Page 58 - Handbook of Electrical Engineering

GAS TURBINE DRIVEN GENERATORS 37

Therefore it is a simple matter to predetermine the required output power and divide this by
the specific energy available to the generator. The result is then the mass flow rate.

2.3.1 Mechanical and Electrical Power Losses

The power and specific energy available to drive the generator determined in the previous sub-section are
those at the output shaft of the gas turbine. In most situations in the oil industry, where these machines
seldomareratedabove40 MW,aspeed-reducinggearboxisplacedbetweentheturbineandthegenerator.
The generators are usually 4-pole machines that operate at 1500 or 1800 rev/min. The power loss in a
typical gearbox is about 1.5% of the rated output power. Let the gearbox efficiency be η gb .
The efficiency (η gen ) of electromechanical conversion in the generator can be defined as,

Power output at the terminals
η gen = pu
Power input to the shaft coupling
Most rotating electrical machines above about 500 kW have efficiencies above 95%, which
increases to about 98% for large machines in the hundreds of megawatts range. Their losses are
due to windage between the rotor and the stator, friction in the bearings and seals, iron and copper
electrical losses.
In some situations, such as ‘packaged’ gas turbine generators, all the necessary auxiliary
electrical power consumers are supplied from the terminals of the generator through a transformer
and a small motor control centre (or switchboard). These auxiliaries include lubricating oil pumps,
fuel pumps, filter drive motors, cooling fans, purging air fans, local lighting, and sump heaters. Some
of these operate continuously while others are intermittent. A rule-of-thumb estimate of the consumed
power of these auxiliaries is between 1% and 5% of the rated power of the generator.
Care needs to be taken when referring to the efficiency of a gas-turbine generator set. See
the worked example in Appendix F. The power system engineer is concerned with the power output
from the terminals of the generator that is obtainable from the fuel consumed. Hence he considers
the practical efficiency η pa of the gas turbine, and the conversion efficiency through the gearbox η gb
and generator η gen . Hence the Overall Thermal Efficiency η pao would be:-

η pao = η pa × η g × η gen

2.3.2 Factors to be Considered at the Design Stage of a Power Plant

The electrical engineer should take full account of the site location and environmental conditions that
a gas turbine generator will need to endure. These conditions can seriously effect the electrical power
output that will be achievable from the machine. The starting point when considering the possible
output is the ISO rating. This is the declared rating of the machine for the following conditions:-

• Sea level elevation.
◦
◦
• 15 C(59 F) ambient temperature.
• Basicengine,nolossesforinletorexhaustsystems,nolossesforgearboxandmechanicaltransmission.
• Clean engine, as delivered from the factory.
The gas turbine manufacturer provides a standardised mechanical output power versus ambient
temperature characteristic, e.g., Figure 2.10. (Some manufacturers also give the electrical output