water outlet 908 to the cooling water tower u2014 not shown the whole skid mounted unit is surrounded by a modular container 101 having two separate doorway entries 103 and 105 such ancillary equipment as control valves lighting and ventilation may be included but are not shown also conspicuously shown are the redundancy of the pumps and compressors the modular unit includes the ability to automatically switch from one to the other upon failure or shut down of the one operating referring now to fig3 a flow diagram of the combustion gas turbine inlet air cooling process utilizing the present invention is shown the process begins with heat being removed from the combustion gas turbine 26 inlet air through the fin tube heat exchanger 31 commonly called the inlet chilling coils this heat is transferred from the inlet chilling coils 31 to the chilling fluid and is carried to the chilling process through the liquid return line 38 where it enters the operating chilled liquid pump 110 or 112 noting that one pump is 100 stand by an isolation valve 10 is provided to facilitate pump service the fluid is pumped through vibration isolator 6 check valve 15 balancing isolation valve 10 u2032 and into the basic liquid chilling unit heat exchanger section 122 evaporator where heat is removed by indirect contact with evaporating refrigerant the refrigerant is compressed in either of compressor 118 or 120 and then condensed in condenser 124 where the heat is removed by condenser water which in turn is cooled in the cooling tower 29 through an evaporative process adiabatic thereby reducing the condenser water temperature to acceptable levels and which is returned to.