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Hardware 23<br />

Chapter 3<br />

Hardware<br />

Aero-derivative and industrial gas turbines have demonstrated<br />

their suitability for heavy duty, continuous, base load operation<br />

in power generation, pump and compressor applications.<br />

While they share many similarities, there are times when<br />

their differences make them uniquely more suitable for a specific<br />

application. These differences are not always adequately considered<br />

during the equipment selection phase. As a result operations and<br />

maintenance personnel must deal with them throughout the plants<br />

useful life. As shown in the previous chapter, schematically there are<br />

little differences between the various types of gas turbines. However,<br />

considering the actual hardware, primarily in the 20,000-horsepower<br />

and above range, the differences are very significant.<br />

SIMILARITIES AND DIFFERENCES 1<br />

In spite of their common background, there are variations between<br />

the aero-derivative and heavy industrial gas turbines. These<br />

are weight, combustor design, turbine design, and bearing design<br />

(including the lube-oil system). Grouping units in the same or similar<br />

horsepower output range, the most obvious difference is in the physical<br />

size of the heavy industrial compared to the aero-derivative gas<br />

turbines (Figure 3-1 and 3-2). This physical size difference leads to<br />

the comparisons in the following table.<br />

The differences between the aero-derivatives and the hybrid industrial<br />

gas turbines are less significant (Figure 3-3). Size, rotating<br />

speed, air flow, and maintenance requirements are similar for both<br />

type machines. The primary distinction is in the bearing selection<br />

where the hybrids use hydrodynamic bearings (similar to the heavy<br />

23

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