Abstract
The direct coupling of a gas cooled reactor with a closed gas turbine cycle leads to a specific dynamic plant behaviour, which may be summarized as follows: a) any operational transient involving a variation of the core mass flow rate causes a variation of the pressure ratio of the turbomachines and leads unavoidably to pressure and temperature transients in the gas turbine cycle; and b) very severe pressure equalization transients initiated by unlikely events such as the deblading of one or more turbomachines must be taken into account. This behaviour is described and illustrated through results gained from computer analyses performed at the Swiss Federal Institute for Reactor Research (EIR) in Wurenlingen within the scope of the Swiss-German HHT project.
Dang, M.;
Dupont, J. F.;
Jacquemoud, P.;
Mylonas, R.
[1]
- Eidgenoessisches Inst. fuer Reaktorforschung, Wuerenlingen (Switzerland)
Citation Formats
Dang, M., Dupont, J. F., Jacquemoud, P., and Mylonas, R.
Pressure transients analysis of a high-temperature gas-cooled reactor with direct helium turbine cycle.
IAEA: N. p.,
1981.
Web.
Dang, M., Dupont, J. F., Jacquemoud, P., & Mylonas, R.
Pressure transients analysis of a high-temperature gas-cooled reactor with direct helium turbine cycle.
IAEA.
Dang, M., Dupont, J. F., Jacquemoud, P., and Mylonas, R.
1981.
"Pressure transients analysis of a high-temperature gas-cooled reactor with direct helium turbine cycle."
IAEA.
@misc{etde_8469474,
title = {Pressure transients analysis of a high-temperature gas-cooled reactor with direct helium turbine cycle}
author = {Dang, M., Dupont, J. F., Jacquemoud, P., and Mylonas, R.}
abstractNote = {The direct coupling of a gas cooled reactor with a closed gas turbine cycle leads to a specific dynamic plant behaviour, which may be summarized as follows: a) any operational transient involving a variation of the core mass flow rate causes a variation of the pressure ratio of the turbomachines and leads unavoidably to pressure and temperature transients in the gas turbine cycle; and b) very severe pressure equalization transients initiated by unlikely events such as the deblading of one or more turbomachines must be taken into account. This behaviour is described and illustrated through results gained from computer analyses performed at the Swiss Federal Institute for Reactor Research (EIR) in Wurenlingen within the scope of the Swiss-German HHT project.}
place = {IAEA}
year = {1981}
month = {Jan}
}
title = {Pressure transients analysis of a high-temperature gas-cooled reactor with direct helium turbine cycle}
author = {Dang, M., Dupont, J. F., Jacquemoud, P., and Mylonas, R.}
abstractNote = {The direct coupling of a gas cooled reactor with a closed gas turbine cycle leads to a specific dynamic plant behaviour, which may be summarized as follows: a) any operational transient involving a variation of the core mass flow rate causes a variation of the pressure ratio of the turbomachines and leads unavoidably to pressure and temperature transients in the gas turbine cycle; and b) very severe pressure equalization transients initiated by unlikely events such as the deblading of one or more turbomachines must be taken into account. This behaviour is described and illustrated through results gained from computer analyses performed at the Swiss Federal Institute for Reactor Research (EIR) in Wurenlingen within the scope of the Swiss-German HHT project.}
place = {IAEA}
year = {1981}
month = {Jan}
}