Method of running an air inlet system

Abstract

The present embodiments disclose a method of running an air inlet system upstream of one or more inlet air filters of a device protected by air filtration, wherein the method comprises: regulating the relative air humidity of the inlet air at the one or more inlet air filters in dependence of the inlet air filters differential pressure.

Claims

1. A method of running an air inlet of a device protected by air filtration, wherein the relative air humidity is set by means of a cooling system, wherein the cooling system includes two cooling stages, wherein the first cooling stage of the cooling system comprises a first stage fogging system upstream of one or more inlet air filters that provides inlet air cooling, and wherein the second cooling stage of the cooling system comprises a second stage fogging system downstream of the one or more inlet air filters that provides supplemental cooling to the first stage fogging system, wherein the method comprises: regulating the relative air humidity of the inlet air by the first stage fogging system at the one or more inlet air filters in dependence of the differential pressure of the respective inlet air filter, and regulating supplemental cooling by the second stage fogging system to the wet bulb temperature of the inlet air.

2. The method of claim 1, wherein the relative air humidity of the inlet air by the first stage fogging system is set to between 70% and 90%.

3. The method of claim 2, wherein the relative air humidity of the inlet air by the first stage fogging system is set to about 80%.

4. The method of claim 1, wherein the cooling system includes an evaporative cooling system.

5. The method of claim 4, wherein the evaporative cooling system includes a fogging system.

6. The method of claim 5, wherein the fogging system includes at least one rotary atomiser.

7. The method of claim 1, wherein the second cooling stage regulates the relative air humidity to be about 100%.

8. The method of claim 1, wherein the relative air humidity of the inlet air by the first stage fogging system is set by means of a heating system.

9. The method of claim 8, wherein the heating system provides heat by means of warm air delivered into the inlet air.

10. The method of claim 9, wherein the warm air includes compressor bleed air.

11. The method of claim 9, wherein the warm air includes exhaust air of a turbine enclosure.

12. The method of claim 9, wherein the warm air includes turbine exhaust air.

13. The method of claim 8, wherein the heating system provides heat by means of a heater.

14. The method of claim 1, wherein the device is selected from a group consisting of a gas turbine, diesel engine, process blower, other motive force, general ventilation, or clean room.

15. A system for reducing inlet air temperature of a device protected by air filtration by means of one or more inlet air filters, comprising: a cooling system including two cooling stages, wherein the first cooling stage of the cooling system comprises a first stage fogging system upstream of one or more inlet air filters that provides inlet air cooling, wherein a first control system controls cooling at the one or more inlet air filters in dependence of the inlet air filters differential pressure to achieve a set relative humidity of the inlet air; and wherein the second cooling stage of the cooling system comprises a second stage fogging system downstream of the one or more inlet air filters that provides supplemental cooling to the first stage fogging system, wherein a second control system controls supplemental cooling to the wet bulb temperature of the inlet air.

16. The method of claim 2, wherein the relative air humidity of the inlet air by the first stage fogging system is set to between 75% and 85%.

17. The method of claim 11, wherein the motive device enclosure comprises a turbine enclosure.

18. The method of claim 13, wherein the heater comprises an electrical heater or a burner.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

(1) FIG. 1 is a schematic view of a gas turbine engine with a two-stage fogging system as may be described herein; the system may include a heater 180;

(2) FIG. 2 is a graph showing measurements of downstream relative humidity as a function of modulating valve position, at ambient 70% relative humidity before, during, and after first-stage fogging using the two stage fogging system described herein;

(3) FIG. 3 is a graph showing the relationship between filter differential pressure and relative humidity curve, for a typical in-service filter which would be downstream of the first stage fogging using the two stage fogging system described herein;

(4) FIG. 4 is a graph showing filter differential pressure and relative humidity curves using the two stage fogging system described herein;

(5) FIG. 5 is a graph showing measurements of downstream temperature as a function of modulating valve position, at ambient 14.3 degrees Celsius wet bulb temperature before, during, and after first-stage fogging using the two stage fogging system described herein;

(6) FIG. 6 is a graph showing measurements of the approach to wet bulb temperature as a function of modulating valve position, at ambient 14.3 degrees Celsius wet bulb temperature before, during, and after first-stage fogging using the two stage fogging system described herein;

(7) FIG. 7 is a perspective view of one embodiment of the two stage fogging system described herein for the rotary atomiser and control panel embodiment.

(8) FIG. 8 is a graph showing measurements of inlet air conditions before, during, and after first-stage fogging using the two stage fogging system described herein;

DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

(9) The present invention now will be described more fully hereinafter. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.

(10) As shown in FIG. 1, the inlet air cooling system 100 comprises two stages of fogging. The first stage of the two-stage fogging introduces water, in the form of droplets, into the air stream before the one or more air filters 120. This introduction of water droplets may occur through the use of one or more high capacity rotary atomisers 110. These high capacity rotary atomisers 110 may include an electric motor with a wire cage around the exterior of the motor, such that when the water passes through the wire cage, the wire cage causes the water to break into small particles or droplets. Due to their high capacity nature, the rotary atomisers are capable of providing a greater water flow rate, for example as measured in litres of water per minute, to the air stream as compared to traditional high pressure nozzles. For example, rotary atomisers may provide about 0.5 to about 3.0 litres of water per minute to the air stream at a droplet size of about 40 to about 70 microns, compared to traditional high pressure nozzles used for in-duct fogging where the average capacity is about 0.18 litres per minute. Further, rotary atomisers are capable of accepting a range of water quality without detrimental effect. Therefore, the rotary atomizers do not require demineralized water and may use any available potable water source. These rotary atomisers have variable frequency drives, and are capable of running from 0% to 100% capacity without affecting the size of the droplets.

(11) Alternatively, other fog generating devices may be used for the introduction of water droplets during the first stage of fogging. For example, medium pressure nozzles or air assisted atomisers that operate between about 5 and about 20 bar can be controlled within acceptable constraints of the droplet size, for example 40 to 70 microns. The current state of the art rotary atomisers may not be suitable for use in some environments, such as for example, but is not limited to, explosion proof environments (e.g. refineries). In these types of environments a high capacity nozzle with an explosion-proof pump may be alternatively used to achieve the first-stage cooling.

(12) Rotary atomisers 110, or alternate first stage fog generation devices, are placed upstream of the one or more filters 120. Generally, the rotary atomisers 110 are placed about 1 meter upstream of the filters, which may place them inside of a weather hood or even in the filter house, depending on the dimensions of the particular set-up. The positioning of the atomisers before the filtering media of about 1 meter allows for the water to evaporate before hitting the filter, preventing the filter from becoming saturated with water. However, if the filter utilizes a droplet catcher (such as for example AAF International's AmerDrop system) or a weather louver (such as for example AAF International's AmerVane product) then the placement of the atomiser may be immediately upstream of the filter within the filter house. Additionally, where a filter has a hydrophobic coalescing media (such as for example AAF International's AMERSHIELD and AMERKOOL products), containing glass fibres and oils, the moisture will coalesce to form larger droplets which drain out of the airstream, which may also allow the placement of the atomiser to be immediately upstream of the filter within the filter house. Preferably, the filter contains some device or coating that protects the filter from condensation, droplets, or water hitting the filter, which may cause an increase in differential pressure. More preferably, the filter contains a coalescing part or a weather louver, such that water is prevented from passing through the filter without a decrease in differential pressure. The use of these hydrophobic filters allows for the first-stage fogging system to enact evaporative cooling with negligible risk of water downstream of the one or more filters 120, protecting the compressor's 10 intake.

(13) Unlike conventional high pressure nozzles used downstream of the filter house, the volume and flow rate of water supplied to the first-stage fogger (such as for example a rotary atomizer) may be controlled through a modulating control valve 140, for example a globe valve or a small tank with a variable frequency drive pump attached, without affecting droplet particle size. The first controller or control system 150 receives signals, in the form of, for example, measurements of temperature, relative humidity, and pressure from both one or more sensors 152, 154 located before the filter 120 and one or more sensors 156 after the filter 120. Measurement of the pressure before and after the filter allows for the controller to calculate the differential pressure. Differential pressure is a calculation of the difference between the pressures measured at two points, here, the points are before the filter and after the filter. The first controller 150 utilizes these measurements in order to control the flow rate of water supplied in order to reach a desired relative humidity, with reduced affect to differential pressure. Differential pressure is a calculation of the difference between the pressures measured at two points; here, the two points are before the filter and after the filter. For example in a system where pressure is measure before and after the filter stage water hitting the filter may cause an increase in differential pressure. A closed loop substantially continuously controls or modulates the water flow rate from the relative humidity measurements. Additionally, it is also possible to control the system to regulate downstream temperature and differential pressure. Control of downstream temperature may be desired due to capacity constraints of downstream equipment (for example an alternator) at high ambient temperature. For example, selecting a set point of minimum temperature after cooling of the first control system may avoid problems of capacity constraint in downstream equipment due to high ambient temperature. Further by example, selecting a set point of minimum temperature after cooling of the first control system may avoid problems of icing at the compressor bell mouth. Also, a set point of maximum filter differential pressure of the first control system is selected as a fail-safe mechanism in the event of a sudden increase of differential pressure due to environmental conditions such as an ingress of hygroscopic material onto the filters.

(14) Generally, the first-stage fogging system is controlled through maintaining a set point of relative humidity, determined according to filter differential pressure and relative humidity curves. It has been observed that downstream relative humidity can be controlled precisely by manually or automatically controlling water flow rate. FIG. 2 shows a straight line relationship between relative humidity and valve position. FIG. 2 is an example observation where the ambient relative humidity was 70%, and the downstream relative humidity was adjusted up to 90%. This set relative humidity is calculated through selection of a point from filter differential pressure and relative humidity curves, as shown in FIG. 3 and FIG. 4. The differential pressure and relative humidity curve of FIG. 3 is generated by plotting the relative humidity (x-axis) by the differential pressure (y-axis). The curve shows the relationship of between these two variables, for example the differential pressure may remain constant while relative humidity increases. These curves indicate at what relative humidity measurement, or range of measurements, the differential pressure may increase. This allows for the controller to set the point with a maximum relative humidity as high as possible without affecting differential pressure. FIG. 3 shows the relationship between differential pressure and relative humidity for a mini-pleat filter with hydrophobic media, with data gathered between 4000 and 5000 running hours.

(15) As shown in FIG. 4, the filter differential pressure and relative humidity curves may be different for various types of filters, such as AAF's HydroVee filter 410 or AAF's AstroCel filter 420 or AAF's DuraCel filter 430. However, as generalized in FIGS. 3 and 4 there is an increase in the filter differential pressure as relative humidity reaches about 90%. Therefore, the target relative humidity should be preferably set at about 80% to about 95%. Even more preferably the target relative humidity should be set at about 90%. The first-stage fogging system, which can finely control relative humidity, can be used to control the temperature and relative humidity without causing spikes of differential pressure. To achieve this temperature control, the water flow rate may be finely controlled through small incremental turns of the modulating control valve 140. This fine control of the water flow rate, combined with set maximum relative humidity (as determined by differential pressure relative humidity curves) allows the first controller 150 to finely control the temperature, such that when the water flow rate is increased slightly, the relative humidity increases slightly and thus the temperature also decreases slightly.

(16) FIG. 5 shows a straight line relationship between downstream temperature and valve position for a given set of ambient conditions. This indicates that a set point temperature between ambient temperature and wet bulb temperature can be controlled by adjusting the water flow rate through controller 150. The control system can therefore be set to provide a depressed temperature after cooling, with an automatic maximum relative humidity which avoids deleterious effects on filter differential pressure.

(17) A thermal efficiency measurement indicates the efficiency of evaporative cooling of the first-stage fogging (e.g. rotary atomisers). Thermal efficiency is calculated as follows:

(18) $\mathrm{Thermal}\mathrm{Efficiency}=\frac{\mathrm{ambient}\mathrm{temperature}-\mathrm{measured}\mathrm{temperature}}{\mathrm{ambient}\mathrm{temperature}-\mathrm{wet}\mathrm{bulb}\mathrm{temperature}}$
As the water flow rate increases, the relative humidity increases in proportion, as the thermal efficiency trends with relative humidity. Further, the relationship between thermal efficiency and water flow rate is mostly linear, such that when the water flow rate increases, so does the thermal efficiency. Therefore, in this two-stage cooling system, about 90% of the total cooling achieved by the system may be achieved through the first-stage fogging system (for example through the use of rotary atomisers). The first stage fogging system has been demonstrated to achieve 100% thermal efficiency at high relative humidity. By controlling set point relative humidity to approximately 90%, the first stage fogging is deliberately constrained to approximately 90% efficiency.

(19) An alternate measure of evaporative cooling efficiency, particularly useful in moderate climates, is the approach to wet bulb temperature. FIG. 6 shows first stage fogging system achieving an approach of less than 0.5 degrees Celsius, with a linear relationship between valve position (water flow rate) and approach to wet bulb temperature.

(20) In particular instances it may be preferable to maintain a certain temperature downstream of the filter, in these instances the first control system may limit the flow rate of water in order to achieve a particular downstream temperature based on site requirements at each stage. This allows for fine control in situations where the ambient temperature is high and extra power is desired, but generator output is the constraining variable in a gas turbine power generation set. Additionally, where there is a marked change in the differential pressure, or when differential pressure falls outside of a specified range, the control system 150 may be programmed to set an alarm or alternatively make proactive in-line modifications such as to trim the water flow rate. This alarm or indicator may be any kind of alarm or notification, including visual, audible, or any combination of the two. However, due to dust and particle build up from incoming air in the filter, the differential pressure increases with the age. For example, the differential pressure may increase a few Pascals from when the filter was new as compared to a filter aged to about 12 to about 24 months old. Therefore, a static control utilizing a set differential pressure is not preferable.

(21) In some embodiments the first-stage fogging system may have a source of low pressure water and a modulating control valve 140 to substantially continuously provide variable water quantities. In other embodiments the system may further comprise a water holding tank with automatic level controls and a fixed speed circulating pump.

(22) In some embodiments the first stage fogging system may have a source of low pressure water, a water holding tank with automatic level control, and a low pressure circulating water pump with variable frequency drive in order to substantially continuously provide variable water quantity.

(23) Front-facing or first stage fogging systems may be installed or retrofitted onto existing filter housings. For retrofitting, a frame may be placed inside of the weather hood or inside the filter house to which the first-stage foggers are attached. Alternatively first stage foggers may be supported directly on the same pipe which supplies water to each fogging unit. Sensors that measure the relative humidity, temperature, and pressure may be placed before the one or more filters 703 such as with sensors 152, 154 and after the one or more filters with sensor 156. Sensors may be connected to the control system 150 or in communication therewith. As shown in FIG. 7, where retrofitted, the first stage fogging devices 702 may be supported on the supply pipe 50 inside weather hoods 701 or a filter house 704. One embodiment uses a modulating control valve 707, actuated via the control system 150. Retrofitting allows for the use of existing systems, reduces installation time, and eliminates the need to shut down the gas turbine for installation or for inspection of the front facing foggers. The first-stage fogging system achieves fine control of inlet air relative humidity and temperature, while maintaining downstream filter differential pressure in an acceptable range. Additionally, the fine control of the first-stage fogging system may prevent problems with over-supply of water often seen in state of the art systems.

(24) The second stage of the two-stage fogging introduces water, in the form of droplets, into the air stream after the air filters 120 from one or more plurality of low capacity nozzles 160 to provide supplemental cooling towards the wet bulb temperature. These low capacity nozzles may be high pressure nozzles, or alternatively may be air assisted nozzles. In embodiments utilizing high pressure nozzles, a water tank with automatic level control and a fixed speed circulating pump may be used. In embodiments utilizing air assisted nozzles, a source of air at low pressure, such as an air compressor, and a modulating control valve 140 to substantially continuously provide variable air quantity may be used. Generally, however, these second stage delivery systems provide water at a significantly reduced flow rate as compared to the first stage.

(25) Due to the efficiency of the first-stage fogging, using for example one or more rotary atomisers 110 which achieve about 90% of the total two-stage system cooling, only a small plurality of low capacity nozzles 160 may be used in the second fogging stage to supplement cooling to the wet bulb temperature. The second stage of the cooling may be desired to achieve only about 10% of the total cooling, this reduced cooling load uses a small plurality of nozzles to achieve.

(26) These low capacity nozzles 160 may be controlled through a second controller or control system 170 reduced to a binary (on/off) function. The decision to turn the second stage fogging on or off may be dependent on ambient relative humidity or a plant operator decision regarding whether the air inlet to the drive requires supplemental cooling to the wet bulb temperature from the second-stage system. For example, this binary control system may switch on or off when the temperature, as measured by the sensor 156 after the filter 120, is above a set value. The low capacity nozzles 160, because of their small plurality, may be positioned around the periphery of the duct at the location downstream of one or more filters 120. Positioning the nozzles 160 around the periphery of the duct decreases complexity of the system, which reduces the cost and downtime required for the installation and maintenance of the nozzles. Additionally, the minimization of hardware in the clean air stream decreases the risk of a foreign object (for example metal from a nozzle) falling into the gas turbine engine or system 20.

(27) While several inventive embodiments have been described and illustrated herein, those of ordinary skill in the art will readily envision a variety of other means and/or structures for performing the function and/or obtaining the results and/or one or more of the advantages described herein, and each of such variations and/or modifications is deemed to be within the scope of the invent of embodiments described herein. More generally, those skilled in the art will readily appreciate that all parameters, dimensions, materials, and configurations described herein are meant to be exemplary and that the actual parameters, dimensions, materials, and/or configurations will depend upon the specific application or applications for which the inventive teachings is/are used. Those skilled in the art will recognize, or be able to ascertain using no more than routine experimentation, many equivalents to the specific inventive embodiments described herein. It is, therefore, to be understood that the foregoing embodiments are presented by way of example only and that, within the scope of the appended claims and equivalents thereto, inventive embodiments may be practiced otherwise than as specifically described and claimed. Inventive embodiments of the present disclosure are directed to each individual feature, system, article, material, kit, and/or method described herein. In addition, any combination of two or more such features, systems, articles, materials, kits, and/or methods, if such features, systems, articles, materials, kits, and/or methods are not mutually inconsistent, is included within the inventive scope of the present disclosure. Further, it is to be understood that continuously or substantially continuously may include one or more interruptions, delays, etc. in controlling characteristics such as but not limited to the quantities, rates, measurements disclosed herein and still be within the scope of the embodiments. Alternatively, control or adjustments may be considered or provided intermittently.

(28) All definitions, as defined and used herein, should be understood to control over dictionary definitions, definitions in documents incorporated by reference, and/or ordinary meanings of the defined terms. The indefinite articles a and an, as used herein in the specification and in the claims, unless clearly indicated to the contrary, should be understood to mean at least one. When used in this description and the claims as an adjective rather than a preposition, about means approximately and comprises the stated value and every value within 10% of that value. For example, about 100% would include measurements of 90% and 110%, as well as every value in between. The phrase and/or, as used herein in the specification and in the claims, should be understood to mean either or both of the elements so conjoined, i.e., elements that are conjunctively present in some cases and disjunctively present in other cases.

(29) Multiple elements listed with and/or should be construed in the same fashion, i.e., one or more of the elements so conjoined. Other elements may optionally be present other than the elements specifically identified by the and/or clause, whether related or unrelated to those elements specifically identified. Thus, as a non-limiting example, a reference to A and/or B, when used in conjunction with open-ended language such as comprising can refer, in one embodiment, to A only (optionally including elements other than B); in another embodiment, to B only (optionally including elements other than A); in yet another embodiment, to both A and B (optionally including other elements); etc.

(30) As used herein in the specification and in the claims, or should be understood to have the same meaning as and/or as defined above. For example, when separating items in a list, or or and/or shall be interpreted as being inclusive, i.e., the inclusion of at least one, but also including more than one, of a number or list of elements, and, optionally, additional unlisted items. Only terms clearly indicated to the contrary, such as only one of or exactly one of, or, when used in the claims, consisting of, will refer to the inclusion of exactly one element of a number or list of elements. In general, the term or as used herein shall only be interpreted as indicating exclusive alternatives (i.e. one or the other but not both) when preceded by terms of exclusivity, such as either, one of, only one of, or exactly one of. Consisting essentially of, when used in the claims, shall have its ordinary meaning as used in the field of patent law.

(31) As used herein in the specification and in the claims, the phrase at least one, in reference to a list of one or more elements, should be understood to mean at least one element selected from any one or more of the elements in the list of elements, but not necessarily including at least one of each and every element specifically listed within the list of elements and not excluding any combinations of elements in the list of elements. This definition also allows that elements may optionally be present other than the elements specifically identified within the list of elements to which the phrase at least one refers, whether related or unrelated to those elements specifically identified. Thus, as a non-limiting example, at least one of A and B (or, equivalently, at least one of A or B, or, equivalently at least one of A and/or B) can refer, in one embodiment, to at least one, optionally including more than one, A, with no B present (and optionally including elements other than B); in another embodiment, to at least one, optionally including more than one, B, with no A present (and optionally including elements other than A); in yet another embodiment, to at least one, optionally including more than one, A, and at least one, optionally including more than one, B (and optionally including other elements); etc.

(32) It should also be understood that, unless clearly indicated to the contrary, in any methods claimed herein that include more than one step or act, the order of the steps or acts of the method is not necessarily limited to the order in which the steps or acts of the method are recited.

(33) In the claims, as well as in the specification above, all transitional phrases such as comprising, including, carrying, having, containing, involving, holding, composed of, and the like are to be understood to be open-ended, i.e., to mean including but not limited to. Only the transitional phrases consisting of and consisting essentially of shall be closed or semi-closed transitional phrases, respectively, as set forth in the United States Patent Office Manual of Patent Examining Procedures, Section 2111.03.

(34) The foregoing description of several methods and embodiments have been presented for purposes of illustration. It is not intended to be exhaustive or to limit the precise steps and/or forms disclosed, and obviously many modifications and variations are possible in light of the above teaching. It is intended that the scope and all equivalents be defined by the claims appended hereto.

EXAMPLES

Example 1

(35) An on-plant inlet cooling trial was conducted demonstrating that the first stage fogging, and associated control system, may control temperature and relative humidity by simply adjusting the water flow rate to the first-fogging system (e.g. rotary atomiser). The trial began by first allowing the inlet conditions to stabilize before the rotary atomiser was turned on. After the inlet conditions stabilized the rotary atomiser was started with a water flow rate of 0.5 litres per minute (A of FIG. 8), at this point the temperature immediately begins to drop from about 19.5 C. to about 18.2 C. and the inlet air relative humidity increases from about 76% to about 84%. An additional increase in water flow rate to 0.7 litres per minute (B of FIG. 8) is tested, and following this increase in the water flow rate the temperature continues to decrease to about 17.5 C. and the inlet air relative humidity increases to about 92%. Incremental decreases in the water flow rate to 0.5 litres per minute (C of FIG. 8) then 0.3 litres per minute (D of FIG. 8), and each cause a slight decrease in the temperature, while relative humidity remained constant. These incremental changes in the water flow rate allows for finer control of the temperature and relative humidity. Once the water flow is turned off (E of FIG. 8) the relative humidity and temperature slowly return to ambient inlet air measurements. This data indicates that the first-stage fogging system (e.g. rotary atomisers) produce a nearly immediate reduction in temperature and relative humidity. This on-plant test indicates that a relative humidity of about 97% may be achieved within 10 minutes of the system being started.

Example 2

(36) Pressure measurements were taken both before and after the filter house during the on-plant inlet cooling trial as conducted in example 1 allowing the differential pressure to be calculated. When the water rate was increased from 0.5 litres per minute to 0.7 litres per minute (B of FIG. 8) the differential pressure begins to increase to its peak of 460 Pascals. This maximum is reached and began declining prior to the incremental decrease of the water flow rate to 0.5 litres per minute (C of FIG. 8). The differential pressure continued to decrease until the after the water flow is turned off (E of FIG. 8), where it stabilizes at about 434 Pascals. The differential pressure measurements can be plotted against the relative humidity to generate a curve showing at what relative humidity measurement the differential pressure increases. The differential pressure relative humidity curve for EXAMPLES 1 and 2 is depicted in FIG. 4. The differential pressure remained constant at approximately 430 Pascals while the relative humidity increased, until the relative humidity measured approximately 87%, at which point the differential pressure begins to increase at an exponential rate.

Example 3

(37) In an embodiment of the two-stage cooling system herein, the ambient temperature at the inlet of the air cooling system was measured at about 50 C. Rotary atomisers were used to generate fog in the first stage of fogging. A maximum relative humidity of 90% (as determined by the differential pressure relative humidity curve) cooled the air to about 26 C. (a 24 C. temperature drop from the ambient air temperature). The second-stage fogging utilized a small plurality of low capacity high pressure nozzles, which provided further cooling of the air to about 24 C. (an additional 2 C. decrease in temperature). The air temperature dropped by a total 26 C. through use of the two-stage system, the majority (about 92%), of which occurred in the first fogging stage. Further, due to the cooling capacity of the first-stage fogging, there was no need to provide overspray cooling in the axial compressor at the compressor inlet.

(38) Finally summarizing, the inventions also refers to a system for reducing inlet air temperature of a motive force protected by air filtration, comprising: a high capacity first stage fogging system upstream of one or more inlet air filters that provides a majority of total air cooling, wherein a first control system substantially continuously modulates water flow rate into the first stage fogging system to achieve a set relative humidity to reduce inlet air temperature as compared to ambient temperature; and a low capacity second stage fogging system downstream of the one or more inlet air filters that provides supplemental cooling to the majority of total air cooling of the first stage fogging system, wherein a second control system controls supplemental cooling to wet bulb temperature.

(39) The first stage fogging system preferably achieves about 80% to about 95% of the majority of total air cooling.

(40) The set relative humidity of the first control system is preferably calculated through selection of a point with highest relative humidity on a differential pressure and relative humidity curve prior to an exponential increase in differential pressure on the curve.

(41) A set point of minimum temperature after cooling of the first control system is preferably selected to avoid problems of capacity constraint in downstream equipment due to high ambient temperature.

(42) A set point of minimum temperature after cooling of the first control system is preferably selected to avoid problems of icing at the compressor bell mouth.

(43) A set point of maximum filter differential pressure of the first control system is preferably selected as a fail-safe mechanism in the event of a sudden increase of differential pressure due to environmental conditions such as an ingress of hygroscopic material onto the filters.

(44) The second control system preferably utilizes an on/off switch operated by an operator preference for supplemental cooling to wet bulb temperature.

(45) The high capacity first stage fogging system preferably comprises: a plurality of rotary atomisers with variable frequency drive;

(46) a source of water at low pressure; and a modulating control valve to substantially continuously provide variable water flow rate.

(47) The high capacity first stage fogging system preferably further comprises: a water holding tank with automatic level controls; and a low pressure circulating water pump with variable frequency drive to provide substantially continuously variable water quantity.

(48) The source of air at low pressure preferably is a compressor.

(49) The high capacity first stage fogging system preferably comprises: a plurality of medium pressure nozzles; a source of water at low pressure; a water holding tank with automatic level controls; and a circulating water pump with variable frequency drive to provide substantially continuously variable water quantity.

(50) The low capacity second stage fogging system preferably comprises: a plurality of air assisted atomisers; a source of water at low pressure; a modulating control valve to substantially continuously provide variable water quantity; a source of air at low pressure; and, a modulating control valve to substantially continuously provide variable air quantity.

(51) The low capacity second stage fogging system preferably comprises: a plurality of high pressure nozzles; and a fixed speed circulating water pump.

(52) A two-stage fogging system for reducing the inlet air temperature of a gas turbine comprising: one or more filters; a first stage positioned upstream of the one or more filters and including one or more rotary atomizers that is capable of achieving about 90% of the air cooling towards wet bulb temperature; and a second stage positioned downstream of the one or more filters and including one or more nozzles that is capable of achieving about 10% of the supplemental air cooling towards wet bulb temperature.

(53) Additionally, the inventions also refers to a method of control for a fogging system for reducing the inlet air temperature of a driver, wherein the method comprises: measuring the ambient temperature, ambient relative humidity, and ambient air pressure; introducing water droplets into the air upstream of the filter; measuring the temperature, relative humidity, and air pressure downstream from the filter; calculating a differential pressure value; maintaining a set relative humidity after the filter, wherein the set relative humidity is determined according to differential pressure relative humidity curves; and controlling a water flow rate to achieve set relative humidity, such that increasing the water flow rate increases the relative humidity and decreasing the water flow rate decreases the relative humidity.

(54) The set relative humidity preferably is about 80% to about 95%.

(55) The set relative humidity preferably is about 90%.

(56) Controlling the water flow rate further preferably comprising turning a valve a quarter-turn at a time.

(57) The driver is preferably selected from a group consisting of a gas turbine, diesel engine, process blower, or other motive force.

(58) The set point of relative humidity preferably is calculated by selecting of a point with highest relative humidity on a differential pressure and relative humidity curve prior to an exponential increase in differential pressure on the curve.