Page 348 - Subyek Teknik Mesin - Forsthoffers Best Practice Handbook for Rotating Machinery by William E Forsthoffer
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Gas Turbine Best Practices   Be st Practice 6.1





























                                        Fig 6.1.10   Mars gas turbine (Courtesy of Solar Turbines)























              Fig 6.1.11   Gas turbine classifications (aero-derivative). Left: used as gas generator only (Courtesy of Dresser Rand). Right: entire engine adapted
              (gas generator and power turbine). Note: power turbine is either turbo-prop or bypasss fan drive in aero-engine version (Courtesy of General Electric).




              Figure 6.1.13. This produces 45 MW (60,000 ISO horsepower),  Figure 6.1.18. Most modern gas turbines are of the triple shaft
              has an efficiency of 43% and can drive a load on either or both  design. Figure 6.1.19 shows a single shaft gas turbine where the
              ends.                                                gas generator and power turbine are mounted on the same shaft.
                The advantages and disadvantages of aero-derivative gas tur-  This figure also shows a dual shaft gas turbine, where the gas
              bines are presented in Figure 6.1.14.                generator and power turbine are mounted on different shafts.
                Figure 6.1.15 shows a hybrid type gas turbine, which is  Single shaft gas turbines are usually limited to generator drive
              a combination of an aero-derivative gas generator and an in-  applications, since the starting turbine load is significantly lower
              dustrial power turbine. This design offers the advantage of  for a generator application, because a generator is started under
              maintainability on the ‘hot section’ of the gas turbine and high  zero load. Dual shaft turbines are used for mechanical drive,
              reliability in the power turbine. These facts are presented in  pump and compressor applications.
              Figure 6.1.16.
                Aero-derivative and industrial facts are discussed in  Gas turbine drive configurations
              Figure 6.1.17.
                                                                   Gas turbines can be designed as hot end drive, or cold end drive.
                                                                   Figure 6.1.20 presents these facts. The majority of first and
              The number of gas turbine shafts                     second generation gas turbines were of a hot end drive, but most
              Gas turbines are configured as single, dual or triple shaft designs.  third generation gas turbines are of the cold and dry type. A cold
              The advantages and disadvantages of each type are presented in  end drive configuration is more reliable, in my opinion, since the

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