Page 24 - Steam Turbines Design, Applications, and Rerating
P. 24

Introduction  5

              Since there is theoretically no pressure drop across the moving
            blades (and thus no reaction), internal clearances are large, and no bal-
            ance piston is needed. These features make the impulse turbine a
            rugged and durable machine that can withstand the heavy-duty ser-
            vice of today’s mechanical drive applications.


            1.2.1 Steam turbine staging can vary
            First, let’s consider velocity-compounded (Curtis) staging. A Curtis
            stage consists of two rows of moving blades. Stationary nozzles direct
            the steam against the first row; reversing blades (not nozzles) then
            redirect it to the second row.
              The large pressure drop through the nozzle produces a high-speed
            steam jet. This high velocity is absorbed in a series of constant pressure
            steps (see Fig. 1.4). The two rotating rows of blades make effective use
            of the high-speed jet, resulting in small wheel diameters and tip speeds,
            fewer stages, and a shorter, more rugged turbine for a given rating.
              In pressure-compounded (Rateau) staging, the heat energy of the
            steam is converted into work by stationary nozzles (diaphragms) direct-
            ing the steam against a single row of moving blades.As in a Curtis stage,
            pressure drops occur almost entirely across the stationary nozzles.


            1.2.2 Modern impulse design
            The importance of steam turbine efficiency has continued to increase
            over the last decade. Today, there is no pure impulse turbine. Manufac-
            turers are using a combination of reaction and impulse design features
            to further improve turbine efficiency. The traditional impulse turbine
            manufacturers, who utilize the basic wheel-and-diaphragm construc-
            tion, have been able to meet, and many times exceed, the performance
            of a pure reaction turbine. This is done on high-pressure stages by
            adding a small amount of reaction to improve the performance, without
            the need for tight leakage controls or increasing thrust forces. Tall, low-
            pressure buckets are designed with more reaction than ever before
            using advanced aerodynamic codes for these complex blade forms.
            The generous clearances of the wheel-and-diaphragm construction
            decrease the dependence on tight leakage control. Field data have
            shown that these modern impulse turbines will sustain their high level
            of performance over time and are much more tolerant to fouling, which
            can have a significant impact on thrust loads.


            1.2.3 Single-valve vs. multivalve
            construction
            Single-valve units (Fig. 1.5) are available when justified by plant eco-
            nomics. When used, individual nozzle ring segments are controlled by
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