Consider that the air in the previous problem after the compressor flows in a pipe to an air tool and at that point the temperature has dropped to ambient 540 R and an air pressure of 110 psia. What is the second law efficiency for the total system?
Consider that the air in the previous problem after the compressor flows in a pipe to an air tool and at that point the temperature has dropped to ambient 540 R and an air pressure of 110 psia. What is the second law efficiency for the total system?
C.V. Compressor
Energy: 0=h_{1}-h_{2}+w_{C}; Entropy: 0=s_{1}-s_{2}+0
T _{2}= T _{1}\left(\frac{ P _{2}}{ P _{1}}\right)^{\frac{ k -1}{ k }}=540\left(\frac{120}{15}\right)^{0.2857}=978.1 RExergy increase through the compressor matches with the ideal compressor work
w _{ C s }= h _{2}- h _{1}= C _{ P }\left( T _{2}- T _{1}\right)=0.24(978.1-540) Btu / lbm =105.14 Btu/lbmThe actual compressor work is
w _{ C a c }= w _{ C s } / \eta_{ C s }=105.14 / 0.85=123.7 Btu / lbmFrom inlet, state 1 to final point of use state 3.
\begin{aligned}\psi_{3}-\psi_{1} &=\left( h _{3}- h _{1}\right)- T _{0}\left( s _{3}- s _{1}\right)=0- T _{0}\left[0- R \ln \left( P _{3} / P _{1}\right)\right] \\&= T _{0} R \ln \left( P _{3} / P _{1}\right)=537 R \times(53.34 / 778) Btu / lbmR \times \ln (110 / 15) \\&=73.36 Btu / lbm\end{aligned}So then the second law efficiency is the gain \left(\psi_{3}-\psi_{1}\right) over the source w _{ C ac } as
\eta_{ II }=\frac{\psi_{3}-\psi_{1}}{ w _{ C a c }}=\frac{73.36}{123.7}= 0 . 5 9