Maintenance Practices - GE MS-6001B Maintenance Instructions Manual

Gas turbines with dln-1 combustion systems gas only
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Introduction
The factors having the greatest influence on the life of parts for any given machine are shown in Fig-
ure 1-1.
Fuel
The effect of the type of fuel on parts life is associated with the radiant energy in the combustion
process and the ability to atomize the various liquid fuels. Therefore, natural gas, which does not
require atomization, has the lowest level of radiant energy and will produce the longest life of parts.
Natural gas has been the traditional fuel for use with gas turbines. Due to the need to back up an inter-
ruptible gas supply many gas turbines are dual fuel with a distillate fuel oil used as the alternate fuel.
Contaminants in the fuel also affect maintenance intervals. This is particularly true for liquid fuels
in which dirt results in accelerated replacement of pumps, metering elements, and fuel nozzles. Con-
taminants in fuel gas can erode or corrode control valves and fuel nozzles.
Starting Frequency
Each stop and start of a gas turbine subjects the hot gas path to significant thermal cycles. Control
systems are designed and adjusted to minimize this effect. However, a gas turbine with frequent
starting and stopping requirements will demonstrate parts lives that are shorter than those for a simi-
lar unit in continuous-duty service. See Figure 1-3.
Load Cycle
The load cycle of the gas turbine, up to its continuous rating, will have little effect on parts lives,
provided it does not require frequent and rapid load changes.
Environment
The condition of the inlet air to the gas turbine can have a significant effect on maintenance costs
and intervals if it is either abrasive or corrosive. If abrasives are in the inlet air (e.g., as from sand
storms), careful attention should be paid to inlet filtering in order to minimize this effect.
If the gas turbine is to be operated in a corrosive atmosphere (for example, one with salts), careful
attention should be paid to the location of the inlet air arrangement and the application of correct
materials and protective coatings. It is essential during the planning stages of an application to rec-
ognize any abrasive or corrosive contaminants and to take the necessary steps to minimize them.
Contaminants in the fuel and air are additive.

Maintenance Practices

Parts condition information is based on estimates only, and will vary with machines and specific operat-
ing conditions. However, estimates are based on previous experience and can be very useful in planning
a maintenance program. As actual operating data is accumulated on a specific application, adjustments
of inspection cycles should be the next step in a well-planned program.
Initial inspection planning can be based on the combustion inspection schedule, hot gas path inspection
schedule, and major inspection schedule tailored to your unit and estimated outage requirements listed
in Figure 1-4.
I–2
Inspection and Maintenance

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