Page 41 - Handbook of Electrical Engineering

20 HANDBOOK OF ELECTRICAL ENGINEERING

Aero-derivative generators are available in single unit form for power outputs from about
8 MW up to about 25 MW. These outputs fall conveniently into the typical power outputs required
in the oil and gas production industry, such as those on offshore platforms.

2.1.2 Light Industrial Gas Turbines

Some manufacturers utilize certain of the advantages of the aero-derivative machines, i.e. high power-
to-weight ratio and easy maintenance. The high power-to-weight ratios are achieved by running
the machines with high combustion and exhaust temperatures and by operating the primary air
compressors at reasonably high compression ratios i.e. above 7. A minimum of metal is used and so
a more frequent maintenance programme is needed. Easier maintenance is achieved by designing the
combustion chambers, the gas generator and compressor turbine section to be easily removable as a
single modular type of unit. The ratings of machines in this category are limited to about 10 MW.

2.1.3 Heavy Industrial Gas Turbines

Heavy industrial gas turbines are usually to be found in refineries, chemical plants and power utilities.
They are chosen mainly because of their long and reliable running times between major maintenance
overhauls. They are also capable of burning most types of liquid and gaseous fuel, even the heavier
crude oils. They also tend to tolerate a higher level of impurities in the fuels. Heavy industrial
machines are unsuitable for offshore applications because:-
• Their poor power-to-weight ratio means that the structures supporting them would need to be much
larger and stronger.
• Maintenance shutdown time is usually much longer and is inconvenient because the machine must
be disassembled into many separate components. A modular concept is not possible in the design
of these heavy industrial machines.
• The thermodynamic performance is usually poorer than that of the light and medium machines.
This is partly due to the need for low compression ratios in the compressor.

They do, however, lend themselves to various methods of heat energy recovery e.g. exhaust
heat exchangers, recuperators on the inlet air.
Figures 2.1 and 2.2 show the relative costs and weights for these types of machines.

2.1.4 Single and Two-shaft Gas Turbines

There are basically two gas turbine driving methods, known as ‘single-shaft’ and ‘two (or twin) shaft’
drives. In a single-shaft gas turbine, all the rotating elements share a common shaft. The common
elements are the air compressor, the compressor turbine and the power turbine. The power turbine
drives the generator.
In some gas turbines, the compressor turbine and the power turbine are an integral component.
This tends to be the case with heavy-duty machines.

The basic arrangement is shown in Figure 2.3.