Modified Vapor Compression Cycle
Consider the same example as Example 14.1 where an R-134a cycle operates between −14°C and 30°C with a cooling capacity of 5.0 kW. The compressor isentropic efficiency is given as 0.8, while the vapor is superheated by 6°C. Find the power input, COP, kW/ton, and the refrigerating efficiency of this cycle, and compare these against the results of Example 14.1.
Given: T_{cond} = 30°C, T_{evap} = −14°C, \dot{Q}_{cool} = 5.0 kW, \eta_{isen} = 0.8, T_{1}´ – T_{1} = 6°C
Figure: See Figure 14.4.
Assumptions: All processes are steady. The cycle follows the modified VC cycle.
Find: \dot{W}_{comp}, COP_{mod}, kW/ton, and \eta_{R}
Lookup values: Thermodynamic properties are read from the R-134a saturation tables (Table A6) or from the online HCB software. As in Example 14.1, the low-side pressure is 0.1707 MPa and the high-side pressure is 0.7701 MPa.
TABLE A.6 (IP Units) Properties of Saturated Liquid and Saturated Vapor of R-134a |
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Temp. (°F) | Pressure (psia) | Density (lb/ft³) | Volume (ft³/lb) | Enthalpy (Btu/lb) | Entropy (Btu/lb · °F) | ||
Liquid | Vapor | Liquid | Vapor | Liquid | Vapor | ||
-153.94 | 0.057 | 99.34 | 564.85 | 32.989 | 80.235 | 0.09154 | 0.2788 |
-150 | 0.072 | 98.95 | 449.29 | 31.902 | 80.783 | 0.08801 | 0.27588 |
-140 | 0.130 | 97.98 | 259.15 | 29.093 | 82.190 | 0.07908 | 0.26903 |
-130 | 0.222 | 97.01 | 155.69 | 26.238 | 83.618 | 0.07029 | 0.26294 |
-120 | 0.367 | 96.05 | 97.027 | 23.359 | 85.066 | 0.06169 | 0.25752 |
-110 | 0.586 | 95.09 | 62.509 | 20.467 | 86.531 | 0.05330 | 0.2527 |
-100 | 0.906 | 94.13 | 41.496 | 17.569 | 88.011 | 0.04513 | 0.24842 |
-90 | 1.363 | 93.17 | 28.303 | 14.665 | 89.504 | 0.03717 | 0.24462 |
-80 | 1.997 | 92.21 | 19.783 | 11.755 | 91.005 | 0.02940 | 0.24125 |
-75 | 2.396 | 91.73 | 16.680 | 10.297 | 91.759 | 0.02559 | 0.23972 |
-70 | 2.859 | 91.25 | 14.138 | 8.837 | 92.514 | 0.02182 | 0.23827 |
-65 | 3.393 | 90.77 | 12.045 | 7.374 | 93.270 | 0.01809 | 0.23691 |
-60 | 4.006 | 90.28 | 10.310 | 5.907 | 94.026 | 0.01440 | 0.23563 |
-55 | 4.707 | 89.80 | 8.8656 | 4.437 | 94.783 | 0.01075 | 0.23443 |
-50 | 5.505 | 89.31 | 7.6569 | 2.963 | 95.539 | 0.00713 | 0.23331 |
-45 | 6.409 | 88.82 | 6.6405 | 1.484 | 96.295 | 0.00355 | 0.23225 |
-40 | 7.429 | 88.32 | 5.7819 | 0.000 | 97.050 | 0.00000 | 0.23125 |
-35 | 8.577 | 87.83 | 5.0533 | 1.489 | 97.804 | 0.00352 | 0.23032 |
-30 | 9.862 | 87.33 | 4.4325 | 2.984 | 98.556 | 0.00701 | 0.22945 |
-25 | 11.297 | 86.82 | 3.9014 | 4.484 | 99.306 | 0.01048 | 0.22863 |
-20 | 12.895 | 86.32 | 3.4452 | 5.991 | 100.054 | 0.01392 | 0.22786 |
-15 | 14.667 | 85.81 | 3.0519 | 7.505 | 100.799 | 0.01733 | 0.22714 |
−14.92 | 14.696 | 85.80 | 3.0462 | 7.529 | 100.811 | 0.01739 | 0.22713 |
-10 | 16.626 | 85.29 | 2.7116 | 9.026 | 101.542 | 0.02073 | 0.22647 |
-5 | 18.787 | 84.77 | 2.4161 | 10.554 | 102.280 | 0.02409 | 0.22584 |
0 | 21.162 | 84.25 | 2.1587 | 12.090 | 103.015 | 0.02744 | 0.22525 |
5 | 23.767 | 83.72 | 1.9337 | 13.634 | 103.745 | 0.03077 | 0.2247 |
10 | 26.617 | 83.18 | 1.7365 | 15.187 | 104.471 | 0.03408 | 0.22418 |
15 | 29.726 | 82.64 | 1.5630 | 16.748 | 105.192 | 0.03737 | 0.2237 |
20 | 33.110 | 82.10 | 1.4101 | 18.318 | 105.907 | 0.04065 | 0.22325 |
25 | 36.785 | 81.55 | 1.2749 | 19.897 | 106.617 | 0.04391 | 0.22283 |
30 | 40.768 | 80.99 | 1.1550 | 21.486 | 107.320 | 0.04715 | 0.22244 |
35 | 45.075 | 80.42 | 1.0484 | 23.085 | 108.016 | 0.05038 | 0.22207 |
40 | 49.724 | 79.85 | 0.9534 | 24.694 | 108.705 | 0.05359 | 0.22172 |
45 | 54.732 | 79.26 | 0.8685 | 26.314 | 109.386 | 0.05679 | 0.22140 |
50 | 60.116 | 78.67 | 0.7925 | 27.944 | 110.058 | 0.05998 | 0.22110 |
55 | 65.895 | 78.07 | 0.7243 | 29.586 | 110.722 | 0.06316 | 0.22081 |
60 | 72.087 | 77.46 | 0.6630 | 31.239 | 111.376 | 0.06633 | 0.22054 |
65 | 78.712 | 76.84 | 0.6077 | 32.905 | 112.019 | 0.06949 | 0.22028 |
70 | 85.787 | 76.21 | 0.5577 | 34.583 | 112.652 | 0.07264 | 0.22003 |
75 | 93.333 | 75.57 | 0.5125 | 36.274 | 113.272 | 0.07578 | 0.21979 |
80 | 101.370 | 74.91 | 0.4715 | 37.978 | 113.880 | 0.07892 | 0.21957 |
85 | 109.920 | 74.25 | 0.4343 | 39.697 | 114.475 | 0.08205 | 0.21934 |
90 | 119.000 | 73.57 | 0.4004 | 41.430 | 115.055 | 0.08518 | 0.21912 |
95 | 128.630 | 72.87 | 0.3694 | 43.179 | 115.619 | 0.08830 | 0.2189 |
100 | 138.830 | 72.16 | 0.3411 | 44.943 | 116.166 | 0.09142 | 0.21868 |
105 | 149.630 | 71.43 | 0.3153 | 46.725 | 116.694 | 0.09454 | 0.21845 |
110 | 161.050 | 70.68 | 0.2915 | 48.524 | 117.203 | 0.09766 | 0.21822 |
115 | 173.110 | 69.91 | 0.2697 | 50.343 | 117.690 | 0.10078 | 0.21797 |
120 | 185.840 | 69.12 | 0.2497 | 52.181 | 118.153 | 0.10391 | 0.21772 |
125 | 199.250 | 68.31 | 0.2312 | 54.040 | 118.591 | 0.10704 | 0.21744 |
130 | 213.380 | 67.47 | 0.2141 | 55.923 | 119.000 | 0.11018 | 0.21715 |
135 | 228.250 | 66.60 | 0.1983 | 57.830 | 119.377 | 0.11333 | 0.21683 |
140 | 243.880 | 65.70 | 0.1836 | 59.764 | 119.720 | 0.11650 | 0.21648 |
145 | 260.310 | 64.77 | 0.1700 | 61.727 | 120.024 | 0.11968 | 0.21609 |
150 | 277.570 | 63.80 | 0.1574 | 63.722 | 120.284 | 0.12288 | 0.21566 |
155 | 295.690 | 62.78 | 0.1455 | 65.752 | 120.495 | 0.12611 | 0.21517 |
160 | 314.690 | 61.72 | 0.1345 | 67.823 | 120.650 | 0.12938 | 0.21463 |
165 | 334.620 | 60.60 | 0.1241 | 69.939 | 120.739 | 0.13268 | 0.214 |
170 | 355.510 | 59.42 | 0.1144 | 72.106 | 120.753 | 0.13603 | 0.21329 |
175 | 377.400 | 58.16 | 0.1052 | 74.335 | 120.677 | 0.13945 | 0.21247 |
180 | 400.340 | 56.80 | 0.0965 | 76.636 | 120.493 | 0.14295 | 0.21151 |
185 | 424.370 | 55.33 | 0.0881 | 79.027 | 120.175 | 0.14655 | 0.21037 |
190 | 449.550 | 53.70 | 0.0801 | 81.534 | 119.684 | 0.15029 | 0.20901 |
195 | 475.950 | 51.86 | 0.0723 | 84.196 | 118.963 | 0.15423 | 0.20733 |
200 | 503.640 | 49.70 | 0.0646 | 87.088 | 117.906 | 0.15847 | 0.20519 |
205 | 532.720 | 47.00 | 0.0566 | 90.368 | 116.289 | 0.16326 | 0.20226 |
210 | 563.340 | 43.03 | 0.0474 | 94.548 | 113.411 | 0.16933 | 0.19750 |
213.85 | 588.270 | 32.04 | 0.0312 | 103.775 | 103.775 | 0.18128 | 0.18128 |
Source: Courtesy of ASHRAE, Handbook of Fundamentals, American Society of Heating, Refrigerating and Air-Conditioning Engineers, Atlanta, GA, 1997. With permission. Notes: Values shown in italics are at the boiling point. Values shown in bold are at the critical point. |
TABLE A.6 (SI Units) Properties of Saturated Liquid and Saturated Vapor of R-134a |
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Temp. (°C) | Pressure (MPa) | Density (kg/m3) | Volume (m³/kg) | Enthalpy (kJ/kg) | Entropy (kJ/kg · K) | ||
Liquid | Vapor | Liquid | Vapor | Liquid | Vapor | ||
-103.3 | 0.00039 | 1591.2 | 35.263 | 71.89 | 335.07 | 0.4143 | 1.9638 |
-100 | 0.00056 | 1581.9 | 25.039 | 75.71 | 337.00 | 0.4366 | 1.9456 |
-90 | 0.00153 | 1553.9 | 9.7191 | 87.59 | 342.94 | 0.5032 | 1.8975 |
-80 | 0.00369 | 1526.2 | 4.2504 | 99.65 | 349.03 | 0.5674 | 1.8585 |
-70 | 0.00801 | 1498.6 | 2.0528 | 111.78 | 355.23 | 0.6286 | 1.8269 |
-60 | 0.01594 | 1471.0 | 1.0770 | 123.96 | 361.51 | 0.6871 | 1.8016 |
-50 | 0.02945 | 1443.1 | 0.60560 | 136.21 | 367.83 | 0.7432 | 1.7812 |
-40 | 0.05122 | 1414.8 | 0.36095 | 148.57 | 374.16 | 0.7973 | 1.7649 |
-30 | 0.08436 | 1385.9 | 0.22596 | 161.10 | 380.45 | 0.8498 | 1.7519 |
-28 | 0.09268 | 1380.0 | 0.20682 | 163.62 | 381.70 | 0.8601 | 1.7497 |
-26.07 | 0.10132 | 1374.3 | 0.19016 | 166.07 | 382.90 | 0.8701 | 1.7476 |
-26 | 0.10164 | 1374.1 | 0.18961 | 166.16 | 382.94 | 0.8704 | 1.7476 |
-24 | 0.11127 | 1368.2 | 0.17410 | 168.70 | 384.19 | 0.8806 | 1.7455 |
-22 | 0.12160 | 1362.2 | 0.16010 | 171.26 | 385.43 | 0.8908 | 1.7436 |
-20 | 0.13268 | 1356.2 | 0.14744 | 173.82 | 386.66 | 0.9009 | 1.7417 |
-18 | 0.14454 | 1350.2 | 0.13597 | 176.39 | 387.89 | 0.9110 | 1.7399 |
-16 | 0.15721 | 1344.1 | 0.12556 | 178.97 | 389.11 | 0.9211 | 1.7383 |
-14 | 0.17074 | 1338.0 | 0.11610 | 181.56 | 390.33 | 0.9311 | 1.7367 |
-12 | 0.18516 | 1331.8 | 0.10749 | 184.16 | 391.55 | 0.9410 | 1.7351 |
-10 | 0.20052 | 1325.6 | 0.09963 | 186.78 | 392.75 | 0.9509 | 1.7337 |
-8 | 0.21684 | 1319.3 | 0.09246 | 189.40 | 393.95 | 0.9608 | 1.7323 |
-6 | 0.23418 | 1313.0 | 0.08591 | 192.03 | 395.15 | 0.9707 | 1.7310 |
-4 | 0.25257 | 1306.6 | 0.07991 | 194.68 | 396.33 | 0.9805 | 1.7297 |
-2 | 0.27206 | 1300.2 | 0.07440 | 197.33 | 397.51 | 0.9903 | 1.7285 |
0 | 0.29269 | 1293.7 | 0.06935 | 200.00 | 398.68 | 1.0000 | 1.7274 |
2 | 0.31450 | 1287.1 | 0.06470 | 202.68 | 399.84 | 1.0097 | 1.7263 |
4 | 0.33755 | 1280.5 | 0.06042 | 205.37 | 401.00 | 1.0194 | 1.7252 |
6 | 0.36186 | 1273.8 | 0.05648 | 208.08 | 402.14 | 1.0291 | 1.7242 |
8 | 0.38749 | 1267.0 | 0.05284 | 210.80 | 403.27 | 1.0387 | 1.7233 |
10 | 0.41449 | 1260.2 | 0.04948 | 213.53 | 404.40 | 1.0483 | 1.7224 |
12 | 0.44289 | 1253.3 | 0.04636 | 216.27 | 405.51 | 1.0579 | 1.7215 |
14 | 0.47276 | 1246.3 | 0.04348 | 219.03 | 406.61 | 1.0674 | 1.7207 |
16 | 0.50413 | 1239.3 | 0.04081 | 221.80 | 407.70 | 1.0770 | 1.7199 |
18 | 0.53706 | 1232.1 | 0.03833 | 224.59 | 408.78 | 1.0865 | 1.7191 |
20 | 0.57159 | 1224.9 | 0.03603 | 227.40 | 409.84 | 1.0960 | 1.7183 |
22 | 0.60777 | 1217.5 | 0.03388 | 230.21 | 410.89 | 1.1055 | 1.7176 |
24 | 0.64566 | 1210.1 | 0.03189 | 233.05 | 411.93 | 1.1149 | 1.7169 |
26 | 0.68531 | 1202.6 | 0.03003 | 235.90 | 412.95 | 1.1244 | 1.7162 |
28 | 0.72676 | 1194.9 | 0.02829 | 238.77 | 413.95 | 1.1338 | 1.7155 |
30 | 0.77008 | 1187.2 | 0.02667 | 241.65 | 414.94 | 1.1432 | 1.7149 |
32 | 0.81530 | 1179.3 | 0.02516 | 244.55 | 415.90 | 1.1527 | 1.7142 |
34 | 0.86250 | 1171.3 | 0.02374 | 247.47 | 416.85 | 1.1621 | 1.7135 |
36 | 0.91172 | 1163.2 | 0.02241 | 250.41 | 417.78 | 1.1715 | 1.7129 |
38 | 0.96301 | 1154.9 | 0.02116 | 253.37 | 418.69 | 1.1809 | 1.7122 |
40 | 1.01650 | 1146.5 | 0.01999 | 256.35 | 419.58 | 1.1903 | 1.7115 |
42 | 1.07210 | 1137.9 | 0.01890 | 259.35 | 420.44 | 1.1997 | 1.7108 |
44 | 1.13000 | 1129.2 | 0.01786 | 262.38 | 421.28 | 1.2091 | 1.7101 |
46 | 1.19010 | 1120.3 | 0.01689 | 265.42 | 422.09 | 1.2185 | 1.7094 |
45 | 1.25270 | 1111.3 | 0.01598 | 268.49 | 422.88 | 1.2279 | 1.7086 |
50 | 1.31770 | 1102.0 | 0.01511 | 271.59 | 423.63 | 1.2373 | 1.7078 |
52 | 1.38520 | 1092.6 | 0.01430 | 274.71 | 424.35 | 1.2468 | 1.7070 |
54 | 1.45530 | 1082.9 | 0.01353 | 277.86 | 425.03 | 1.2562 | 1.7061 |
56 | 1.52800 | 1073.0 | 0.01280 | 281.04 | 425.68 | 1.2657 | 1.7051 |
58 | 1.60330 | 1062.8 | 0.01212 | 284.25 | 426.29 | 1.2752 | 1.7041 |
60 | 1.68150 | 1052.4 | 0.01146 | 287.49 | 426.86 | 1.2847 | 1.7031 |
62 | 1.76250 | 1041.7 | 0.01085 | 290.77 | 427.37 | 1.2943 | 1.7019 |
64 | 1.84640 | 1030.7 | 0.01026 | 294.08 | 427.84 | 1.3039 | 1.7007 |
66 | 1.93340 | 1019.4 | 0.00970 | 297.44 | 428.25 | 1.3136 | 1.6993 |
68 | 2.02340 | 1007.7 | 0.00917 | 300.84 | 428.61 | 1.3234 | 1.6979 |
70 | 2.11650 | 995.6 | 0.00867 | 304.29 | 428.89 | 1.3332 | 1.6963 |
72 | 2.21300 | 983.1 | 0.00818 | 307.79 | 429.1 | 1.3430 | 1.6945 |
74 | 2.31270 | 970.0 | 0.00772 | 311.34 | 429.23 | 1.3530 | 1.6926 |
76 | 2.41590 | 956.5 | 0.00728 | 314.96 | 429.27 | 1.3631 | 1.6905 |
78 | 2.52270 | 942.3 | 0.00686 | 318.65 | 429.20 | 1.3733 | 1.6881 |
80 | 2.63310 | 927.4 | 0.00646 | 322.41 | 429.02 | 1.3837 | 1.6855 |
85 | 2.92590 | 886.2 | 0.00550 | 332.27 | 427.91 | 1.4105 | 1.6775 |
90 | 3.24450 | 836.9 | 0.00461 | 343.01 | 425.48 | 1.4392 | 1.6663 |
95 | 3.59160 | 771.6 | 0.00374 | 355.43 | 420.60 | 1.4720 | 1.6490 |
100 | 3.97210 | 646.7 | 0.00265 | 374.02 | 407.08 | 1.5207 | 1.6093 |
101.03 | 4.05600 | 513.3 | 0.002 | 389.79 | 389.79 | 1.5593 | 1.5593 |
Source: Courtesy of ASHRAE, Handbook of Fundamentals, American Society of Heating, Refrigerating and Air-Conditioning Engineers, Atlanta, GA, 1997. With permission. Notes: Values shown in bold italics are at the triple point. Values shown in italics are at the boiling point. Values shown in bold are at the critical point. |
We start with the fact that the vapor at state 1´ is superheated by 6°C. Hence, for a temperature of (−14 + 6 =) −8°C and pressure of 0.1707 MPa, the vapor enthalpy h´_{1} = 395.24 kJ/kg. With the condition that the process is isentropic from 1´ to 2´, i.e., s´_{1} = s´_{2}, we can determine the enthalpy of point 2´.
We determine h´_{2} = 427.5 kJ/kg
We can deduce the enthalpy of the subcooled uid leaving the condenser (Equation 14.13)
(h_{3} – h´_{3}) = (h´_{1} – h_{1}) (14.13)
h_{3} = h_{3} – (h´_{1} – h_{1}) = 241.65 – (395.24 – 390.33)= 236.74 kJ/kg
Next, we compute the refrigerant mass flow from Equation 14.6 with h´_{4} = h´_{3}
\dot{m}_{r} = \frac{\dot{Q}_{cool}}{(h_{1} – h´_{4})} = \frac{5.0 kW}{(390.33 – 236.74) kJ/kg}= 0.0326 kg/s (earlier it was 0.0336)
We rearrange Equation 14.14 to get the enthalpy of the vapor leaving the compressor:
\eta_{isen} = \frac{h´_{2} – h´_{1}}{h"_{2} – h´_{1}} (14.14)
h"_{2} = h´_{1} + \frac{(h´_{2} – h´_{1})}{\eta_{isen}} = 395.24 + \frac{(427.50 – 395.24)}{0.8}= 435.565 kJ/kg
This allows the compressor power input to be determined (from Equation 14.7)
\dot{W}_{comp} = \dot{m}_{r} (h_{2} – h_{1}) (14.7)
\dot{W}_{comp} = 0.0326 kg/s \times (435.565 – 390.33) kJ/kg= 1.473 kW (earlier it was 1.05)
The COP of the modied VC cycle:
COP_{mod} = \frac{5.0}{1.473} = 3.40 (earlier it was 4.76)
From Equation 14.10, the kW/ton of the machine = 3.516/3.39 = 1.04 kW/ton (earlier it was 0.739) The Carnot efficiency remains unaltered and is the same as that of Example 14.1, i.e., COPCarnot = 5.886. The refrigerating efficiency from Equation 14.11 is finally determined:
\eta_{R} = (COP_{std}/COP_{Carnot}) (14.11)
\eta_{R} = \frac{COP_{std}}{COP_{Carnot}} = \frac{3.40}{5.886} = 0.577Comments
Due to the isentropic efficiency of the compressor, the COP and the kW/ton have become worse than those for the standard VC cycle of Example 14.1. In fact, multiplying the COP found in Example 4.1 by \eta_{R} =0.8 (the value assumed in Example 14.2) yields a COP for the modified cycle of 3.81. The further difference in COP between 3.81 and 3.40 found earlier is because of the superheat effect.