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Gas Turbine Handbook : Principles and Practices

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Case Study #1 245<br />

with the DCS.<br />

The natural gas/doped propane fuel system is st<strong>and</strong>ard apart<br />

from a customer signal which indicates which fuel is in use. Logic<br />

within the control system makes the necessary specific gravity adjustment<br />

for fuel flow measurement.<br />

A new, patented syngas control system is being provided for the<br />

Sierra Pacific IGCC application. It provides an integrated control<br />

system for the syngas boost compressor <strong>and</strong> the gas turbine that will<br />

minimize fuel supply delivery pressure losses. The boost compressor<br />

raises the compressor extraction pressure prior to the gasifier. After<br />

the gasifier, fuel is metered to the gas turbine through the stop ratio<br />

<strong>and</strong> gas control valves. Pressure drops through these valves are minimized<br />

by controlling them to the full open position during normal control<br />

operation. By this method the system operates at the minimum<br />

pressure drop <strong>and</strong> controls the gasifier flow via the boost compressor,<br />

thereby controlling the gas turbine output. When the fuel flow is not<br />

meeting dem<strong>and</strong>, a signal is sent to the gasification isl<strong>and</strong> control<br />

panel, which translates this input to the necessary response from the<br />

Figure 14-7. View of MS6001FA Combustor Case Extraction Manifold.

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