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Gas Turbine Handbook : Principles and Practices

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Detectable Problems 195<br />

COMPRESSOR FOULING<br />

Indications And Corrective Action<br />

Compressor fouling normally occurs due to foreign deposits on<br />

the airfoils. In petro-chemical operations, this is the result of the oil<br />

<strong>and</strong> other hydrocarbons in the atmosphere caused by neighboring<br />

process plant flares, etc. In coastal areas, this could be the deposit of<br />

salt in the compressor. In any event, compressor fouling is indicated<br />

by a drop in compressor efficiency, which is more readily seen as a<br />

drop in compressor discharge pressure at a constant speed <strong>and</strong> load.<br />

This will also manifest itself as a reduction in load capacity at a constant<br />

compressor inlet temperature. A compressor efficiency drop of 2<br />

percent is indicative of compressor fouling. This can be calculated as<br />

shown.<br />

η c =<br />

CDP<br />

k–1<br />

k<br />

P in<br />

–1<br />

CDT<br />

T in<br />

–1<br />

(12-4)<br />

For the field engineer or operator, compressor fouling is best<br />

indicated by a 2 percent drop in compressor discharge pressure at<br />

constant speed <strong>and</strong> load. Another indication of fouling is a 3 percent<br />

to 5 percent reduction in load capacity at constant compressor inlet<br />

temperature or ambient air temperature. The 1 psig decrease in compressor<br />

discharge pressure, which will accompany the load reduction<br />

is not easily detectable with field instrumentation.<br />

As shown in Figure 12-7 for the single spool gas turbine, a decrease<br />

in compressor efficiency (at constant load) results in a decrease<br />

in rotor speed, compressor discharge pressure, <strong>and</strong> airflow, <strong>and</strong> a<br />

increase in fuel flow, exhaust gas temperature, <strong>and</strong> compressor discharge<br />

temperature.<br />

Similarly, for the dual spool gas turbine, a decrease in low pressure<br />

compressor efficiency results in decreases in N 1<br />

rotor speed, low<br />

pressure compressor discharge pressure (P 3<br />

), <strong>and</strong> airflow, <strong>and</strong> increases<br />

in fuel flow, exhaust gas temperature (T 7<br />

), N 2<br />

rotor speed, <strong>and</strong><br />

low <strong>and</strong> high pressure compressor discharge temperatures (T 3<br />

<strong>and</strong> T 4<br />

)<br />

as shown in Figure 12-8. The decrease in high pressure compressor<br />

discharge pressure (P 4<br />

) is small <strong>and</strong> not easily detected.

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