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Numerical simulation and analysis of axial instabilities occurrence and development in turbomachines. Application to a break transient in a helium nuclear reactor; Simulation numerique et analyse du declenchement et du developpement des instabilites axiales dans les turbomachines: application a un transitoire de breche dans un reacteur nucleaire a helium

Abstract

The subject of the present work was to develop models able to simulate axial instabilities occurrence and development in multistage turbomachines. The construction of a 1D unsteady axisymmetric model of internal flow in a turbomachine (at the scale of the row) has followed different steps: generation of steady correlations, adapted to different regimes (off-design conditions, low mass flowrate, negative mass flow rate); building of a model able to describe transient behaviour; use of implicit time schemes adapted to long transients; validation of the model in comparison of experimental investigations, measurements and numerical results from the bibliography. This model is integrated in a numerical tool, which has the capacity to describe the gas dynamics in a complete circuit containing different elements (ducts, valves, plenums). Thus, the complete model can represent the coupling between local and global phenomena, which is a very important mechanism in axial instability occurrence and development. An elementary theory has also been developed, based on a generalisation of Greitzer's model. These models, which were validated on various configurations, have provided complementary elements for the validation of the complete model. They have also allowed a more comprehensive description of physical phenomena at stake in instability occurrence and development by  More>>
Authors:
Publication Date:
Feb 15, 2006
Product Type:
Thesis/Dissertation
Report Number:
FRNC-TH-7081
Resource Relation:
Other Information: TH: These mecanique; [190 refs.]; Also available from Ecole centrale de Lyon. Bibliotheque, 36, rue Guy de Collongue, 69134 - Ecully Cedex (France)
Subject:
42 ENGINEERING; AFTER-HEAT REMOVAL; BRAYTON CYCLE; COMPUTERIZED SIMULATION; DEPRESSURIZATION; FLOW MODELS; FLOW RATE; GAS COMPRESSORS; HELIUM COOLED REACTORS; INSTABILITY; OSCILLATIONS; PRESSURE DEPENDENCE; PUMPING; TEMPERATURE DISTRIBUTION; TRANSIENTS; TURBOMACHINERY
OSTI ID:
20992584
Research Organizations:
Ecole Centrale de Lyon, 69 - Ecully (France)
Country of Origin:
France
Language:
French
Other Identifying Numbers:
TRN: FR0704429016514
Availability:
Available from INIS in electronic form
Submitting Site:
FRN
Size:
263 pages
Announcement Date:
Mar 27, 2008

Citation Formats

Tauveron, N. Numerical simulation and analysis of axial instabilities occurrence and development in turbomachines. Application to a break transient in a helium nuclear reactor; Simulation numerique et analyse du declenchement et du developpement des instabilites axiales dans les turbomachines: application a un transitoire de breche dans un reacteur nucleaire a helium. France: N. p., 2006. Web.
Tauveron, N. Numerical simulation and analysis of axial instabilities occurrence and development in turbomachines. Application to a break transient in a helium nuclear reactor; Simulation numerique et analyse du declenchement et du developpement des instabilites axiales dans les turbomachines: application a un transitoire de breche dans un reacteur nucleaire a helium. France.
Tauveron, N. 2006. "Numerical simulation and analysis of axial instabilities occurrence and development in turbomachines. Application to a break transient in a helium nuclear reactor; Simulation numerique et analyse du declenchement et du developpement des instabilites axiales dans les turbomachines: application a un transitoire de breche dans un reacteur nucleaire a helium." France.
@misc{etde_20992584,
title = {Numerical simulation and analysis of axial instabilities occurrence and development in turbomachines. Application to a break transient in a helium nuclear reactor; Simulation numerique et analyse du declenchement et du developpement des instabilites axiales dans les turbomachines: application a un transitoire de breche dans un reacteur nucleaire a helium}
author = {Tauveron, N}
abstractNote = {The subject of the present work was to develop models able to simulate axial instabilities occurrence and development in multistage turbomachines. The construction of a 1D unsteady axisymmetric model of internal flow in a turbomachine (at the scale of the row) has followed different steps: generation of steady correlations, adapted to different regimes (off-design conditions, low mass flowrate, negative mass flow rate); building of a model able to describe transient behaviour; use of implicit time schemes adapted to long transients; validation of the model in comparison of experimental investigations, measurements and numerical results from the bibliography. This model is integrated in a numerical tool, which has the capacity to describe the gas dynamics in a complete circuit containing different elements (ducts, valves, plenums). Thus, the complete model can represent the coupling between local and global phenomena, which is a very important mechanism in axial instability occurrence and development. An elementary theory has also been developed, based on a generalisation of Greitzer's model. These models, which were validated on various configurations, have provided complementary elements for the validation of the complete model. They have also allowed a more comprehensive description of physical phenomena at stake in instability occurrence and development by quantifying various effects (inertia, compressibility, performance levels) and underlying the main phenomena (in particular the collapse and recovery kinetics of the plenum), which were the only retained in the final elementary theory. The models were first applied to academic configurations (compression system), and then to an innovative industrial project: a helium cooled fast nuclear reactor with a Brayton cycle. The use of the models have brought comprehensive elements to surge occurrence due to a break event. It has been shown that surge occurrence is highly dependent of break location and that surge development is very limited (no more than few seconds). It is also shown that in the case of a break event, the turbomachine can have a significant contribution to decay heat removal from the nuclear core. At last, such a device is autonomous for a certain time only, and that this time is sensitive to some parameters such as break location and back pressure value. (author)}
place = {France}
year = {2006}
month = {Feb}
}