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HEATINC VENTILATING AIR CONDITIONING CUIDE 1941
Table 1. Properties of Ammonia
Sat. Temp.
F
Abb.
Press, Lb naa 8q itv.
Volume
liquid Vapor
Hfu t Content and Entropt Taken From --40 F
Heat Content
Idquit Vapor
Entropy Liquit Vapor
100 F Snperheat 200 F Superheat
Ht Ct Entropy Ht Ct
0 30.42 0.02419 2 31.92 0.02424 4 33.47 0.02430 5 34.27 0.02432 6 35.09 0.02435
8 36.77 0.02440 10 38.51 0.02446 12 4031 0.02451 14 42.18 0.02457 16 44.12 0.02462
18 46.13 0.02468 20 48.21 0.02474 22 50.36 .0.02479 24 5239 0.02485 26 54.90 0.02491
28 57.28 0.02497 30 59.74 0.02503 32 62.29 0.02508 34 64.91 0.02514 36 67.63 0.02521
38 70.43 0.02527 39 71.87 0.02530 40 7332 0.02533 41 7430 0.02536 42 7631 0.02539
44 79.38 0.02545 46 82.55 0.02551 48 85.82 0.02558 50 89.19 0.02564 52 92.66 0.02571
54 96.23 0.02577 56 99.91 0.02584 58 103.7 0.02590 60 107.6 0.02597 62 111.6 0.02604
64 66
68 . 70
72
115.7 120.0 1244 128.8 133.4
0.02611
0.02618 0.02625 0.02632
0.02639
74 138.1 0.02646 76 143.0 0.02653 78 147.9 0.02661 80 153.0 0.02668 82 158.3 0.02675
84 163.7 0.02684 86 169.2 0.02691 88 174.8 0.02699 90 180.6 0.02707 92 186.6 0.02715
94 192.7 0.02723 96 198.9 0.02731 98 2054 0.02739 100 211.9 0.02747 102 218.6 0.02756
104 225.4 0.02764 106 2324 0.02773 108 239.7 0.02782 120 247.0 0.02790 112 254.5 0.02799
114 262.2 0.02808 116 270.1 0.02817 118 278.2 0.02827 120 286.4 0.02836
122 2944 0.02846 124 303.4 0.02855 126 312.2 0.02865 228 321.2 0.02875
9.116 8.714 8333 8.150 7.971
7.629 7.304* 6.996 6.703 6.425
6.161 5.910 5.671 5.443 5327
5.021 4.825 4.637 4.459 4.289
4.126 4.048 3.971 3.897 3.823
3.682 3.547 3.418 3.294 3.176
3.063 2.954 2451 2.751 2.656
2.565 2.477 2.393 2.312 .2.235
2.161 2.089 2.021 1.955 1.892
1.831 1.772 1.716 1.661 1.609
1.5S9 1.510 1.464 1.419 1.375
1.334 1.293 1.254 1.21? 1.180
1.145 1.112 1.079 1.047
1.017 0.987 0.958 0.931
42.9 45.1 47.2 483 49.4
51.6 533 56.0 58.2 603
62-5 64.7 66.9 69.1 71J
733 75.7 77.9 80.1 823
84.6 85.7 863 87.9 89.0
91.2 93.5 95.7 97.9 100.2
611.8 612.4
613.0 613.3 613.6
0.0975 0.1022 0.1069
0.1092 0.1115
614.3 614.9
615.5 616.1
616.6 :
0.1162
0.1208 0.1254
0.1300 0.1346
617.2 617.8 6183 618.9
619.4
0.1392
0.1437 0.1483
0.1528 0.1573
619.9
620.5 621.0 621.5
622.0
0.1618
0.1663 0.1708 0.1753 0.1797
622.5
622.7 623.0 623.2 623.4
0.1841
0.1863
0.1885 0.1908
0.1930
623.9 624.4
624.8 625.2 625.7
0.1974 0.2018
0.2062 0.2105
0.2149
1.3352 13312 1-3273 1.3253 1.3234
1.3195 13157 1.3118 13081 1.3043
1.3006 1.2969 1.2933 1.2897 1.2861
1.2825 1.2790 1.2755 I.2721 1.2686
J.2652 1.2635 1.2618 1.2602 1.2585
1.2SS2 1.2519 1.2486 1.2453 1.2421
666.8 667.6 668.4 6683 6693
670.1 670.9 671.7 672.5 673.4
674.2 675.0 675.8 676.6 6773
678.1 678.9 679.7 680.4 681.2
681.9 682.3 682.7 683.1 683.4
684.2 684.9 685.6 686.4 687.1
1.4439 1.4400 1.4360
1.4340 1.4321
7203 721.2
722.2 722.6 723.1
1.4281
1.4242 1.4205 1.4168 1.4130
724.1
725.0 725.9 726.8 727.8
1.4093
1.4056 1.4021 1.3985 1.3950
728.7 729.6
730.5 731.4 732.4
U914 1.3879
1.3846
1.3812 1.3779
7333 734.2 735.1
736.0
736.8
1.3745
1.3729 1.3712 1.3696 13680
737.7 738.2
738.6 739.0
739.5
13648
13616
13584 13552 13521
740.4' 7413 7423 743.1
744.0
13317 13277
13236 13216 13196
13155 13115 1.5077 1.5039
13001
1.4963
1.4925 1.4889 1.4853
1.4816
1.4780 1.4744 1.4710
1.4676 1.4643
1.4609 1.4592
1.4575 1.4559
1.4542
1.4510
1.4477 1.4445 1.4412 1.4382
102.4
104.7 106.9 109.2
111.5
626.1
626.5 626.9
627.3 627.7
0.2192
0.2236 0.2279 0.2322 0.2365
1.2389 1.2357 1.2325 1.2294
1.2262
687.8
688.5 689.2 689.9 690.6
13491 13460
1.3430 13399 13370
7443
745.7 746.5 747.4
7483
1.4351 1.4321
1.4290 1.4260
1.4231
113.7 116.0 118.3
120.5 1223
628.0 628.4
628.8 629.1 629.4
0.2408 0.2451
0.2494 0.2537
0.2579
1.2231 1.2201
1.2170 1.2140 1.2110
691.3
691.9 692.6
693.3 694.0
13341
13312 13283 13254
13226
749.1 749.9 750.8 751.6 752.4
1.4202
1.4172 1.4143 1.4114
1.4086
125.1
127.4 129.7
132.0 134.3
629.8 630.1 630.4
630.7 631.0
0.2622 0.2664 0.2706 0.2749 0.2791
1.2080 1.2050 1.2020 1.1991
1.1962
694.6 695.3 695.9
696.6 697.2
1.3199 13171 13144
13116 13089
753.3 754.1
755.0 7S53
756.6
1.4059 1.4031 1.4004
1.3976 1.3949
136.6 138.9 141.2 143.5
145.8
631.3 631.5 631.8 632.0
632.2
0.2833 0.2875
0.2917 0.2958 0.3000
1.1933 1.1904
1.1875 1.1846
1.1818
697.8 698.5 699.1
699.7 700.3
1.3063 1.3040
13010 1.2983
1.2957
757.4 7583 759.1
759.9 760.7
1.3923 13896 1.3870
13843 13818
148.2
150.5 152.9 155.2
157.6
632.5 632.6 *
632.9 633.0
633.2
0.3041
0.3083 0.3125 0.3166 0.3207
1.1789 1.1761
1.1733 1.1705
1.1677
700.9 701.5 702.1
702.7 703.3
1.2932 1.2906 1.2881
1.2855 1.2830
7613 7623
763.0 7633
764.6
13793
13768 13743 13718
13693
159.9
1623 164.6 167.0 169.4
633.4
633.5 633.6 633.7
633.8
0.3248 0.3289 0.3330 0.3372 0.3413
1.1649 1.1621
1.1593 1.1566
1.1538
703.8
704.3 705.0
705.5 706.1
1.2805 1.2780 13755 1.2731
1.2708
7653 766.1 *766.9
767.6 768.3
13668 1.3643 13619
13596 13573
171.8 174.2 176.6 179.0
633.9 634.0
634.0 634.0
0.3453 0.3495 0.3535
0.3576
1.1510 1.1483 1.1455
1.1427
706.6 707.2 707.7
708.2
1.2684 1.2661
1.2636 1.2612
769.1 769.8 770.5
7 71.3
13550 13527
1.3503 1.3479
181.4 183.9 186.3
188.8
634.0
634.0 633.9 633.9
0.3618 0.3659
0.3700 0.3741
1.1400 1.1372 1.1344 1.1316
708.6 709.1 709.6 ' 710.0
1.2587 1.2563
1.2538 1.2513
772.0 7723
7733 7743
1.3455 13431
1.3407
1.3383
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CHAPTER 24. REFRICERATION
removed by an available cooling medium. In order to conserve refri gerant, virtually, all refrigeration systems are completely closed and the same refrigerant is recirculated.
The fundamental heat equations (disregarding losses) which should be kept in mind are: (1) the heat absorbed in the evaporator plus the heat added to the refrigerant during compression equals the heat rejected by the condenser; (2) the heat added to the refrigerant during compression is equal to the input to the compressor shaft less the heat dissipated from the compressor to the surroundings.
In the case where the compressor is driven by an electric motor, the heat due to compression is equal to the motor input less the electrical motor losses, less the power transmission losses and less the heat dis sipated from the compressor to the surroundings.
Heat of Compression Added to Qas
Refrigerants
There are many substances which might be used as refrigerants in mechanical refrigeration systems, but in practice the choice is limited by a wide variety of considerations including availability, cost, safety, chemical stability and adaptability to the type of refrigerating system to be used.
In this chapter detailed consideration is limited to six substances, viz: ammonia, dichlorodifluoromethane (F ), methyl chloride, carbon dioxide, monofluorotrichloromethane (Fn), and water, properties for each of which are given in Tables 1,2,3,4,5 and 6. Each table gives the principal physi cal properties of the saturated substance, and all are arranged in uniform fashion. In all except the water table, columns are included which'give the heat content and entropy of the superheated vapor at two selected points. The first four refrigerants named are used in reciprocating and rotary compressors. The last two are used in centrifugal compressors. Water is also used in steam jet equipment.
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