The Constant-pressure-combustion TurbineCornell University, 1938 - Gas-turbines |
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20 pages matching plant thermal efficiencies in this book
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Contents
SECTION | 4 |
SECTION THREE Present Day Experience with | 18 |
SECTION FOUR | 26 |
6 other sections not shown
Common terms and phrases
35 atmospheres actual plant adiabatic efficiency assumed atmosphere pressure atoms blades Btu per lb bustion cal per mole centrifugal compressor Chem CO₂ combustion chamber combustion pressures compressed air compression process Compressor efficiencies constant pressure degrees of freedom determinations enthalpy Entropy equipartition of energy estimate excess air exhaust gases exhaust-gas turbine expansion F F F fuel gas turbine gas-turbine plant gases of combustion heat capacity heat exchanger heats of gases high temperature Holzwarth ideal plant increase Ingersoll-Rand internal-combustion engine involved isentropic isothermal efficiencies kinetic energy lb per sq limit Lorenzen losses machine maximum temperature mean specific heat molecule nozzles operate patent performance plant thermal efficiencies products of combustion reciprocating compressor reduced rotor Section shown speeds stages steam plant steam turbine substance supercharging superheater Table 21 temp turbine and compressor turbine exhaust temperature turbo-supercharger unit values velocity Velox vibrational weight