Gas Turbine Inlet Air Fogging Systems: Application of Psychrometric Principles to Study Cooling and Humidification Processes

Author(s):  
Sanjay Mahapatra ◽  
Jeffrey K. Gilstrap

Gas turbine inlet air-cooling utilizing a high pressure fogging system is theoretically based on the thermodynamic principle of adiabatic saturation. The dry bulb temperature of inlet air decreases by losing its sensible heat to the liquid water droplets generated by the fogging system. This sensible heat is enough to provide the latent heat necessary to evaporate and diffuse these droplets into the surrounding air stream. As a result of this heat interchange accomplished through a complex mechanism of heat transfer and fluid dynamics, the temperature and moisture content of inlet air is decreased & increased respectively resulting in an increase in its density. Neglecting the enthalpy of liquid water, which is insignificant compared to the water’s latent heat of vaporization, the total heat, i.e. enthalpy of the air stream remains unchanged. The net heat exchange outside of this control volume is zero because the droplets, which subsequently diffuse into the air stream, gain the sensible heat lost by inlet air. Therefore, the theoretical concept of adiabatic saturation is valid in this case. However, in real systems, the cooling and humidification process is seldom adiabatic. This paper applies psychrometric principles in conducting a detailed mathematical analysis of various cooling and humidification processes accomplished by fogging systems. The measurement of actual moisture content of air upstream and downstream of a fogging system is vital to gas turbine inlet air-cooling. The moisture content of air and its dry bulb temperature can provide accurate information on the system path and how well it approximates the adiabatic saturation process and determining system efficiency. The deviation from the adiabatic saturation process is attributed to several factors, such as external heat gain or loss, water temperature, etc. The measurement of moisture content can enable the fogging system control logic to control the required water flow rate through the system to obtain maximum performance without over spraying excessive water or under cooling inlet air. This paper presents possible scenarios of deviation from an adiabatic process and methods to determine fogging system total effectiveness.

Author(s):  
Sanjay Mahapatra ◽  
Jeffrey K. Gilstrap

Gas turbine inlet air-cooling using a fogging system is accomplished by using an array of high-pressure nozzles that inject micron-sized droplets in air stream. These droplets evaporate and diffuse in the air stream resulting in cooling and humidification of air. The cooled and moist inlet air increases net turbine power output, improves heat rate and reduces Nitrogen Oxides formation (NOx). The evaporation and mass diffusion of these droplets are influenced, among other factors, by its surface area to volume ratio. Large surface area facilitates drop interfacial heat transfer and smaller volume or weight aids higher droplet residence times. A fogging nozzle’s atomizing performance can be evaluated from its spray properties that include a mean drop size, droplet distribution, numerical droplet density, spray cone angle, and spray penetration. The spray industry adopts various definitions of mean drop size that suits its application and objective. Mean drop sizes or more commonly droplet diameters used in the gas turbine inlet air fogging industry are 90% cumulative volume frequency, Dv0.90 and the Sauter Mean Diameter, D32. Two sprays having identical mean or representative diameter are not necessarily similar in performance. Further, a spray from nozzle ‘A’ having a Dv0.90 less than another nozzle ‘B’ does not necessarily imply that ‘A’ is superior to ‘B’. This paper explains why the use of one or both of the above characteristic diameters does not effectively reflect a fog nozzle’ atomizing performance. This paper also analyzes various characteristic diameters and their relevance to evaporative cooling using fog nozzles. In fogging applications, the smallest and/or the largest sized drops in a spray will have significant impact on performance and neither Dv0.90 nor D32 can independently provide this information. Therefore, at least one other parameter such as the droplet distribution must be known in order to qualitatively define a spray from a fogging nozzle. This paper also determines these parameters such as the Relative Span Factor and Dispersion Boundary Factor and analyzes their importance to fogging performance.


2007 ◽  
Vol 31 (13) ◽  
pp. 1292-1306 ◽  
Author(s):  
Galal M. Zaki ◽  
Rahim K. Jassim ◽  
Majed M. Alhazmy

Author(s):  
John Confurius

The profits that can be gained by use of inlet air cooling on gas turbines has been recognised for quite some time now and the systems installed throughout the world have shown the users in the gas turbine field that cooling indeed can be used to boost power at times when the ambient temperature reaches or exceeds the ISO rating temperature of the gas turbine. Drawback however being that the initial investment asked of the gas turbine user is rather large thus only justifying a cooling system in regions where the outdoor temperatures exceed the ISO rating time and again due to the climate in that region. Lately gas turbine users in colder climates have become interested in power augmentation during their short summer, however there is no justification for an investment like necessary when installing one of the presently available systems on the market. As the question reached us from more and more of our clients it stimulated us to go out and search for a low-investment solution to this problem. This resulted in the world’s first low pressure gas turbine inlet cooling system.


Author(s):  
A Nordin ◽  
D A Salim ◽  
M A Othoman ◽  
S N Omar Kamal ◽  
Danny Tam ◽  
...  

2020 ◽  
pp. 47-52
Author(s):  
Андрій Миколайович Радченко ◽  
Микола Іванович Радченко ◽  
Богдан Сергійович Портной ◽  
Сергій Анатолійович Кантор ◽  
Олександр Ігорович Прядко

The processes of the gas turbine inlet air cooling by exhaust heat conversion chillers, which utilizing the gas turbine exhaust gas heat, converting it into cold were analyzed. The use of two-stage air cooling has been investigated: to a temperature of 15°C – in an absorption lithium-bromide chiller and below to a temperature of 10°C – in an ejector chiller as stages of a two-stage absorption-ejector chiller. To simulate air cooling processes, the program "Guentner Product Calculator", one of the leading manufacturers of heat exchangers "Guentner", was used. The possibility of using the accumulated excess refrigeration capacity of a combined absorption-ejector chiller, which is formed at reduced current heat loads on air coolers at the gas turbine inlet, to cover the refrigeration capacity deficit arising at increased heat loads due to high ambient air temperatures has been investigated. The refrigeration capacity required to the gas turbine inlet air cooling was compared to an excess refrigeration capacity which excess of the current heat load. The considered air cooling system provides pre-cooling of air at the gas turbine inlet by using the excess refrigeration capacity of the absorption-ejector chiller, accumulated in the cold accumulator, to provide the required refrigeration capacity of the air pre-cooling booster stage. The simulation results proved the expediency of the gas turbine inlet air cooling using the accumulated excess refrigeration capacity of the combined absorption-ejector chiller. The proposed solution reduces by about 50% the design refrigeration capacity and, accordingly, the cost of the installed absorption lithium-bromide chiller, which acts as a high-temperature stage for cooling the ambient air at the gas turbine inlet.


Author(s):  
Andrii Radchenko ◽  
Lukasz Bohdal ◽  
Yang Zongming ◽  
Bohdan Portnoi ◽  
Veniamin Tkachenko

2015 ◽  
Vol 80 ◽  
pp. 168-177 ◽  
Author(s):  
Mirko Morini ◽  
Michele Pinelli ◽  
Pier Ruggero Spina ◽  
Anna Vaccari ◽  
Mauro Venturini

2020 ◽  
Author(s):  
A. Radchenko ◽  
N. Radchenko ◽  
A. Tsoy ◽  
B. Portnoi ◽  
S. Kantor

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