************************************* Gas heat pump and refrigeration cycle ************************************* *Gas heat pumps* and *gas regrigerators* are basically following the reverse **Brayton cycle** (or Joule cycle). .. _Fig:chap5:BraytonReverse: .. figure:: ./_static/fig/chap5/BraytonReverse.png :scale: 30% :align: center Reverse *Brayton* cycle for gas refrigeration. As for any heat pump or refrigerator, (:eq:`COPr`, and :eq:`COPhp`) the *coefficients of performance* of *Reverse Brayton cycle* are: .. math:: COP_{R,Joule} = \frac{1}{\frac{|q_{23}|}{|q_{41}|}-1} \qquad \text{and} \qquad COP_{HP,Joule} = \frac{1}{1-\frac{|q_{41}|}{|q_{23}|}} Considering the working fluid as an **ideal gas**, and because no machine is working in transformations 2-3 and 4-1, application of the balance energy equation reads: .. math:: |q_{23}| = \dot{m} c_p (T_2-T_3) \qquad \text{ and } \qquad |q_{41}| = \dot{m} c_p (T_1-T_4) such that the COPs of *Reverse Brayton cycle* become: .. math:: COP_{R,Joule} = \frac{1}{\frac{T_2-T_3}{T_1-T_4}-1} \qquad \text{and} \qquad COP_{HP,Joule} = \frac{1}{1-\frac{T_1-T_4}{T_2-T_3}} As for gas turbine, it is possible to determine gas temperatures after the compressor and the turbine thanks to isentropic relations for ideal gases: .. math:: \frac{T_1}{T_2} = \frac{p_2}{p_1}^{\frac{1-\gamma}{\gamma}} = \frac{p_3}{p_4}^{\frac{1 - \gamma}{\gamma}} = \frac{T_4}{T_3} we finally obtain: .. math:: :label: COPEffBraytonIGRev COP_{R,Joule} = \frac{1}{r_p^{\frac{\gamma-1}{\gamma}}-1} \qquad \text{and} \qquad COP_{HP,Joule} = \frac{1}{1-r_p^{\frac{1-\gamma}{\gamma}}} where :math:`r_p=\frac{p_2}{p_1}` is the **pressure ratio**. .. _Fig:chap5:COPJoule: .. figure:: ./_static/fig/chap5/COPJoule.png :scale: 50% :align: center COP for *reverse Brayton cycle* (Joule cycle) for heat pump or refrigerators as a function of the pressure ratio for IG with :math:`\gamma=1.4`. :numref:`Fig:chap5:COPJoule` reveals that the performance of such machine is good for low pressure ratio. .. admonition:: Remarks * As for gas turbine, it is possible to easily account for the adiabatic compressor and adiabatic turbine irreversibilities by using the isentropic efficiency of both components (see :numref:`Sec:chap4:RealGasTurbineCycle`). * It is also possible to improve the cycle using **regeneration** (see :numref:`Sec:chap4:regeneration`) * Heat pumps and Refrigerators using the *reverse Brayton cycle* have low performances and are used only for specific applications.