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Gas Turbine Handbook : Principles and Practices

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<strong>Gas</strong> <strong>Turbine</strong> Control 75<br />

Figure 5-3. Shaft horsepower vs. inlet temperature.<br />

Controls for a typical gas turbine generator or mechanical drive<br />

application in the early 1970s were electric controls <strong>and</strong> consisted<br />

of Station Control, a Process Control, <strong>and</strong> a <strong>Turbine</strong> Control 2 . In<br />

this type of control system all control functions ( Start, Stop, Load,<br />

Unload, Speed, <strong>and</strong> Temperature) were generated, biased, <strong>and</strong> computed<br />

electrically. Output amplifiers were used to drive servo valves,<br />

employing high pressure hydraulics, to operate hydraulic actuators.<br />

These actuators were sometimes fitted with position sensors to provide<br />

electronic feedback.<br />

The advent of programmable logic controllers <strong>and</strong> microprocessors<br />

(Figure 5-5) in the late 1970s eliminated these independent control<br />

loops, <strong>and</strong> facilitated multi-function control. Regardless of type,<br />

all controls must accomplish the same basic functions.

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