The Theory of Heat Engines
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The velocity diagram for one stage is shown in Fig. 98. Using the same notation as before, 6 and denote the angles of the moving blades at entrance and exit respectively, whilst and y denote the corresponding angles for the fixed blades. Fig. 98 has been drawn on the assumption that the relative velocity of the steam at entrance and exit of each ring of blades is the same, i. E. R = R (see Art. 112), and also that the velocity of the tips of all the moving blades is equal, i. E.
cb = de = gf= ...hk = ml If the absolute velocity of the steam entering the first set of moving blades be denoted by V, and the absolute velocity on leaving the last sef ART. 115] THEORY OF THE STEAM TURBINE 197 of moving blades' by v, then, as in Art. 112, the efficiency of the stage will be (neglecting losses) V2 Moving Fixed Moving Fixed Moving n o FIG. 98. Velocity diagram for one stage of Curtis turbine.
115. Multi-Stage Reaction Turbines The Parsons Tur- bine. 1 Although commonly called a reaction turbine, this turbine works partly by impulse and partly by reaction.
What to read after The Theory of Heat Engines?
You can find similar books in the "Read Also" column, or choose other free books by William Inchley to read onlineMoreLess
To quickly assess the difficulty of the text, read a short excerpt:
The velocity diagram for one stage is shown in Fig. 98. Using the same notation as before, 6 and
cb = de = gf=
115. Multi-Stage Reaction Turbines The Parsons Tur- bine. 1 Although commonly called a reaction turbine, this turbine works partly by impulse and partly by reaction.
What to read after The Theory of Heat Engines?
You can find similar books in the "Read Also" column, or choose other free books by William Inchley to read onlineMoreLess
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