Page 9 - Uninterruptible Power Supplies
P. 9

Standby Power Generating Sets
                                                Standby Power Generating Sets  7


            Standard Reference Conditions for Diesel Engines
            The standard conditions for diesel engines are specified in ISO 8528-1
            and ISO 3046-1 as:
              Total barometric pressure       100 kPa (1 bar)
              Air temperature                   25°C
              Charge air coolant temperature    25°C
              Relative humidity                 30 percent

              The barometric pressure of 100 kPa is equivalent to an altitude of
            150 meters above sea level. The altitude at which an engine is working
            has an important effect on the engine’s performance. At high altitudes
            a smaller mass of aspiration air is drawn into each cylinder, less fuel
            can be burnt and less power is produced.
              The ambient air temperature of 25°C imposes some limitation of out-
            put in temperate and warm climates. It is usual to allow a 10°C rise in
            the engine room ventilating air and if the outside ambient exceeds
            15°C the temperature within the engine room is likely to exceed 25°C
            and some degree of derating will be necessary. The engine manufac-
            turer should be made aware of the maximum operating temperature
            expected and of its duration.

            Gas Turbines
            Gas turbines are currently available from about 500 kW upwards; at
            the time of going to press units as small as 50 kW were being consid-
            ered for combined heat and power purposes so there may be a future
            downward trend in the size of gas turbines for standby power applica-
            tions. The turbine shaft will run at tens of thousands of rpm and a gear
            box is interposed between the turbine and the generator, which will run
            at 1500 or 3000 rpm for 50-Hz supplies.
              There are two types of gas turbine, the single-shaft machine and the
            two-shaft machine. The single-shaft machine has the turbine and the com-
            pressor on a single shaft, and is used for standby generation applications.
            The turbine and the compressor run at constant speed and the mass flow
            of air through the machine is constant. There is always adequate combus-
            tion air and any increase of fuel leads to an immediate increase of power;
            full load can be accepted in a single step.
              The two-shaft machine is of higher efficiency but is not used often for
            standby generation purposes because it has a poor step load acceptance.
            The turbine and the compressor are on separate shafts, the compressor
            being driven by the turbine exhaust gas flow. The speed of the compres-
            sor and mass flow of air through it is variable; any increase of load



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