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GAS TURBINE DRIVEN GENERATORS      23

           removable coupling shaft between the two turbines. Some points to consider with regard to the two
           types of driver are:-

           a) High speed of rotation tends to improve the compressor and turbine efficiency. Hence, with
              two separate shafts, the best thermodynamic performance from both turbines and the compressor
              is obtainable.
           b) Using aero-derivative machines means that a simple ‘add on’ power turbine can be fitted in the
              exhaust streams of the aero engine. This enables many manufacturers to design a simple power
              turbine and to use a particular aero engine.
           c) Two-shaft machines are often criticised as electrical generators because of their slower response
              to power demands in comparison with the single-shaft machines. This can be a problem when a
              two-shaft machine may have to operate in synchronism with other single-shaft machines or steam
              turbine generators. Sometimes the slower response may affect the power system performance
              during the starting period of large motors. A power system computerised stability study should
              be carried out to investigate these types of problem.

                 Some of the recent aero engines could be called ‘three-shaft’ arrangements because within the
           gas generator there are two compressor turbines and two compressors.


           2.1.5 Fuel for Gas Turbines


           The fuels usually consumed in gas turbines are either in liquid or dry gas forms and, in most cases,
           are hydrocarbons. In special cases non-hydrocarbon fuels may be used, but the machines may then
           need to be specially modified to handle the combustion temperatures and the chemical composition
           of the fuel and its combustion products.
                 Gas turbine internal components such as blades, vanes, combustors, seals and fuel gas valves
           are sensitive to corrosive components present in the fuel or its combustion products such as carbon
           dioxide, sulphur, sodium or alkali contaminants, see also sub-section 2.2.5.

                 The fuel can generally be divided into several classifications:-
           • Low heating value gas.
           • Natural gas.
           • High heating value gas.
           • Distillate oils.
           • Crude oil.
           • Residual oil.


           2.2 ENERGY OBTAINED FROM A GAS TURBINE

           A gas turbine functions as a heat engine using the thermodynamic Joule cycle, as explained in many
           textbooks, see for example References 1 to 5. Most gas turbines used in the oil industry use the
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