Thermodynamics: An Engineering Approach 8th Edition

Published by McGraw-Hill Education
ISBN 10: 0-07339-817-9
ISBN 13: 978-0-07339-817-4

Chapter 10 - Vapor and Combined Power Cycles - Problems - Page 592: 10-25

Answer

$n_{T}=0.788$ $\dot{W}_{\text {net }}=20,165\text{ kW}$ $\eta_{\text {th }}=12.4\%$

Work Step by Step

(a) We need properties of isobutane, which are not available in the book. However, we can obtain the properties from EES. Turbine: $$ \begin{aligned} & P_3=3250\ \mathrm{kPa} \mid h_3=761.54 \mathrm{~kJ} / \mathrm{kg} \\ & \left.T_3=147^{\circ} \mathrm{C} \quad\right\} s_3=2.5457 \mathrm{~kJ} / \mathrm{kg} \cdot \mathrm{K} \\ & \left.\begin{array}{l} P_4=410\ \mathrm{kPa} \\ s_4=s_3 \end{array}\right\} h_{4 s}=670.40 \mathrm{~kJ} / \mathrm{kg} \\ & \left.\begin{array}{l} P_4=410 \mathrm{kPa} \\ T_4=179.5^{\circ} \mathrm{C} \end{array}\right\} h_4=689.74 \mathrm{~kJ} / \mathrm{kg} \\ & \eta_T=\frac{h_3-h_4}{h_3-h_{4 s}}=\frac{761.54-689.74}{761.54-670.40}=\mathbf{0 . 7 8 8} \end{aligned} $$ (b) Pump: $$ \begin{aligned} & h_1=h_{f$410 \mathrm{kPa}}=273.01 \mathrm{~kJ} / \mathrm{kg} \\ & v_1=v_{f@410 \mathrm{kPa}}=0.001842 \mathrm{~m}^3 / \mathrm{kg} \\ & w_{p, \text { in }}=v_1\left(P_2-P_1\right) / \eta_P \\ & =\left(0.001842 \mathrm{~m}^3 / \mathrm{kg}\right)(3250-410) \mathrm{kPa}\left(\frac{1 \mathrm{~kJ}}{1 \mathrm{kPa} \cdot \mathrm{m}^3}\right) / 0.90 \\ & =5.81 \mathrm{~kJ} / \mathrm{kg} \\ & h_2=h_1+w_{\rho \text { in }}=273.01+5.81=278.82 \mathrm{~kJ} / \mathrm{kg} \end{aligned} $$ $$ \begin{aligned} & \dot{W}_{\mathrm{T}, \text { out }}=\dot{m}\left(h_3-h_4\right)=(305.6 \mathrm{~kJ} / \mathrm{kg})(761.54-689.74) \mathrm{kJ} / \mathrm{kg}=21,941 \mathrm{~kW} \\ & \dot{W}_{\mathrm{P}, \mathrm{in}}=\dot{m}\left(h_2-h_1\right)=\dot{m} w_{\mathrm{p} \text { in }}=(305.6 \mathrm{~kJ} / \mathrm{kg})(5.81 \mathrm{~kJ} / \mathrm{kg})=1777 \mathrm{~kW} \\ & \dot{W}_{\text {net }}=\dot{W}_{\mathrm{T}, \text { out }}-\dot{W}_{\mathrm{P}, \text { in }}=21,941-1777=\mathbf{2 0 , 1 6 5} \mathbf{k W} \end{aligned} $$ Heat Exchanger: $$ \dot{Q}_{\text {in }}=\dot{m}_{\text {geo }} c_{\text {geo }}\left(T_{\text {in }}-T_{\text {eut }}\right)=(555.9 \mathrm{~kJ} / \mathrm{kg})\left(4.18 \mathrm{~kJ} / \mathrm{kg} \cdot{ }^{\circ} \mathrm{C}\right)(160-90)^{\circ} \mathrm{C}=162,656 \mathrm{~kW} $$ (c) $$ \eta_{\text {th }}=\frac{\dot{W}_{\text {net }}}{\dot{Q}_{\text {in }}}=\frac{20,165}{162,656}=\mathbf{0 . 1 2 4}=12.4 \% $$
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