Patent Publication Number: US-11649766-B1

Title: Mobile gas turbine inlet air conditioning system and associated methods

Description:
PRIORITY CLAIMS 
     This is a continuation of U.S. Non-Provisional application Ser. No. 17/954,118, filed Sep. 27, 2022, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” now U.S. Pat. No. 11,598,263 which is a continuation of U.S. Non-Provisional application Ser. No. 17/403,373, filed Aug. 16, 2021, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” now U.S. Pat. No. 11,560,845 which is a continuation of U.S. Non-Provisional application Ser. No. 17/326,711, filed May 21, 2021, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” now U.S. Pat. No. 11,156,159, issued Oct. 26, 2021, which is a continuation U.S. Non-Provisional application Ser. No. 17/213,802, filed Mar. 26, 2021, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” now U.S. Pat. No. 11,060,455, issued Jul. 13, 2021, which is a continuation of U.S. Non-Provisional application Ser. No. 16/948,289, filed Sep. 11, 2020, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” now U.S. Pat. No. 11,002,189, issued May 11, 2021, which claims priority to and the benefit of U.S. Provisional Application No. 62/704,565, filed May 15, 2020, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” and U.S. Provisional Application No. 62/900,291, filed Sep. 13, 2019, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM,” the disclosures of which are incorporated herein by reference in their entireties. 
    
    
     TECHNICAL FIELD 
     In one aspect, the present disclosure relates to a gas turbine and, more particularly, to systems and method for increasing the efficiency of the gas turbine. 
     BACKGROUND 
     The present disclosure relates generally to a turbine such as, but not limiting of, a gas turbine, a bi-fuel turbine, and the like, and may generally include, in serial flow arrangement, an inlet assembly for receiving and channeling an ambient airstream, a compressor which receives and compresses that airstream, a combusting system that mixes a fuel and the compressed airstream, ignites the mixture, and allows for the gaseous by-product to flow to a turbine section, which transfers energy from the gaseous by-product to an output power. 
     For example, a gas turbine engine may be used to supply power to a hydraulic fracturing system. Hydraulic fracturing is an oilfield operation that stimulates production of hydrocarbons, such that the hydrocarbons may more easily or readily flow from a subsurface formation to a well. For example, a fracturing system may be configured to fracture a formation by pumping a fracturing fluid into a well at high pressure and high flow rates. Some fracturing fluids may take the form of a slurry including water, proppants, and/or other additives, such as thickening agents and/or gels. The slurry may be forced via one or more pumps into the formation at rates faster than can be accepted by the existing pores, fractures, faults, or other spaces within the formation. As a result, pressure may build rapidly to the point where the formation may fail and may begin to fracture, thereby releasing the load on the pumps. By continuing to pump the fracturing fluid into the formation, existing fractures in the formation are caused to expand and extend in directions farther away from a well bore, thereby creating flow paths to the well bore. The proppants may serve to prevent the expanded fractures from closing when pumping of the fracturing fluid is ceased or may reduce the extent to which the expanded fractures contract when pumping of the fracturing fluid is ceased. 
     Gas turbine engines may be used to supply power to hydraulic fracturing pumps for pumping the fracturing fluid into the formation. For example, a plurality of gas turbine engines may each be mechanically connected to a corresponding hydraulic fracturing pump via a transmission and operated to drive the hydraulic fracturing pump. The gas turbine engine, hydraulic fracturing pump, transmission, and auxiliary components associated with the gas turbine engine, hydraulic fracturing pump, and transmission may be connected to a common platform or trailer for transportation and set-up as a hydraulic fracturing unit at the site of a fracturing operation, which may include up to a dozen or more of such hydraulic fracturing units operating together to perform the fracturing operation. Once a fracturing operation has been completed, the hydraulic fracturing units may be transported to another geographic location to perform another fracturing operation. 
     Hydraulic fracturing may be performed generally at any geographic location and during any season of the year, often in harsh environmental conditions. As a result, hydraulic fracturing may occur under a wide variety of ambient temperatures and pressures, depending on the location and time of year. In addition, the load on the hydraulic fracturing pumps and thus the gas turbine engines may change or fluctuate greatly, for example, depending on the build-up and release of pressure in the formation being fractured. 
     The performance of a gas turbine engine is dependent on the conditions under which the gas turbine engine operates. For example, ambient air pressure and temperature are large factors in the output of the gas turbine engine, with low ambient air pressure and high ambient temperature reducing the maximum output of the gas turbine engine. Low ambient pressure and/or high ambient temperature reduce the density of air, which reduces the mass flow of the air supplied to the intake of the gas turbine engine for combustion, which results in a lower power output. Some environments in which hydraulic fracturing operations occur are prone to low ambient pressure, for example, at higher elevations, and/or higher temperatures, for example, in hot climates. In addition, gas turbine engines are subject to damage by particulates in air supplied to the intake. Thus, in dusty environments, such as at many well sites, the air must be filtered before entering the intake of the gas turbine engine. However, filtration may reduce the pressure of air supplied to the intake, particularly as the filter medium of the filter becomes obstructed by filtered particulates with use. Reduced power output of the gas turbine engines reduces the pressure and/or flow rate provided by the corresponding hydraulic fracturing pumps of the hydraulic fracturing units. Thus, the effectiveness of a hydraulic fracturing operation may be compromised by reduced power output of the gas turbine engines of the hydraulic fracturing operation. 
     To generate additional power from an existing gas turbine, an inlet air conditioning system may be used. The air conditioning system may increase the airstream density by lowering the temperature of the airstream. This increases the mass flowrate of air entering the compressor, resulting in increased efficiency and power output of the gas turbine. An air conditioning system may include, for example, but not limited to, a chiller, an evaporative cooler, a spray cooler, or combinations thereof, located downstream of an inlet filter house within an inlet assembly of the gas turbine. Some air conditioning systems, however, add resistance to the airstream entering the compressor. This resistance may cause a pressure drop in the inlet assembly. Reduced gas turbine efficiency and power output may result from inlet assembly pressure drop. 
     The higher the inlet assembly pressure drop, the lower the efficiency and power output of the gas turbine. Typical pressure drop values across the gas turbine inlet assembly for power generation varies from about two (2) to about five (5) inches of water column (about five to about 12.7 centimeters of water). This includes the pressure drop across the air conditioning system, which varies from about 0.5 inches to about 1.5 inches of water column (about 1.27 to about 3.8 centimeters of water). Depending on the size of the gas turbine frame, the value of this pressure drop adversely affects the gas turbine output. For example, a gas turbine could lose up to 5% of rated output power from the pressure drop alone if the altitude and temperature remained at ISO conditions. Any change in temperature and/or pressure from ISO rated conditions could increase the rated output power loss. Every point of efficiency and power, however, is essential in the competitive business of power generation or the variety of other uses for mechanical drive gas turbines. 
     Accordingly, Applicant has recognized a need for an air condition system for an operating a gas turbine, for example, in a wide variety of ambient conditions and during changing loads on the gas turbine. Desirably, the system should reduce the inlet assembly pressure drop when not in operation. 
     SUMMARY 
     As referenced above, a gas turbine may be used to supply power in a wide variety of locations and may be operated during any time of the year, sometimes resulting in operation in harsh environments, for example, when used to supply power to a hydraulic fracturing system. In addition, a gas turbine may be subjected to a fluctuating load during operation, for example, when used to supply power to a hydraulic fracturing system. 
     The present disclosure is generally directed to systems and methods for increasing the efficiency of operation of a gas turbine, for example, during operation in a wide variety of ambient conditions and/or under fluctuating loads. In some embodiments, a system for increasing the efficiency of a conventional gas turbine having an inlet assembly and a compressor, the inlet assembly being located upstream of the compressor, may include a housing, an air treatment module, and at least one air conditioning module. As contemplated and discussed above, performance losses may be expected at increased temperatures, increased altitude, and/or increased humidity when using a dual fuel turbine system in a mobile application that is configured to drive a reciprocating hydraulic fracturing pump or drive a generator as part of a gen-set. These environmental conditions may lead to the air being less dense, which may adversely affect turbine system performance as the turbine mass air flow through the air intake axial compression stages are directly proportional to the turbines performance output. The air treatment module may include one or more air conditioning modules that may condition input air to effect a desired increase in the mass flow of air through the air intake axial compression stages of the turbine. 
     According to some embodiments, the housing may be configured to channel an airstream towards the inlet assembly, the housing being positioned upstream of the inlet assembly, which channels the airstream to the compressor. The air treatment module may be positioned at a proximal end of the housing and may include a plurality of inlet air filters and at least one blower in fluid communication with an interior of the housing and configured to pressurize air entering the air treatment module. The at least one conditioning module may be mounted downstream of the air treatment module and may be configured to adjust the temperature of the airstream entering the compressor, such that the airstream enters the air conditioning module at a first temperature and exits the air conditioning module at a second temperature. 
     According to some embodiments, a hydraulic fracturing unit may include a trailer, and a hydraulic fracturing pump to pump fracturing fluid into a wellhead, with the hydraulic fracturing pump connected to the trailer. The hydraulic fracturing unit also may include a gas turbine to drive the hydraulic fracturing pump, and an air treatment system to increase the efficiency of the gas turbine, the gas turbine including an inlet assembly and a compressor. The air treatment system may include a housing positioned to channel an airstream towards the inlet assembly, and an air treatment module positioned at a proximal end of the housing. The air treatment module may include a plurality of inlet air filters to provide fluid flow to a first internal chamber, and one or more blowers mounted in the first internal chamber and providing fluid flow to an interior of the housing via at least one outlet of the first internal chamber, the one or more blowers positioned to pressurize air entering the air treatment module. The air treatment module further may include one or more air conditioning modules mounted downstream of the air treatment module to adjust the temperature of the airstream entering the compressor, such that the airstream enters the one or more air conditioning modules at a first temperature and exits the one or more air conditioning modules at a second temperature. 
     According to some embodiments, a method to enhance the efficiency of a gas turbine including an inlet assembly and a compressor may include causing an airstream to flow toward the inlet assembly and passing the airstream through a plurality of inlet air filters to a first internal chamber. The method also may include operating one or more blowers to pressurize the airstream and provide fluid flow to an interior of a housing via at least one outlet of the first internal chamber. The method further may include causing the airstream to enter one or more air conditioning modules at a first temperature and exit the one or more air conditioning modules at a second temperature. 
     Still other aspects, embodiments, and advantages of these exemplary aspects and embodiments, are discussed in detail below. Moreover, it is to be understood that both the foregoing information and the following detailed description are merely illustrative examples of various aspects and embodiments, and are intended to provide an overview or framework for understanding the nature and character of the claimed aspects and embodiments. Accordingly, these and other objects, along with advantages and features of the present disclosure herein disclosed, will become apparent through reference to the following description and the accompanying drawings. Furthermore, it is to be understood that the features of the various embodiments described herein are not mutually exclusive and may exist in various combinations and permutations. 
    
    
     
       BRIEF DESCRIPTION OF THE DRAWINGS 
       The accompanying drawings, which are included to provide a further understanding of the embodiments of the present disclosure, are incorporated in and constitute a part of this specification, illustrate embodiments of the present disclosure, and together with the detailed description, serve to explain the principles of the embodiments discussed herein. No attempt is made to show structural details of this disclosure in more detail than may be necessary for a fundamental understanding of the exemplary embodiments discussed herein and the various ways in which they may be practiced. According to common practice, the various features of the drawings discussed below are not necessarily drawn to scale. Dimensions of various features and elements in the drawings may be expanded or reduced to more clearly illustrate the embodiments of the disclosure. 
         FIG.  1    is a schematic diagram of an embodiment of an air treatment system for increasing the efficiency of a gas turbine according to an embodiment of the disclosure. 
         FIG.  2    shows an exemplary system setup of the air conditioning system according to an embodiment of the disclosure. 
         FIG.  3    illustrates example performance loss of the gas turbine with increased temperature according to an embodiment of the disclosure. 
         FIG.  4    illustrates, in table form, air properties at different elevations and temperatures according to an embodiment of the disclosure. 
         FIG.  5    is a schematic diagram of an example of an electrical system for operating the air treatment system according to an embodiment of the disclosure. 
         FIG.  6    is a schematic diagram of an example of a hydraulic system for operating the air treatment system according to an embodiment of the disclosure. 
     
    
    
     DETAILED DESCRIPTION 
     Referring now to the drawings in which like numerals indicate like parts throughout the several views, the following description is provided as an enabling teaching of exemplary embodiments, and those skilled in the relevant art will recognize that many changes may be made to the embodiments described. It also will be apparent that some of the desired benefits of the embodiments described may be obtained by selecting some of the features of the embodiments without utilizing other features. Accordingly, those skilled in the art will recognize that many modifications and adaptations to the embodiments described are possible and may even be desirable in certain circumstances, and are a part of the disclosure. Thus, the following description is provided as illustrative of the principles of the embodiments and not in limitation thereof. 
     The phraseology and terminology used herein is for the purpose of description and should not be regarded as limiting. As used herein, the term “plurality” refers to two or more items or components. The terms “comprising,” “including,” “carrying,” “having,” “containing,” and “involving,” whether in the written description or the claims and the like, are open-ended terms, i.e., to mean “including but not limited to.” Thus, the use of such terms is meant to encompass the items listed thereafter, and equivalents thereof, as well as additional items. Only the transitional phrases “consisting of” and “consisting essentially of,” are closed or semi-closed transitional phrases, respectively, with respect to any claims. Use of ordinal terms such as “first,” “second,” “third,” and the like in the claims to modify a claim element does not by itself connote any priority, precedence, or order of one claim element over another or the temporal order in which acts of a method are performed, but are used merely as labels to distinguish one claim element having a certain name from another element having a same name (but for use of the ordinal term) to distinguish claim elements. 
     Referring to  FIGS.  1  and  2   , an example air treatment system  10  is described for operation with a gas turbine  12 . Such a gas turbine may generally include, in serial flow arrangement, an inlet assembly including an inlet  14  for receiving and channeling an ambient airstream, a compressor which receives and compresses that airstream, a combusting system that mixes a fuel and the compressed airstream, ignites the mixture, and allows for the gaseous by-product to flow to a turbine section, which transfers energy from the gaseous by-product to an output power. Other components of the gas turbine may be used therein as will be understood by those skilled in the art. 
     In some embodiments, the air treatment system  10  may be incorporated into a hydraulic fracturing unit. For example, a hydraulic fracturing unit may include a trailer and a hydraulic fracturing pump to pump fracturing fluid into a wellhead, with the hydraulic fracturing pump connected to the trailer. The hydraulic fracturing unit also may include a gas turbine to drive the hydraulic fracturing pump, for example, via a gearbox, and the air treatment system  10 , in some embodiments, may be used to increase the efficiency of the gas turbine. Hydraulic fracturing may be performed generally at any geographic location and during any season of the year, often in harsh environmental conditions. As a result, hydraulic fracturing may occur under a wide variety of ambient temperatures and pressures, depending on the location and time of year. In addition, the load on the hydraulic fracturing pumps and thus the gas turbine engines may change or fluctuate greatly, for example, depending on the build-up and release of pressure in the formation being fractured. In some embodiments, the air treatment system  10  may be configured to increase the efficiency of operation of a gas turbine, for example, during operation in a wide variety of ambient conditions and/or under fluctuating loads. As referenced above, performance losses may be expected at increased temperatures, increased altitude, and/or increased humidity when using a dual fuel turbine system for a mobile hydraulic fracturing unit configured to drive a reciprocating hydraulic fracturing pump via a gearbox or drive a generator as part of a gen-set. These environmental conditions may lead to the air being less dense, which may adversely affect turbine system performance as the turbine mass air flow through the air intake axial compression stages are directly proportional to the turbines performance output. In some embodiments, the air treatment system  10  may include one or more air conditioning modules that may condition input air to effect a desired increase in the mass flow of air through the air intake axial compression stages of the gas turbine, thereby at least partially mitigating or overcoming any performance losses of the gas turbine of a hydraulic fracturing unit due to increased temperatures, increased altitude, and/or increased humidity, while being able to respond to fluctuating loads. 
     In some embodiments, the air treatment system  10  may include a housing  20 , an air treatment module  30 , and/or at least one air conditioning module  50 . Optionally, the air treatment system  10  may further include a filter module  70  positioned intermediate the at least one conditioning module  50  and the input side of the gas turbine. As contemplated and discussed above, performance losses may be expected at increased temperatures, increased altitude, and/or increased humidity, for example, when using a dual fuel turbine system in a mobile application that is configured to drive a reciprocating hydraulic fracturing pump or drive a generator as part of a gen-set. These environmental conditions may lead to the air being less dense. One skilled in the art will appreciate that the relative density of air may be an important factor for a turbine as turbine mass air flow through the air intake axial compression stages may be directly proportional to the turbine&#39;s performance output. The air treatment system  10  described herein may allow for the selective conditioning of air, which may affect a desired increase in air density of air entering the intake of the turbine. As described in more detail below, the air treatment module  30  and/or the at least one air conditioning module  70  of the air treatment system may filter air entering the air treatment system, may boost the pressure of air entering the air treatment system, and may lower the temperature of the air entering the air treatment system air to increase the operating efficiency of the turbine. 
     As illustrated, the example housing  20  may be configured to channel an airstream towards the inlet assembly of the turbine and may be positioned upstream of the input side of the turbine, which channels the airstream to the compressor. The housing  20  may have a shape that is configured for allowing for structural integration with the inlet assembly of the turbine. The integration of the inlet assembly of the turbine and the housing may allow for more controlled flow of the airstream flowing through the air treatment module  30  and the air conditioning module  50  and then flowing to the inlet assembly of the turbine. The housing  20  may be joined to the inlet assembly of the turbine via a plurality of connection means, such as, but are not limited to, welding, bolting, other fastening methods, or combinations thereof. The housing  20  may be formed of or include any material(s) capable of supporting the air treatment module and/or the air conditioning module. Such material(s) may include, for example, but are not limited to, a metal, an alloy, and/or other structural materials as will be understood by those skilled in the art. 
     The air treatment module  30  may include a plurality of inlet air filters or pre-cleaners  32  and at least one blower fan  35  configured to pressurize air. In some embodiments, the air treatment module  30  may be positioned at a proximal end  22  of the housing  20 . The plurality of inlet air filters  32  may be in fluid communication with a first internal chamber  34  of the air treatment module, and the at least one blower fan  35  may be mounted in the first internal chamber  34  to pressurize air entering the first internal chamber  34  via the plurality of inlet air filters. In some embodiments, it is contemplated that plurality of inlet air filters may knock down debris, including mud, snow, rain, leaves, sawdust, chaff, sand, dust, and the like. As shown, the inlet air filters  32  may be configured to continuously or intermittently eject debris before reaching an optional filter module  70  that may be mounted internally within the housing, for example, without the need for further cleaning or shutting-down the unit to replace one or more of the plurality of inlet air filters. 
     As one skilled in the art will appreciate, to compensate for the pressure drop through the plurality of inlet air filters and to boost the pressure and flow of the air to the turbine, the at least one blower fan  35 , which may be operated by an electrical or hydraulic motor, may be installed to bring the overall airflow up to a desired air feed rate, such as, for example and without limitation, about 28,000 CFM, to increase the inlet pressure at the inlet of the turbine with a resultant increase in efficiency of the turbine. Without limitation, in the schematic example shown in  FIG.  1   , at least one blower fan  35  with a coupled electrical motor may be positioned in the first internal chamber  34  of the air treatment module to boost the pressure of intake air to a desired level after the pressure drop through the plurality of inlet air filters and into the downstream filter module  70 . For example, the at least one blower fan  35  may be a squirrel cage blower fan. However, and without limitation, other conventional electrically or hydraulically powered blower fans, such as vane axial fans, and the like, are contemplated. Optionally, the air treatment system  10  may be integrated with a bypass. The bypass may reduce the pressure drop derived from a non-operating air conditioning system. 
     It is contemplated that the at least one blower fan  35  may pressurize the air exiting the air treatment module to a degree sufficient to at least partially overcome the pressure losses associated with passing through the upstream plurality of air filters  32  and through the downstream air conditioning module  50  and, if used, a downstream filter module  70  positioned upstream of the at least one conditioning module, and any other losses the system may encounter, such as rarefication of the inlet air to the blower. In such embodiments, the downstream filter module  70  may be a conventional high-efficiency filter, such as, and without limitation, a conventional vane inlet with a low cartridge- or bag-type pre-filter that would be suitable for periodic cleaning and changing. 
     It is contemplated that the at least one blower fan  35  may be oversized to allow for further pressurization of the air at the downstream inlet of the turbine or engine. Oversizing may allow for suitable compensation for the loss of atmospheric pressure and air density, for example, with increased elevation. The change in pressure due to a change in elevation may be calculated via the following equation: 
             P   =         P   b     [       T   b         T   b     +       L   b     (     H   -     H   b       )         ]           g   0     ⁢   M         R   *     ⁢     L   b                 
where:
 
P=local atmospheric pressure;
 
P b =static pressure at sea level;
 
T b =temperature at sea level;
 
L b =temperature lapse rate;
 
H b =elevation at sea level;
 
H=local elevation;
 
R*=universal gas constant;
 
g 0 =gravity; and
 
M=molar mass of air.
 
     From the calculated pressure, the ideal gas law may be used to calculate a new density of the air at the constant atmospheric pressure.  FIG.  3    shows the change in pressure as a function of increased elevation. It also shows the calculated density in reference to temperature change and elevation change. 
             ρ   =     p       R   sp     ⁢   T             
where:
 
P=absolute pressure;
 
ρ=density;
 
T=absolute temperature; and
 
R SP =specific gas constant.
 
     Referring now to  FIG.  4   , the conventional factor for performance loss of the turbine with increased temperature is a 0.4% to about 0.5% reduction in performance for every one degree Fahrenheit increase over 59 degrees F. For example, it may be seen that at 500 ft, dropping the temperature from 100 degrees F. to 90 degrees F., the HHP output will increase by 140 horsepower, or about 4%. 
     The increase in power results from the temperature decreasing and holding the air pressure constant. The ideal gas law equation may be used to calculate the density of the air as a function of the change in temperature. As may be seen from the table illustrated in  FIG.  4   , a decrease to 90 degrees F. from 100 degrees F. will result in a density increase of 0.0013 lbm/ft 3  or a 1.8% increase. The described relationship is that for every percentage of air density increase the output efficiency increases by approximately 2.2%. 
     Referring to  FIGS.  1  and  2   , the first internal chamber  34  of the air treatment module  30  is in fluid communication with an interior chamber  24  of the housing via at least one outlet  39  of the air treatment module. Optionally, the air treatment module  30  may further include a plurality of drift eliminator and/or coalescer pads suitable for reducing the content of liquids within the airstream flowing through the air treatment module. 
     The at least one air conditioning module  50  for adjusting the temperature of the airstream passing thorough the housing and toward the input side of the gas turbine may be mounted downstream of the air treatment module  30 . The airstream enters the at least one air conditioning module  50  at a first temperature and exits the air conditioning module at a second temperature. The at least one air conditioning module  50  may have a conventional form such as a chiller. One skilled in the art will appreciate that other forms of conventional air conditioning modules are contemplated. The specific form of the at least one air conditioning module may be determined in part from the configuration of the gas turbine. 
     In some embodiments, the at least one conditioning module  50  may include at least one chiller module  55 . The chiller module  55  may include a conventional arrangement of a plurality of condenser coils  56  disposed in the housing and that are configured to span the substantial width of the housing, such that the airstream passes through and/or around the plurality of condenser coils  56  to effect a desired lowering of the temperature of the airstream that is directed downstream toward the input side of the gas turbine. The plurality of condenser coils  56  may be in communication with a source of pressurized chilled refrigerant. The refrigerant may be any conventional refrigerant, such as, without limitation, R22, R410a, and the like as will be understood by those skilled in the art. In one example, the refrigerant fluid may be cooled to about 45 degrees F., but it is contemplated that the desired coolant temperature may be changed to suit varying operating conditions as desired. 
     It is contemplated that the at least one air conditioning module  50  may decrease the temperature of the airstream entering the inlet assembly of the gas turbine to increase the efficiency and power output. In one exemplary aspect, the at least one conditioning module  50  may preferably decrease a temperature of the airstream by between about 2 and 20 degrees F. and optionally between about 5 and 10 degrees F. In some applications, increasing the efficiency and/or the power output of the gas turbine may lead to more efficient operations. For example, in a hydraulic fracturing operation including a plurality of hydraulic fracturing units, each operating a gas turbine to supply power to drive fracturing pumps, such increases in efficiency and/or power output may facilitate reducing the number the gas turbines operating, while still providing sufficient power to meet fracturing fluid pressure and/or flow rate needs to complete the fracturing operation. 
     In various exemplary aspects, it is contemplated that, in elevational cross-sectional view, the plurality of condenser coils  56  of the chiller module  55  may have a planar shape, a W shape, a V shape, or other geometric shape. The chiller module  55  may further comprise a means for chilling the source of pressurized chilled refrigerant. The means for chilling the source of pressurized chilled refrigerant may be a conventional refrigeration cycle using a compressor  58  that is configured to supply pressurized chilled refrigerant to the plurality of coils. The compressor may include a plurality of compressors, which may include one or more of the following types of compressors: a reciprocating compressor, a scroll compressor, a screw compressor, a rotary compressor, a centrifugal compressor, and the like. 
     Optionally, the means for chilling the source of pressurized chilled supply may include at least one chill line carrying pressurized refrigerant that may be routed through and/or around a cold source. It is contemplated that the cold source may include at least one gas source in liquid form. 
     Optionally, the plurality of condenser coils  56  may be placed in an existing radiator package where the lube coolers and engine coolers for the gas turbine are housed. It is also optionally contemplated that the plurality of condenser coils  56  may be packaged along with the compressor and an expansion valve of a conventional refrigeration cycle system. It is contemplated that the heat rejection requirement of the plurality of condenser coils  56  may be higher than the heat rejection of the evaporator because the plurality of condenser coils  56  must also reject the heat load from the coupled compressors. 
     Referring now to  FIGS.  5  and  6   , schematic diagrams of an electrical system and a hydraulic system for operating the air treatment system are presented. It is contemplated that the air conditioning system  10  will not actuate the air treatment module  30  and at least one air conditioning module  50  at a constant speed or power output. For example, during a cold day with low humidity and at low elevation, the air conditioning system may only utilize the plurality of inlet air filters or pre-cleaners  32  and the optional filter module  70 . In some embodiments consistent with this example, the at least one blower fan  35  may be selectively engaged to ensure the pressure drop across the inlet air filters or pre-cleaners  32  are within the turbine manufacturer&#39;s guidelines, but the at least one blower fan  35  will not be run at the respective blower fan&#39;s cubic feet per minute (cfm) rating, nor will the at least one air conditioning module  50  be attempting to reduce the temperature of the air to an unnecessary temperature. As illustrated, the example air treatment module  30  and at least one air conditioning module  50  may be selectively controlled via proportional motor control that may be operatively configured to function through a combination of the use of programmable VFDs, a PLC control system, an instrumentation and hydraulic control system, and the like. 
     In some embodiments, ISO conditions of 59 degrees F., 14.696 pounds per square inch atmospheric pressure, at sea level, and 60% relative humidity may be the baseline operating levels for control of the air conditioning system  10 , as these are the conditions that are used to rate a turbine engine for service. As shown in  FIG.  5   , the assembly and implementation of instruments such as atmospheric pressure sensors and/or temperature sensors allow the air conditioning system  10  to monitor air density through the data inputs and to calculate, at a desired sample rate, the density in reference to temperature change and elevation change. Further, it is contemplated that the pressure drop through the plurality of inlet air filters or pre-cleaners  32  may be monitored via a pair of pressure sensors, which may be positioned at the air intake of the plurality of inlet air filters or pre-cleaners  32  and at the air intake of the turbine also. This noted pressure differential between the pair of pressure sensors may allow the air conditioning system  10  to command the operation of the plurality of blower fans  35  to operate at a desired speed to mitigate or overcome the sensed pressure drop. 
     It is contemplated that in the event there is a loss of one or more control signals from the supervisory control system of the air conditioning system  10 , the chillers and blowers may be configured to automatically revert to operation at maximum output as a failsafe and/or to ensure that operation of the coupled turbine is not ceased. During operation, the pressure transducers and temperature transducers may be configured to provide continuous or intermittent feedback to the supervisory control system. As described, during normal operation according to some embodiments, the supervisory control system may operate to detect the deficiency of the inlet airstream, such as a temperature and/or pressure drop, and may be configured to send control outputs to the blower fan motors and/or the at least one air conditioning module  50 , for example, to condition the airstream to mitigate or overcome the environmental losses. For example, and without limitation, the supervisory control system may include, but is not limited to, PLC, micro-controllers, computer-based controllers, and the like as will be understood by those skilled in the art. 
     Similarly,  FIG.  6    illustrates an example use of hydraulic power to turn hydraulic motors on the blower fans  35  (if hydraulically-powered blower fans  35  are used) and the hydraulically-powered fans on the at least one air conditioning module  50  (if used). In such embodiments, proportional hydraulic control valves may be positioned and may be configured to receive operational input from the supervisory control system for the selective operation of a spool to ensure that the correct amount of hydraulic fluid is delivered into the air conditioning system. 
     This is a continuation of U.S. Non-Provisional application Ser. No. 17/954,118, filed Sep. 27, 2022, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” which is a continuation of U.S. Non-Provisional application Ser. No. 17/403,373, filed Aug. 16, 2021, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” which is a continuation of U.S. Non-Provisional application Ser. No. 17/326,711, filed May 21, 2021, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” now U.S. Pat. No. 11,156,159, issued Oct. 26, 2021, which is a continuation U.S. Non-Provisional application Ser. No. 17/213,802, filed Mar. 26, 2021, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” now U.S. Pat. No. 11,060,455, issued Jul. 13, 2021, which is a continuation of U.S. Non-Provisional application Ser. No. 16/948,289, filed Sep. 11, 2020, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” now U.S. Pat. No. 11,002,189, issued May 11, 2021, which claims priority to and the benefit of U.S. Provisional Application No. 62/704,565, filed May 15, 2020, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM AND ASSOCIATED METHODS,” and U.S. Provisional Application No. 62/900,291, filed Sep. 13, 2019, titled “MOBILE GAS TURBINE INLET AIR CONDITIONING SYSTEM,” the disclosures of which are incorporated herein by reference in their entireties. 
     Although only a few exemplary embodiments have been described in detail herein, those skilled in the art will readily appreciate that many modifications are possible in the exemplary embodiments without materially departing from the novel teachings and advantages of the embodiments of the present disclosure. Accordingly, all such modifications are intended to be included within the scope of the embodiments of the present disclosure as defined in the following claims.