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and Recommendations Up: Heat
Exchanger Mean Temperature Previous: Application
of the Numerical Technique
Subsections
Results and Discussion
Ammonia-Water Mixtures
Properties
As can be seen from the temperature versus enthalpy profile of Figure 1.4,
ammonia-water (NH3/H2O) mixtures generally have extremely
nonlinear temperature profiles. This nonlinearity indicates a potential
for large error when the LMTD is used to compute the size of a heat exchanger.
Therefore, an ammonia-water mixture is an ideal case for the initial application
of the methods developed in Chapters 3-4.
Three separate mixture concentrations were studied: ninety-five percent,
ninety-eight percent, and ninety-nine percent ammonia. These are typical
concentrations for condensers in ammonia-water absorption refrigeration
cycles. Furthermore, each mixture was analyzed at five pinch points (at
the refrigerant mixture entrance) ranging from 1-10 K. For each
concentration and pinch, the NH3/H2O EES program
(Appendix B) was executed.
Given the above conditions, the temperature of the NH3/H2O
refrigerant stream was found to range widely, from approximately 30 to
100 °C. While the temperature glides and the operating pressures vary
with both pinch and concentration, glide increases significantly with concentration
while pressure is a weak function of pinch, as expected. The pressures
and temperature glides for all the runs are listed in Table 5.1.
Table 5.1: Operating Pressures and Temperature Glides for
NH3/H2O
| Concentration = 0.95 |
|
| |
Pinch (K) |
| |
1 |
3 |
5 |
7 |
10 |
| P (bar) |
11.119 |
11.793 |
12.497 |
13.233 |
14.397 |
| Tglide (K) |
65.96 |
65.59 |
65.24 |
64.89 |
64.34 |
|
|
| Concentration = 0.98 |
|
| |
Pinch (K) |
| |
1.74 |
3 |
5 |
7 |
10 |
| P (bar) |
11.693 |
12.135 |
12.862 |
13.621 |
14.824 |
| Tglide (K) |
49.65 |
49.36 |
48.89 |
48.41 |
47.69 |
|
|
| Concentration = 0.99 |
|
| |
Pinch (K) |
| |
2.47 |
3 |
5 |
7 |
10 |
| P (bar) |
12.068 |
12.257 |
12.992 |
13.76 |
14.976 |
| Tglide (K) |
38.82 |
38.68 |
38.15 |
37.61 |
36.79 |
The Fallacy of an End-Point Pinch
Figure 5.1: NH3/H2O: Concentration
= 0.99, Pinch = 1 K
 |
Figure 5.2: Concentration and Nonlinearity for NH3/H2O
 |
The nonlinearity of NH3/H2O can lead to results
that are physically unrealistic. For example, at a concentration of 99%
and a pinch point of 1 K, the LMTD is found to be 9.6 K,
resulting in a UA equal to 132.72 [kJ/kg ·K].
In fact, a pinch of 1 K at the mixture inlet is impossible, as demonstrated
in Figure 5.1. An identical problem occurs
at the same pinch for a concentration of 98%. Furthermore, by comparing
the curves for a pinch point of 5 K and concentrations of ninety-five,
ninety-eight, and ninety-nine percent ammonia (Figure 5.2)
it can be observed that while the nonlinearity increases with ammonia concentration,
it remains strong even at ninety-five percent.
To avoid physically impossible calculations, care was taken to select
pinch points where the streams' temperatures would not cross. It should
be noted, however, that for NH3/H2O, all listed pinch
conditions are solely applicable to the mixture entrance, as smaller temperature
differences will consistently occur within the heat exchanger. The occurrence
of an internal pinch can be predicted by comparing the value of
¶h/¶T
for the refrigerant mixture at the inlet and
the outlet. If
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then an interior pinch will occur (Venkatarathnam
et al., 1996).
Log Error Ratio for Ammonia-Water
Figure 5.3: Log Error Ratio vs. Pinch Point for NH3/H2O
 |
As predicted, differences between the LMTD-calculated and the actual
UA were observed at every concentration and pinch point. Since these
differences can be quite large, the log error ratio was utilized. The LER
does indeed provide a meaningful scale for evaluation, as the error can
easily be graphically displayed (Figure 5.3).
Furthermore, the values of the UA, UALMTD, and
LER are compiled in Table 5.2
for every run.
Table 5.2: UA, UALMTD, and LER
for NH3/H2O
| Concentration = 0.95 |
|
| |
Pinch (K) |
| |
1 |
3 |
5 |
7 |
10 |
| UA |
1392.392 |
342.442 |
204.114 |
146.909 |
104.327 |
| UALMTD |
96.175 |
71.188 |
59.882 |
52.63 |
45.16 |
| LER |
1.161 |
0.682 |
0.533 |
0.446 |
0.364 |
|
|
| Concentration = 0.98 |
|
| |
Pinch (K) |
| |
1.74 |
3 |
5 |
7 |
10 |
| UA |
6206.845 |
571.118 |
274.649 |
182.668 |
122.328 |
| UALMTD |
97.132 |
81.83 |
67.895 |
59.038 |
50.002 |
| LER |
1.806 |
0.844 |
0.607 |
0.491 |
0.389 |
|
|
| Concentration = 0.99 |
|
| |
Pinch (K) |
| |
2.47 |
3 |
5 |
7 |
10 |
| UA |
7857.926 |
951.709 |
330.693 |
206.368 |
132.644 |
| UALMTD |
100.793 |
94.104 |
77.017 |
66.259 |
55.415 |
| LER |
1.892 |
1.005 |
0.633 |
0.493 |
0.379 |
The UAs at the smallest pinch points may appear to be excessive,
but this is because the streams at these points only narrowly avoid converging
in temperature. For the water and refrigerant streams to actually converge
to the same temperature, the heat exchanger area would need to be infinite,
a reality reflected in the large actual UAs.
Other Refrigerants
Properties
Table 5.3: HCFC-22 Alternatives
| # |
Comp. 1 |
Comp. 2 |
Comp. 3 |
Mass % 1 |
Mass % 2 |
Mass % 3 |
Name |
| 1 |
32 |
125 |
134a |
0.23 |
0.25 |
0.52 |
407c |
| 2 |
32 |
125 |
134a |
0.3 |
0.1 |
0.6 |
|
| 3 |
32 |
152a |
124 |
0.2 |
0.2 |
0.6 |
|
| 4 |
32 |
152a |
134 |
0.3 |
0.4 |
0.3 |
|
| 5 |
32 |
152a |
134a |
0.4 |
0.5 |
0.1 |
|
| 6 |
32 |
125 |
134a |
0.1 |
0.7 |
0.2 |
407b |
| 7 |
125 |
143a |
134a |
0.4 |
0.45 |
0.15 |
|
| 8 |
32 |
134 |
n/a |
0.5 |
0.5 |
n/a |
|
| 9 |
32 |
125 |
n/a |
0.5 |
0.5 |
n/a |
410A |
In addition to ammonia-water mixtures, zeotropic and near-azeotropic
refrigerant mixtures that are currently under consideration as replacements
for HCFC-22 were also analyzed. A literature search was conducted, and
the most promising and/or widely endorsed mixtures were chosen for study,
and are listed in Table 5.3 (all refrigerants
will henceforth be referred to by their reference number). Refrigerants
1 and 8 are currently being considered by DuPont (Bivens,
1997), and refrigerant 9 (also known as AZ-20) has been developed by
Allied Signal, two of the largest refrigerant producers in the United States.
Refrigerants 3 through 5 were designated by Radermacher
& Jung in their comprehensive survey (1993)
as the most promising three-component blends. Refrigerant 2 was endorsed
by Mei et al. in a follow-up study to
that survey (1995). Refrigerant 2 was
also earlier advocated by the Air Conditioning and Refrigeration Institute
(ARI), as were refrigerants 6 and 7 (Kondepudi,
1992).
Each refrigerant was analyzed at pinch points of 2 to 7 K at
the mixture inlet. Refrigerant 9 is an exception to this; due to its concave
rather than convex temperature profile, its pinch was specified at the
mixture outlet. Throughout this range, the properties of these refrigerants
varied widely, as did their operating pressures and temperature glides.
The glides were much smaller than those observed for NH3/H2O,
but the pressures were considerably higher. Tables 5.4
- 5.5 contain a complete list of the pressures
and glides for comparison purposes. Note that the temperature glides are
in the range of 5 to 10 °C,
and that the pressures are listed in kPa rather than bar.
The linearity of temperature versus enthalpy has increased, as can be seen
at a pinch of 5 K for three of refrigerants in Figure 5.4,
but there is still the possibility of an interior pinch. For each refrigerant
and pinch, the EES program found in Appendix C
was executed.
Table 5.4: Operating Pressures and Temperature Glides for
Refrigerants 1-5
| Refrigerant # 1
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| P (kPa) |
1399.839 |
1436.386 |
1473.632 |
1511.587 |
1550.259 |
1589.655 |
| Tglide (K) |
5.189 |
5.154 |
5.118 |
5.081 |
5.044 |
5.006 |
|
|
| Refrigerant # 2
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| P (kPa) |
1381.817 |
1418.121 |
1455.124 |
1492.835 |
1531.262 |
1570.413 |
| Tglide (K) |
5.447 |
5.412 |
5.377 |
5.341 |
5.305 |
5.268 |
|
|
| Refrigerant # 3
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| P (kPa) |
1093.765 |
1121.81 |
1150.374 |
1179.461 |
1209.076 |
1239.226 |
| Tglide (K) |
10.07 |
10.03 |
9.988 |
9.947 |
9.904 |
9.86 |
|
|
| Refrigerant # 4
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| P (kPa) |
1128.243 |
1158.306 |
1188.955 |
1220.198 |
1252.042 |
1284.492 |
| Tglide (K) |
5.971 |
5.938 |
5.904 |
5.87 |
5.835 |
5.799 |
|
|
| Refrigerant # 5
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| P (kPa) |
1240.457 |
1273.366 |
1306.912 |
1341.105 |
1375.951 |
1411.458 |
| Tglide (K) |
6.879 |
6.849 |
6.819 |
6.789 |
6.758 |
6.726 |
Table 5.5: Operating Pressures and Temperature Glides for
Refrigerants 6-9
| Refrigerant # 6
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| P (kPa) |
n/a |
1593.875 |
1634.642 |
1676.177 |
1718.489 |
1761.588 |
| Tglide (K) |
n/a |
2.813 |
2.787 |
2.759 |
2.732 |
2.704 |
|
|
| Refrigerant # 7
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| P (kPa) |
n/a |
n/a |
1499.032 |
1537.131 |
1575.948 |
1615.493 |
| Tglide (K) |
n/a |
n/a |
1.245 |
1.228 |
1.212 |
1.196 |
|
|
| Refrigerant # 8
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| P (kPa) |
1511.117 |
1550.362 |
1590.347 |
1631.08 |
1672.57 |
1714.824 |
| Tglide (K) |
8.347 |
8.302 |
8.257 |
8.211 |
8.164 |
8.116 |
|
|
| Refrigerant # 9
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| P (kPa) |
2197.791 |
2252.694 |
2308.622 |
2365.586 |
2423.6 |
2482.678 |
| Tglide (K) |
0.116 |
0.116 |
0.116 |
0.115 |
0.115 |
0.114 |
Figure 5.4: Nonlinearity of Refrigerants 1, 6, and 8
 |
Standard Error for R-22 Alternatives
Table 5.6: UA and UALMTD for Refrigerants
1-5
| Refrigerant # 1
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| UA |
7254.367 |
4935.324 |
3727.552 |
2986.106 |
2484.39 |
2122.149 |
| UALMTD |
7157.052 |
4891.5665 |
3703.247 |
2970.873 |
2474.0563 |
2114.772 |
|
|
| Refrigerant # 2
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| UA |
6840.15 |
4772.05 |
3655.525 |
2955.366 |
2474.807 |
2124.406 |
| UALMTD |
6840.782 |
4774.1654 |
3657.343 |
2956.769 |
2475.9275 |
2125.29 |
|
|
| Refrigerant # 3
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| UA |
3466.033 |
2816.027 |
2389.221 |
2080.984 |
1845.409 |
1658.438 |
| UALMTD |
3692.544 |
2971.2297 |
2503.058 |
2168.255 |
1914.4263 |
1714.205 |
|
|
| Refrigerant # 4
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| UA |
5032.711 |
3855.596 |
3131.735 |
2636.972 |
2275.836 |
1999.993 |
| UALMTD |
5437.96 |
4092.7362 |
3287.357 |
2746.599 |
2356.9411 |
2062.201 |
|
|
| Refrigerant # 5
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| UA |
5676.224 |
4212.46 |
3350.749 |
2779.464 |
2371.927 |
2066.072 |
| UALMTD |
5933.173 |
4355.0611 |
3441.034 |
2841.484 |
2416.9026 |
2100.036 |
Table 5.7: UA and UALMTD for Refrigerants
6-9
| Refrigerant # 6
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| UA |
n/a |
9792.723 |
5349.748 |
3735.791 |
2870.195 |
2324.879 |
| UALMTD |
n/a |
9152.4246 |
5153.854 |
3640.876 |
2814.8496 |
2289.129 |
|
|
| Refrigerant # 7
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| UA |
n/a |
n/a |
11946.56 |
5327.101 |
3671.643 |
2822.269 |
| UALMTD |
n/a |
n/a |
11423.38 |
5217.044 |
3619.7126 |
2792.065 |
|
|
| Refrigerant # 8
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| UA |
5465.339 |
4024.631 |
3193.355 |
2646.892 |
2258.31 |
1967.168 |
| UALMTD |
4841.3632 |
3680.786 |
2975.881 |
2497.552 |
2149.9769 |
1885.358 |
|
|
| Refrigerant # 9
|
|
| |
Pinch (K) |
| |
2 |
3 |
4 |
5 |
6 |
7 |
| UA |
3213.858 |
2483.476 |
2027.328 |
1711.092 |
1477.374 |
1296.872 |
| UALMTD |
3210.3017 |
2481.3435 |
2025.898 |
1710.07 |
1476.6088 |
1296.289 |
As would be expected from the smaller temperature glides, the UA
error for refrigerants 1 through 9 is less than for NH3/H2O.
The magnitude of the differences can be seen in Tables 5.6
- 5.7.
Table 5.8: Standard Error for Refrigerants 1-9
| |
Pinch (K) |
| Number |
2 |
3 |
4 |
5 |
6 |
7 |
| 1 |
1.341 |
0.887 |
0.652 |
0.510 |
0.416 |
0.348 |
| 2 |
0.009 |
0.044 |
0.050 |
0.047 |
0.045 |
0.042 |
| 3 |
6.535 |
5.511 |
4.765 |
4.194 |
3.740 |
3.363 |
| 4 |
8.052 |
6.151 |
4.969 |
4.157 |
3.564 |
3.110 |
| 5 |
4.527 |
3.385 |
2.694 |
2.231 |
1.896 |
1.644 |
| 6 |
n/a |
6.539 |
3.662 |
2.541 |
1.928 |
1.538 |
| 7 |
n/a |
n/a |
4.379 |
2.066 |
1.414 |
1.070 |
| 8 |
11.417 |
8.544 |
6.810 |
5.642 |
4.797 |
4.159 |
| 9 |
0.111 |
0.086 |
0.071 |
0.060 |
0.052 |
0.045 |
Figure 5.5: Standard Error for Refrigerants 1-3
 |
Figure 5.6: Standard Error for Refrigerants 4-6
 |
Figure 5.7: Standard Error for Refrigerants 7-9
 |
Because |UA - UALMTD| is relatively small,
the standard error calculation will produce values that are easy to evaluate
both numerically (Table 5.8) and graphically
(Figures 5.5 - 5.7).
When a table entry is marked not applicable, an infeasible interior pinch
was generated.
Drop-In Replacements vs. System
Reconfiguration
In the search for alternatives to R-22, a primary
objective of the refrigeration industry has been the discovery of a ``drop-in''
replacement. A drop-in replacement is one that:
1) operates under very similar pressures to,
2) has chemical properties compatible with the equipment used with,
and
3) provides a refrigeration capacity at the level of
the refrigerant that it replaces. While R-134a has proven to be a successful
drop-in replacement for CFC-12, no completely satisfactory drop-in replacement
has been found for R-22. However, both R-407c and R-410a work fairly well
for selected applications, and are likely to become the preferred replacements
for existing systems.
Zeotropes and near-azeotropes should not just be thought of as straight
replacements, though. For a pure refrigerant, there is usually a trade-off
between improving the efficiency and the volumetric capacity. Zeotropic
mixtures can mitigate this somewhat (Didion
& Bivens, 1990). A zeotropic mixture in the two-phase region constantly
changes its composition as temperature changes, making it possible to control
composition during operation.
Figure 5.8: Carnot and Lorenz Cycle Diagrams
 |
The greatest potential, though, is a result of a zeotrope's gliding
temperature. When properly utilized, this can actually result in efficiencies
that are higher than those demonstrated by R-22. The diagram for a Lorenz
cycle demonstrates that entropy generation can be reduced (below that of
a Carnot cycle) if temperature profiles are properly matched (Figure 5.8).
The Lorenz cycle consists of two constant-entropy adiabatic expansion or
compression processes and two constant-heat capacity heat transfer processes
(Cavallini, 1996).
Unfortunately, the nonlinearity of the temperature versus the enthalpy
creates difficulties in accurately matching the profiles for a Lorenz cycle.
Three ways to correct this are through chemical, mechanical, and thermal
controls. The chemical approach uses an additional component to linearize
the temperature profile. The mechanical approach cuts off the phase-change
process so that the majority of the heat exchanger has a minimum temperature
difference. The thermal approach adds additional heat processes so that
the heat exchange avoids pinch points. Each of these approaches also has
the advantage of separating the interdependency of the composition and
temperature glides (Didion & Bivens,
1990).
Figure 5.9: The Liquid-Line/Suction-Line Heat Exchanger
 |
Figure 5.10: The Desorber-Absorber Heat Exchange Cycle
 |
The characteristics of zeotropes and near-azeotropes can also be exploited
in other ways. For example, the addition of a liquid-line/suction-line
heat exchanger (Figure 5.9) results in
impressive efficiency improvements. The idea of a desorber-absorber heat
exchange cycle (Figure 5.10) is fairly old,
but it can take unique advantage of zeotropic properties.
Whatever cycle is chosen, the results of this study can be used to more
accurately determine the size of the heat exchangers.
Next: Conclusions
and Recommendations Up: Heat
Exchanger Mean Temperature Previous: Application
of the Numerical Technique
Laura Atkinson Schaefer
12/3/1997