1982
DOI: 10.1007/978-3-642-96632-3
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Thermische Turbomaschinen

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Cited by 51 publications
(15 citation statements)
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“…The isentropic efficiency of the turbines is calculated from the real data of the existing plant by means of the turbine constant defined here. The turbine constant is a parameter that depends on the turbine mass flow, the inlet temperature as well as inlet and outlet pressure defined as (see e.g., [18]): The plant net output power is 264MW with an efficiency of 33% (LHV).Live steam temperature, pressure and mass flow (point 1 in Figure 1) is 500˝C, 80 bar and 280 kg/s, respectively. The power required to generate such steam is about 756.168 MW, which can be calculated from the enthalpy difference between the economizer inlet and super heater outlet (live steam) multiplied by the mass flow rate.…”
Section: Original Plant Modelmentioning
confidence: 99%
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“…The isentropic efficiency of the turbines is calculated from the real data of the existing plant by means of the turbine constant defined here. The turbine constant is a parameter that depends on the turbine mass flow, the inlet temperature as well as inlet and outlet pressure defined as (see e.g., [18]): The plant net output power is 264MW with an efficiency of 33% (LHV).Live steam temperature, pressure and mass flow (point 1 in Figure 1) is 500˝C, 80 bar and 280 kg/s, respectively. The power required to generate such steam is about 756.168 MW, which can be calculated from the enthalpy difference between the economizer inlet and super heater outlet (live steam) multiplied by the mass flow rate.…”
Section: Original Plant Modelmentioning
confidence: 99%
“…The isentropic efficiency of the turbines is calculated from the real data of the existing plant by means of the turbine constant defined here. The turbine constant is a parameter that Energies 2016, 9, 399 4 of 22 depends on the turbine mass flow, the inlet temperature as well as inlet and outlet pressure defined as (see e.g., [18]):…”
Section: Original Plant Modelmentioning
confidence: 99%
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“…The masses for the casing and the shaft are considered in corresponding wall models. The mass flow through the turbine section is calculated by using Stodola's law [4]. Heat transfer between the steam and the casing respectively the shaft is calculated at the inlet volume.…”
Section: Modeling Approachmentioning
confidence: 99%
“…The obtained material temperature is then used to get an allowable stress level from a material database. With some simplified beam theory methods [11] a first estimate of the airfoil's radial area distribution and its mass is made possible. Even though this procedure is a good starting point, it has some disadvantages: If the material temperature used for the airfoil design is determined from the mean gas temperatures and the cooling air assumptions only, all uncertainties of the prediction are directly transferred to the allowable design stress and the estimated mass.…”
Section: Introductionmentioning
confidence: 99%