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Gas Turbine Handbook : Principles and Practices

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Hardware 43<br />

heavy-industrial unit requires an elaborate emergency lube system to<br />

protect the bearings through this long shutdown period. Furthermore,<br />

cool-down time approaches 48 hours during which time the unit must<br />

be slow-rolled to achieve uniform shaft cooling <strong>and</strong> to avoid bowing of<br />

the shaft. Shaft bowing is extremely critical on these heavy industrial<br />

machines. It is not practical to “motor” the heavy machines at cranking<br />

speeds (in an attempt to shorten the cool-down time) because the<br />

starting motors are not designed for prolonged running.<br />

The aero-derivative units can be started with 50-150 horsepower<br />

starting motors. All the aero-derivative gas generators can be factory<br />

tested to maximum turbine inlet temperature <strong>and</strong> maximum gas<br />

horsepower using an exhaust “jet” nozzle, if necessary. Some manufacturers<br />

have the capability of testing to maximum shaft horsepower.<br />

In very few instances are the heavy industrial units tested<br />

to either maximum temperature or maximum horsepower. At most,<br />

manufacturers provide testing to rated speed only.<br />

American Petroleum Institute (API) St<strong>and</strong>ard 616 was written<br />

<strong>and</strong> published specifically for the heavy industrial gas turbine, although<br />

it is also used for the aero-derivative industrial turbine.<br />

References<br />

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

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

2. “The Crystallography of Cast <strong>Turbine</strong> Airfoils,” by D.H. Maxwell <strong>and</strong> T.A.

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