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Page | 011 shown in Figure 7, influences such as fuel type and quality, firing temperature setting, and the amount of steam or water injection are considered with regard to the hours-based criteria. Startup rate and the number of trips are considered with regard to the starts- based criteria. In both cases, these influences may reduce the maintenance intervals. Typical baseline inspection intervals (6B.03/7E.03): Hot gas path inspection 24,000 hrs or 1200 starts Major inspection 48,000 hrs or 2400 starts Criterion is hours or starts (whichever occurs first) Factors affecting maintenance: Hours-Based Factors • • Fuel type Peak load • Diluent (water or steam injection) Starts-Based Factors • • • Start type (conventional or peaking-fast) Start load (max. load achieved during start cycle, e.g. part, base, or peak load) Shutdown type (normal cooldown, rapid cooldown, or trip) Figure 7. Maintenance factors When these service or maintenance factors are involved in a unit’s operating profile, the hot gas path maintenance “rectangle” that describes the specific maintenance criteria for this operation is reduced from the ideal case, as illustrated in Figure 8. The following discussion will take a closer look at the key operating factors and how they can affect maintenance intervals as well as parts refurbishment/replacement intervals. Maintenance Factors Reduce Maintenance Interval 1,400 1,200 1,000 Starts 800 600 400 200 Hours-Based Factors • Fuel type • Peak load • Diluent 0 0 20 24 28 4 8 12 16 Thousands of Fired Hours Figure 8. GE maintenance intervals Starts-Based Factors • Start type • Start load • Shutdown type Fuel Fuels burned in gas turbines range from clean natural gas to residual oils and affect maintenance, as illustrated in Figure 9. Although Figure 9 provides the basic relationship between fuel severity factor and hydrogen content of the fuel, there are other fuel constituents that should be considered. Selection of fuel severity factor typically requires a comprehensive understanding of fuel constituents and how they affect system maintenance. The selected fuel severity factor should also be adjusted based on inspection results and operating experience. Heavier hydrocarbon fuels have a maintenance factor ranging from three to four for residual fuels and two to three for crude oil fuels. This maintenance factor is adjusted based on the water-to-fuel ratio in cases when water injection for NOx abatement is used. These fuels generally release a higher amount of radiant thermal energy, which results in a subsequent reduction in combustion hardware life, and frequently contain corrosive elements such as sodium, potassium, vanadium, and lead that can cause accelerated hot corrosion of turbine nozzles and buckets. In addition, some elements in these fuels can cause deposits either directly or through compounds formed with inhibitors that are used to prevent corrosion. These deposits affect performance and can require more frequent maintenance. Distillates, as refined, do not generally contain high levels of these corrosive elements, but harmful contaminants can be present in these fuels when delivered to the site. Two common ways of contaminating number two distillate fuel oil are: salt-water ballast mixing with the cargo during sea transport, and contamination of the distillate fuel when transported to site in tankers, tank trucks, or pipelines that were previously used to transport contaminated fuel, chemicals, or leaded gasoline. GE’s experience with distillate fuels indicates that the hot gas path maintenance factor can range from as low as one (equivalent to natural gas) to as high as three. Unless operating experience suggests otherwise, it is recommended that a hot gas path maintenance factor of 1.5 be used for operation on distillate oil. Note also that contaminants in liquid fuels can affect the life of gas turbine auxiliary components such as fuel pumps and flow dividers. Not shown in Figure 9 are alternative fuels such as industrial process gas, syngas, and bio-fuel. A wide variety of alternative fuels exist, each with their own considerations for combustion in GE Power | GER-3620P (2/21) 7 |