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62c67d | João Lopes | 2025-03-13 12:01:58 | 1 |  |
374ad8 | João Lopes | 2025-03-13 11:57:41 | 2 | |
3 | > Departamento de Engenharia Química |
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4 | > |
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5 | > Mestrado Integrado em Engenharia Química |
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6 | > |
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7 | > Integração e intensificação de processos |
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8 | > |
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9 | > Shell and Tubes Heat Exchangers |
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10 | > |
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11 | > **Docente** **Responsável:** |
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12 | > |
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13 | > Nuno Manuel Clemente de Oliveira |
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14 | > |
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15 | > **Integrantes** **do** **grupo:** |
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16 | ||||
17 | João Victor Vieira |
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18 | ||||
19 | > Matteo Gecchele |
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20 | ||||
21 | ||||
22 | > **Introduction** **&** **Structure** |
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23 | > |
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24 | > The most common type of heat exchanger is the shell-and-tube, usually |
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25 | > used in a lot of industrial applications. This type of heat exchanger |
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26 | > has large number of tubes, sometimes several hundred, packed in a |
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27 | > shell with their axes parallel to that of the shell. The heat transfer |
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28 | > takes place between two fluid, one flowing inside the tubes and one |
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29 | > flowing outside the tubes through the shell. Baffles are commonly |
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30 | > placed in the shell to force the shell-side fluid to flow across the |
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31 | > shell to enhance heat transfer, to maintain uniform spacing between |
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32 | > the tubes and, also in order to maintain the turbulent flow inside the |
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33 | > exchanger. The baffle spacing is usually not greater than a distance |
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34 | > equal to the inside diameter or closer than a distance equal to |
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35 | > one-fifth the inside diameter of the shell. |
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36 | > |
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37 | > Usually the shell-and-tube heat exchangers have large size and weight, |
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38 | > and for this reason they are not using in automotive and aircraft |
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39 | > applications. At both ends of the shell, the tubes open to some large |
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40 | > flow areas, called headers, where the tube-side fluid accumulates |
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41 | > before entering the tubes and after leaving them. |
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62c67d | João Lopes | 2025-03-13 12:01:58 | 42 | > |
5b9f6d | João Lopes | 2025-03-13 12:02:35 | 43 | > |
374ad8 | João Lopes | 2025-03-13 11:57:41 | 44 | > Shell-and-tube heat exchangers are further classified according to the |
45 | > number of shell and tube passes involved. Heat exchangers in which all |
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46 | > the tubes make one U-turn in the shell, for example, are called |
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47 | > one-shell-pass and two-tube-passes heat exchangers. Likewise, a heat |
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48 | > exchanger that involves two passes in the shell and four passes in the |
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49 | > tubes is called a two-shell- passes and four-tube-passes heat |
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50 | > exchanger. |
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51 | ||||
62c67d | João Lopes | 2025-03-13 12:01:58 | 52 |  |
53 | ||||
374ad8 | João Lopes | 2025-03-13 11:57:41 | 54 | |
55 | > **Operation** **principle** |
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56 | > |
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57 | > In order to calculate the temperature difference ∆𝑡 in a 1-2 |
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58 | > exchanger, it is necessary to make some assumptions: |
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59 | > |
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60 | > 1\. The shell fluid temperature is an average isothermal temperature |
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61 | > at any cross section |
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62 | > |
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63 | > 2\. There is an equal amount of heating surface in each pass 3. The |
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64 | > overall coefficient of heat transfer is constant |
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65 | > |
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66 | > 4\. The specific heat of each fluid is constant 5. The flowrate of |
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67 | > each fluid is constant |
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68 | > |
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69 | > 6\. There are not phase change (evaporation or condensation) in a part |
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70 | > of the exchanger |
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71 | > |
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72 | > 7\. Heat losses are negligible |
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73 | > |
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74 | > The overall heat balance where ∆𝑡 is the true difference of |
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75 | > temperatures, is: |
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76 | > |
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77 | > 𝑄 = 𝑈𝐴∆𝑡 = 𝑊𝐶(𝑇 − 𝑇 ) = 𝑤𝑐(𝑡2 − 𝑡1) where U is the heat transfer |
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78 | > coefficient and A is the surface of contact. |
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79 | > |
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80 | > Shell-and-tube heat exchangers are complicated devices and the |
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81 | > simplified approaches should be used with care. In fact, it is assumed |
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82 | > that the overall heat transfer coefficient U is constant throughout |
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83 | > the heat exchanger and that the convection heat transfer coefficients |
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84 | > can be predicted using the convection correlations. However, in some |
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85 | > practical application, the predicted value of U can exceed 30 percent. |
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86 | > Thus, it is natural to tend to overdesign the heat exchangers in order |
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87 | > to avoid unpleasant surprises. |
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88 | > |
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89 | > Heat transfer enhancement in heat exchangers is usually accompanied by |
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90 | > increased |
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91 | > |
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92 | > pressure drop, and this causes higher pumping power. Therefore, any |
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93 | > gain from the enhancement in heat transfer should be balanced against |
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94 | > the cost of the accompanying pressure drop. Also, some thought should |
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95 | > be given to which fluid should pass through the tube side and which |
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96 | > through the shell side. Usually, the more viscous fluid is more |
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97 | > suitable for the shell side (larger passage area and lower pressure |
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98 | > drop) and the fluid with the higher pressure for the tube side. |
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99 | > |
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100 | > Usually, it is convenient to relate the equivalent temperature |
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101 | > difference to the log |
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102 | > |
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103 | > mean temperature difference relation for the counter-flow case as |
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104 | > |
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105 | > ∆ 𝑙𝑚 = 𝐹∆ 𝑙𝑚,𝐶𝐹 |
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106 | ||||
107 | where *F* is the correction factor**,** which depends on the geometry of |
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108 | the heat exchanger and the inlet and outlet temperatures of the hot and |
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109 | cold fluid streams. The |
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110 | ||||
111 | > ∆𝑇𝑚,𝐶𝐹 is the log mean temperature difference for the case of a |
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112 | > counter-flow heat exchanger with the same inlet and outlet |
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113 | > temperatures. |
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114 | > |
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115 | > The correction factor *F* for a shell-and-tube heat exchanger is shown |
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116 | > in the figures below versus two temperature ratios *P* and *R* defined |
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117 | > as |
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118 | > |
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119 | > 𝑡2 − 𝑡1 𝑇 − 𝑡1 |
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120 | > |
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121 | > 𝑇 − 𝑇 𝑡2 − 𝑡1 |
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122 | > |
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123 | > where the subscripts 1 and 2 represent the inlet and outlet*,* |
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124 | > respectively. Note that for |
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125 | > |
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126 | > a shell-and-tube heat exchanger, *T* and *t* represent the shell-side |
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127 | > and tube-side temperatures, respectively. |
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128 | ||||
62c67d | João Lopes | 2025-03-13 12:01:58 | 129 |  |
374ad8 | João Lopes | 2025-03-13 11:57:41 | 130 | |
131 | > **Factors** **that** **influence** **performances** *Fouling:* |
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132 | > |
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133 | > The performance of heat exchangers usually deteriorates with time as a |
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134 | > result of accumulation of deposits on heat transfer surfaces. The |
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135 | > layer of deposits represents additional resistance to heat transfer |
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136 | > and this causes a decrease of the rate of heat transfer in a heat |
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137 | > exchanger. The net effect of these accumulations on heat transfer is |
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138 | > represented by a fouling factor, which is a measure of the thermal |
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139 | > resistance introduced by fouling. |
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140 | > |
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141 | > For a shell-and-tube heat exchanger it possible to write the overall |
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142 | > heat transfer relation as |
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143 | > |
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144 | > 𝑈𝐴𝑠 = 𝑈𝐴𝑖 = 𝑈0𝐴0 = 𝑅 = ℎ𝑖𝐴𝑖 + 𝐴𝑖𝑖 + ln𝑈0𝐴0 𝑖) + 𝐴0 + ℎ0𝐴0 |
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145 | > |
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146 | > where 𝐴𝑖 = 𝐷𝐿 and 𝐴0 = 𝐷0𝐿 L are the areas of inner and outer |
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147 | > surfaces, and 𝑅,𝑖 and 𝑅,0 are the fouling factors at those surfaces. |
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148 | > |
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149 | > *Heat* *transfer* *rate:* |
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150 | > |
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151 | > The heat transfer rate is the most important parameter of a heat |
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152 | > exchanger. A heat exchanger should be capable of transferring heat at |
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153 | > the specified rate in order to achieve the desired temperature change |
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154 | > of the fluid at the specified mass flow rate. |
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155 | > |
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156 | > *Size* *and* *Weight:* |
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157 | > |
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158 | > The heat exchanger is better if it is smaller and lighter, in |
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159 | > particular, in the automotive and aerospace industries, where size and |
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160 | > weight requirements are most stringent. For this reason, |
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161 | > shell-and-tube heat exchangers cannot be used in this type of |
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162 | > application. Also, a larger heat exchanger normally carries a higher |
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163 | > price tag. The space available for the heat exchanger in some cases |
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164 | > limits the length of the tubes that can be used. |
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165 | > |
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166 | > *Material:* |
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167 | > |
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168 | > The thermal and structural stress effects need not be considered at |
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169 | > pressures below 15 *atm* or temperatures below 150*°C*. But these |
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170 | > effects are major considerations above 70 *atm* or 550*°C* and |
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171 | > seriously limit the acceptable materials of the heat exchanger. |
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172 | > |
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173 | > A temperature difference of 50*°C* or more between the tubes and the |
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174 | > shell will probably pose differential thermal expansion problems and |
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175 | > needs to be considered. In the case of corrosive fluids, we may have |
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176 | > to select expensive corrosion-resistant materials such as stainless |
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177 | > steel or even titanium. |
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178 | > |
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179 | > **Cost** |
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180 | > |
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181 | > The purchase cost of a shell and tube depends on the rear head type |
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182 | > and on the heat transfer |
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183 | > |
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184 | > area (size factor). The relationship between the purchase cost and the |
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185 | > size factor is |
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186 | > |
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187 | > represented in the graph below |
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188 | ||||
62c67d | João Lopes | 2025-03-13 12:01:58 | 189 |  |
374ad8 | João Lopes | 2025-03-13 11:57:41 | 190 | |
191 | > Both fluids are usually forced to flow by pumps or fans that consume |
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192 | > electrical power. The annual cost of electricity associated with the |
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193 | > operation of the pumps and fans can be determined from |
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194 | > |
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195 | > 𝑂𝑝𝑒𝑟𝑎𝑡𝑖𝑛𝑔𝐶𝑜𝑠𝑡 = 𝑃𝑢𝑚𝑝𝑖𝑛𝑔𝑃𝑜𝑤𝑒𝑟\[𝑘𝑊\] × 𝐻𝑜𝑢𝑟𝑠𝑜𝑓𝑂𝑝𝑒𝑟𝑎𝑡𝑖𝑜𝑛\[ℎ\] × |
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196 | > 𝑃𝑟𝑖𝑐𝑒𝑜𝑓𝐸𝑙𝑒𝑐𝑟𝑖𝑐𝑖𝑡𝑦\[\$ 𝑘𝑊ℎ\] |
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197 | > |
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198 | > where the pumping power is the total electrical power consumed by the |
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199 | > motors of the pumps and fans. |
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200 | > |
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201 | > Minimizing the pressure drop and the mass flow rate of the fluids will |
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202 | > minimize the operating cost of the heat exchanger, but it will |
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203 | > maximize the size of the heat exchanger and thus the initial cost. As |
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204 | > a rule of thumb, doubling the mass flow rate will reduce the initial |
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205 | > cost by half but will increase the pumping power requirements by a |
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206 | > factor of roughly eight. Typically, fluid velocities encountered in |
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207 | > heat exchangers range between 0.7 and 7 m/s for liquids and between 3 |
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208 | > and 30 m/s for gases. Low velocities are helpful in avoiding erosion, |
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209 | > tube vibrations, and noise as well as pressure drop. |
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210 | > |
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211 | > **Advantages**: |
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212 | > |
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213 | > *Size:* |
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214 | > |
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215 | > Shell-and-tube heat exchangers are capable of providing a larger |
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216 | > surface area for heat transfer to take place while having a shorter |
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217 | > length overall due to presence of multiple tubes. |
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218 | > |
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219 | > *Heat* *duty:* |
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220 | > |
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221 | > Shell-and-tube heat exchangers can handle higher temperatures and |
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222 | > pressures and hence higher heat duty. This is because besides |
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223 | > providing a higher overall heat transfer coefficient, additions can |
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224 | > also be made to negate thermal expansion effects and the thickness can |
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225 | > also be varied (more in the next point). |
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226 | > |
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227 | > *Versatility:* |
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228 | > |
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229 | > From the design point of view, shell-and-tube heat exchangers are the |
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230 | > most versatile of all heat exchangers. Being tubular in shape, heads / |
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231 | > closures of required shape and thickness can be used. The number of |
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232 | > tubes and tube pitch can be selected according to operating |
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233 | > conditions. Expansion bellows can be used to negate thermal expansion |
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234 | > effects, baffles if different cuts and spacings can be used to |
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235 | > influence the overall heat transfer coefficients and there's even |
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236 | > something called a floating head which can be added to negate thermal |
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237 | > expansion of the tubes. The number of passes on shell side and tube |
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238 | > side can be altered as well. |
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239 | > |
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240 | > **Disadvantages**: |
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241 | > |
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242 | > *Size:* |
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243 | > |
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244 | > This can also be a disadvantage as at lower heat duty, there are more |
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245 | > compact heat exchangers such as plate type exchanger. Also, the |
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246 | > absence of hairpin bends causes shell-and-tube heat exchangers to take |
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247 | > up more space than double pipe heat exchangers in some cases. |
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248 | > |
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249 | > *Maintenance:* |
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250 | > |
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251 | > Cleaning of tubes is difficult and fouling is always an issue when |
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252 | > overall heat transfer coefficient is addressed. This requires periodic |
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253 | > cleaning of the shell as well as the tubes. Cleaning tubes may be more |
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254 | > difficult if the pitch is triangular. |
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255 | > |
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256 | > **Utilities** |
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257 | > |
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258 | > The selection of utilities to be used in the shell and tubes tube |
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259 | > exchanger takes into |
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260 | > |
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261 | > account the type of industry in which it is being operated and the |
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262 | > desired parameters, such as the required power, thermal stability and |
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263 | > thermal capacity. |
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264 | > |
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265 | > *Cooling* *Water*: |
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266 | > |
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267 | > Cooling water is used to cool and/or condense currents. The cooling |
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268 | > water circulates inside heat exchangers. About 80% of the temperature |
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269 | > reduction is due to the evaporation of the cooling water and the |
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270 | > transfer of heat to the surrounding air. |
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271 | > |
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272 | > *Steam:* |
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273 | > |
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274 | > Steam is the most common heat utility used in the chemical industry |
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275 | > and can be used to power pumps, compressors and heat exchangers. Using |
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276 | > steam allows a more efficient heat source since the heat of |
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277 | > condensation of the steam is quite high, which translates into a high |
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278 | > yield per utility mass, at a constant temperature. Another reason is |
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279 | > that steam is non-flammable, non-toxic and inert to various process |
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280 | > fluids (more safe than other utilities like oil). |
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281 | > |
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282 | > **Conclusion** |
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283 | > |
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62c67d | João Lopes | 2025-03-13 12:01:58 | 284 | > The simple design of a shell and tube heat exchanger makes it an ideal |
374ad8 | João Lopes | 2025-03-13 11:57:41 | 285 | > cooling solution for a wide variety of applications and as a |
286 | > consequence shell-and-tube heat exchangers are very popular and |
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287 | > commonly found in industrial use. |
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288 | > |
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289 | > **References** |
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290 | > |
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291 | > \[1\] Notes on Transfer Phenomena II, Professor Maria Graça Carvalho, |
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292 | > 2018/2019; |
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293 | > |
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294 | > \[2\] Warren D. Seider, University of Pennsylvania |
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295 | > |
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296 | > \[3\] Heat Transfer by Changel 2nd Edition |
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297 | > |
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298 | > \[4\] Heat Transfer by Holman 6th Edition |