Page 114 - Steam Turbines Design, Applications, and Rerating
P. 114

Chapter
                                                                    5








                      Rotors for Reaction Turbines













            During the first two decades of this century, experienced manufactur-
            ers used solid forged rotors for small turbines. For larger units they
            preferred built-up rotors, consisting of a number of disks shrunk on to
            a central shaft. For small machines the solid forged rotor is still stan-
            dard, but for the large machines the shrunk disk design was subse-
            quently discarded because of its higher stress levels. Articles from a
            number of independent sources deal with the stress levels and quality
            of this type of rotor.


            5.1 Solid Rotors
            Solid rotors can be defined as those forged from a single piece
            (monoblock). Figure 5.1 shows a solid rotor forging being produced in a
            steel plant. Only after extensive testing, which is described later, is the
            rotor accepted for further machining. Figure 5.2 shows a solid rotor
            being machined in a lathe.
              The bladed rotor of an 11.5-MW turbine is shown in Fig. 5.3, while
            Fig. 5.4 shows a section through a 15-MW mechanical drive turbine
            rotor.
              The choice of whether a solid rotor can be used is dependent on the
            start-up procedure. The temperature and stress conditions arising
            because of the admission of hot steam onto the cold rotor must be
            exactly known and controlled. This is because the thermal stresses due
            to the temperature difference between the surface and the center line
            of the rotor determine whether it can be manufactured as a solid rotor.
              The factors responsible for the stress levels in the rotor are basically
            the steam temperature, the geometry (diameter) of the rotor and, in
            particular, the time available to reach the full-load condition. The exact
            relationship between these criteria has been established following
                                                                           95
   109   110   111   112   113   114   115   116   117   118   119