Page 346 - 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 6.1.5   Gas turbine configuration





                                          Year   Milestone
                                          1900–30  Various works – expansion
                                                 turbines (Delaval, Parsons, etc.)
                                          1930   Sir Frank Whittle granted gas turbine patent
                                          1943   First successful gas turbine (jet engine)
                                          1950s  Industrial gas generators and
                                                 power turbines used in pipeline service (1st generation)
                                          1960s  Improved efficiency through use of
                                                 material and cooling improvements. Use in power
                                                 generation and industrial plants
                                          1970s     Development of 2nd generation – larger sizes,
                                                    higher efficiency (higher firing temperatures)
                                                    First uses of aero-derivative gas generators and
                                                    power turbine for ‘off shore’ applications
                                                    Increased availability
                                                    Increased preventive maintenance cycle time
                                          1980s     Extensive use of gas turbines in combined
                                                    cycles for co-generation
                                                    Aero-derivative types gain further acceptance
                                                    Continued efficiency increase (higher firing
                                                    temperatures) – retrofits of 1st generation units
                                                    Development of 3rd generation gas turbines
                                                    (use of advanced materials, processing,
                                                    coating and cooling techniques)
                                          1990s     Further acceptance of gas turbine as an
                                                    industrial prime mover
                                                    Simple cycle efficiencies approach 45%. Firing
                                                    temperatures approach 1400°C (2500°F)

                                        Fig 6.1.6   Gas turbines e history of development

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