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124 Gas Turbine Handbook: Principles and Practices<br />

ure 5-3). This power curve is influenced by four distinct factors: inlet<br />

air temperature, turbine inlet temperature (i.e., combustor discharge<br />

temperature), rotor speed(s), and compressor aerodynamics.<br />

Turbine inlet temperature is a limiting factor in all gas turbines,<br />

regardless of design configuration. This limit has been extended<br />

through utilization of internal turbine airfoil cooling. Limitations due<br />

to speed and compressor aerodynamics are distinguished as break<br />

points or slope changes in the power curve. Often, these limitations<br />

are of little consequence since they are small relative to the turbine<br />

inlet temperature limitations. The effects of increasing ambient temperature<br />

on gas turbine output clearly indicate the advantages of<br />

cooling the compressor inlet, especially in hot climates. Lowering the<br />

compressor inlet temperature can be accomplished by the installation<br />

of an evaporative cooler, a fogger system, or a chiller in the inlet ducting.<br />

Evaporative Cooling<br />

The evaporative cooler is a cost-effective way to recover capacity<br />

during periods of high temperature and low or moderate relative<br />

humidity. The biggest gains are realized in hot, low humidity climates.<br />

However, evaporative cooler effectiveness is limited to ambient<br />

temperatures of 50°F (10°C) to 60°F (16°C) and above. Below these<br />

temperatures, parameters other than turbine temperature will limit<br />

gas turbine operation. Also, as the inlet air temperature drops the<br />

potential for ice formation in the wet inlet increases.<br />

Evaporative cooler effectiveness is a measure of how close the<br />

cooler exit temperature approaches the ambient wet bulb temperature.<br />

For most applications coolers having an effectiveness of 80%-<br />

90% provide the most economic benefit. The actual temperature drop<br />

realized is a function of both the equipment design and atmospheric<br />

conditions. The design controls the effectiveness of the cooler, defined<br />

as follows:<br />

cooler effectiveness = (T 1DB<br />

– T 2DB<br />

)/(T 1DB<br />

– T 2WB<br />

) (8-1)<br />

where:<br />

T 1DB<br />

is the dry bulb temperature upstream of the cooler<br />

T 2DB<br />

is the dry bulb temperature downstream of the cooler<br />

T 2WB<br />

is the wet bulb temperature downstream of the cooler.

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