Page 343 - Subyek Teknik Mesin - Forsthoffers Best Practice Handbook for Rotating Machinery by William E Forsthoffer
P. 343

Be st Practice 6 .1           Gas Turbine Best Practices


         Best
         Best
         Best Practice 6.1Practice 6.1Practice 6.1
         Always consider aero-derivative gas generator/industrial  have a higher reliability than aero-derivative/industrial
         power turbine (hybrid type) gas turbine units.     power turbine units. There has finally been a realization
           Aero-derivative gas turbines (initially designed for flight and using  by end users that greater MTTR times, longer start-up
         anti-friction bearings) have been thought to have lower MTBFs than  and cool-down times for industrial types outweigh any
         industrial types. End user fleet experience has shown anti-friction  reliability advantages for the industrial e if one actually
         bearing life to exceed 100 months.
                                                            exists.
           The use of an aero-derivative gas generator while using an industrial
         type power turbine (with hydrodynamic bearings) has the following  Benchmarks
         advantages:
                                                            The use of hybrid (aero-derivative/industrial) gas turbines, for me-
           Shorter start-up and shut down time
                                                            chanical dive and generator applications above 15 MW site power
           Equal or greater bearing MTBF than industrial type gas turbines
                                                            rating, has been recommended in project design phases since 1990.
           Module replacement of the gas generator (as low as 36 hours
           guaranteed) without the necessity for gas generator to power
           turbine alignment
         Lessons Learned
         Industrial gas turbines are used for mechanical drive
         applications based, on the pre-conceived idea that they




       B.P. 6.1. Supporting Material                        that a steam turbine is an external combustion engine, whereas
                                                            a gas turbine is an internal combustion engine. That is, the
       In this section, we will discuss functions and types of gas tur-  motive fluid for a steam turbine is generated external (in the
       bines. In my personal experience, the gas turbine is the most  boiler) to the engine. In the case of a gas turbine, the motive
       misunderstood rotating equipment item. Because of its many  fluid is generated internal to the engine (air compressor and
       support systems and various configurations, the gas turbine is  combustor).
       often approached with mystery and confusion. In order to  Figure 6.1.2 compares the gas and steam turbine cycles; the
       thoroughly explain the gas turbine from a functional standpoint,  latter is known as the ‘Rankine cycle’. As shown, the hot vapor is
       we will build on prior knowledge. We will also compare the gas  generated in the boiler, which is external to the steam turbine
       turbine to an automotive engine in terms of its combustion  (expander).
       cycle. Having done this, we will then use a building block ap-  The gas turbine cycle is known as the ‘Brayton cycle’. Here, air
       proach to explain the total configuration of a gas turbine and  is brought into the engine by the axial compressor, and combined
       conclude with a brief history of its evolution.      with fuel and an ignition source in the combustor to produce a hot
          Gas  turbine  classifications  will  then  be  presented,  vapor, which then is expanded through the HP (high pressure)
       specifically:                                         turbine. The combination of the compressor, combustor and HP
                                                            turbine is commonly known as the gas generator. This is because
       - Design type                                        its function is to generate or produce a hot vapor from the
       - Number of shafts                                   combination of an air and fuel mixture. Essentially, a gas
       - Drive and number of shafts                         generator can be considered to have the same function as
       - Cycle                                              aboiler e both produce a hot vapor. One can think of the gas
       - Drive and location                                 generator as a ‘rotating boiler’. After the hot vapor is generated, it
          We will discuss the major design differences between aero-  then is expanded additionally in the power turbine. The power
       derivative and hybrid (aero-derivative gas generator/industrial  turbine, therefore, serves exactly the same function as the steam
       power) turbines. Single and multiple shaft gas turbines will be  turbine. That is, both components are hot gas expanders.
       discussed and reviewed. The three major application cycles for
       gas turbines: simple, regenerative, and combined will be
       presented and discussed.                             Comparison to an automotive engine
          Finally, we will present applications of different gas turbine
       types, and provide information concerning where the different  Figure 6.1.3 shows the similarities between an automotive
       types are used.                                      engine and a gas turbine. If one considers a gas turbine as only
                                                            a dynamic internal combustion engine, understanding it be-
                                                            comes significantly easier. As shown in the figure, an automotive
       Comparison to a steam turbine                        engine is a positive displacement internal combustion engine,
                                                            having an intake, compression, combustion and exhaust stroke.
       Figure 6.1.1 shows a typical condensing steam turbine and an  A gas turbine engine is a dynamic internal combustion engine.
       industrial gas turbine. The major difference between the two is  The process in this case is continuous e and not intermittent as

           314
   338   339   340   341   342   343   344   345   346   347   348