Darryl D. DesMarteau is the Tobey-Beaudrot professor of chemistry and Adolph Beyerlein is retired chair and professor emeritus, Chemistry Department, Clemson University,
14、 Clemson, S.C. 02004 ASHRAE. 189 R-El25(33.3%)/R-32(33.3%)/R-134a(33.3%) P -40.4 40.7 86.2 187.2 H Figure 1 A pressure-enthalpy diagram illustrating an ideal refrigeration cycle. The measured data, which is used to estimate the coe6 cient of performance (COP) on six ether mixtures that are Iisted in
15、 Table i, are reported in the Ph.D. thesis of one of the authors (Ku1 2001). The COPs for the mixtures are estimated using the methods of Morrison and McLinden (1985, 1986) and the Camahan-Starling-DeSantis (CSD) equation of state (Carnahan and Starling 1969; DeSantis et al. 1976). It is the purpose
16、 of this paper to report the results of these investiga- tions. ESTIMATION OF COEFFICIENT OF PERFORMANCE In this section we briefly review the methods of Morrison and McLinden (1985, 1986) that are used for calculating the enthalpies needed to estimate the COP. The COPs of the vari- ous refrigerants
17、 in Table 1 are estimated for the ideal cycle sketched in Figure 1. The cycle is ideal in the sense that it does not account for the irreversibility in a real cycle. Briefly, the cycle includes a reversible evaporation at constant pressure represented by line ab in Figure I in which the liquid is va
18、por- ized to gas phase. The evaporation absorbs heat from the low- temperature heat reservoir (refrigeration or cooling effect) whose temperature should be above the normal boiling point of the refiigerant in order for the refrigerator to operate above atmospheric pressure. After this expansion ther
19、e is a reversible adiabatic, i.e., isentropic compression, of the vapor, repre- sented by line bc in Figure 1, which increases the temperature of the vapor to a temperature above the condensation temper- ature. The refrigerant is then released into a condenser repre- sented by line cde in Figure 1 i
20、n which all of the vapor is condensed to a liquid and in the process heat is transported from the refrigerant to the condenser heat reservoir. Following the condensation there is a Joule-Thomson expansion (constant enthalpy) represented by line ea in Figure 1, which brings the temperature of the sys
21、tem back to the Iow-temper- ature heat reservoir. The coefficient of performance (COP) is calculated by using the following equation, where H represents the molar enthalpy, qab is the heat absorbed during the evaporation cycle ab, and W is the work done for the complete cycle. Implicit in Equation 1
22、, we assume the isobaric condensa- tion and isobaric evaporation are also isothermal processes, which implies the equation is exact for pure chemicals and azeotropk mixtures. However, it also useful for “near azeo- tropic” mixtures that exhibit a minimal temperature glide (less than 1C to 2C l.SF to
23、 3.6”FI) during the evaporation portion of the cycle. The enthalpy change represented by line ab in Figure 1 can be obtained from the heat of vaporization calculated from vapor pressure measurements. The enthalpy change Hc-Hbfor the compression portion of the cycle is estimated using the methods of
24、Morrison and McLinden (1985, 1986). An advan- tage of their method is that it allows one to extrapolate the enthalpy of vaporization obtained from vapor pressure 190 ASHRAE Transactions: Research measurements to H, ofthe superheated vapor using the follow- ing Camahan-Starling-DeSantis (CSD) equatio
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