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Gas Turbine Handbook : Principles and Practices

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Detectable Problems 203<br />

Running<br />

Running problems associated with fuel controls consist of the<br />

inability to accelerate (or increase load), or accelerate too rapidly.<br />

There are also numerous running problems (such as miscellaneous<br />

trips, aborts, etc.) that are specific to the type of control method<br />

employed. Pneumatic <strong>and</strong> hydraulic controls are very susceptible to<br />

leaks <strong>and</strong> contamination. In addition pneumatic controls are sensitive<br />

to moisture in the lines, that can result in erratic operation. This often<br />

leads to erratic or otherwise unstable operation. Mechanical <strong>and</strong><br />

electric controls are subject to wear <strong>and</strong> leaks in bellows <strong>and</strong> capillary<br />

sensors. In addition, accuracy deteriorates over a period of time.<br />

Computer or electronic controls are generally the most problem free,<br />

once the unit has been commissioned <strong>and</strong> all the programming logic<br />

fully <strong>and</strong> completely implemented.<br />

Acceleration problems, either a lack or too much of, usually<br />

result from governor malfunctions (although the malfunctions may<br />

not be specifically with the governor mechanism). These malfunctions<br />

may result from faulty governor input signals such as speed,<br />

compressor discharge pressure, temperature, or fuel flow. Overspeed<br />

could be the result of a governor malfunction, electrical upsets (generator<br />

drives), or coupling failure. Overspeed is detrimental not only<br />

to the gas turbine but also to the driven load. Redundant systems<br />

(usually two electrical <strong>and</strong> one mechanical) are installed to protect<br />

against overspeed. The electrical systems should be checked periodically<br />

(simulation test) <strong>and</strong> the mechanical fly-bolt should be cleaned.<br />

It is not possible to check the operation of the mechanical fly-bolt<br />

mechanism in the field.<br />

References<br />

1. “<strong>Gas</strong> <strong>Turbine</strong> Parameter Interrelationships,” Louis A. Urban, 1969.<br />

2. American Society of Mechanical Engineers Power Test Code 22, 1974.<br />

3. Sawyer’s Turbomachinery Maintenance <strong>H<strong>and</strong>book</strong>, First Edition, Vol 1, p<br />

12-25.<br />

4. “How Lightweight And Heavy <strong>Gas</strong> <strong>Turbine</strong>s Compare,” Anthony J. Giampaolo,<br />

Oil & <strong>Gas</strong> Journal, January 1980.

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