Thermalhydraulic and Conjugate Heat Transfert Analysis of ... · 2 Ensight UGM Paris, France -...

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Thermalhydraulic and Conjugate Heat Transfert Analysis of a 1300 MW PWR Core Internal Baffle Structure Isabelle RUPP EDF R&D

Transcript of Thermalhydraulic and Conjugate Heat Transfert Analysis of ... · 2 Ensight UGM Paris, France -...

Page 1: Thermalhydraulic and Conjugate Heat Transfert Analysis of ... · 2 Ensight UGM Paris, France - September 27, 2010 Outline 1. Introduction 2. Geometry description 3. Numerical tools

Thermalhydraulic and Conjugate Heat Transfert Analysis of a 1300 MW PWR Core Internal Baffle Structure

Isabelle RUPP

EDF R&D

Page 2: Thermalhydraulic and Conjugate Heat Transfert Analysis of ... · 2 Ensight UGM Paris, France - September 27, 2010 Outline 1. Introduction 2. Geometry description 3. Numerical tools

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Outline

1. Introduction2. Geometry description3. Numerical tools and

computation methodology4. Configurations simulated

and results5. High Parallel Computations

with SYRTHES

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Introduction : the reactor vessel internals

About 1800 bolts required for connection between vertical sheets, horizontal formers and core barrelPWR vessel and location of the baffle

- It allows the transition between the polygonal core and the cylindrical core barrel- It protects the vessel (radiation and temperature)

It is important for the lifetime of the power unitsA better knowledge allows maintenance optimization

The internal structure is a baffle-former-barrel bolted assembly

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The problem studied

The internal baffle structure is affected by a strong internal energy deposit induced by gamma radiation (proximity of the core)

After controls, a certain number of bolts were found cracked. Thisphenomenon is attributed to Irradiation Assisted Stress Corrosion Cracking (IASCC)

Temperature is one of the main factors playing a part in the IASCC phenomenon

the goal of this numerical studiy is to gain a better and precise knowledge of the temperature distribution inside the whole structure and particularly around and inside the bolts.

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Methodology

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TRIPOLI calculation

Interpolation of the heat deposit on the SYRTHES mesh

Conjugate heat tranfert calculationSYRTHES / Code_Saturne

Code_Aster

Temperature in the structures

Stresses and strain in the whole structure

Bolts grid for mechanical computation

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1300MWe geometry description

CPY

4 m1.7 m

• 10 formers• Baffle• Core barrel• 1840 bolts

One underlines the large geometrical scale difference between the whole structure and the bolts

After going down through the down-comer, the cold fluid goes up through the core but a small by-pass flow is in charge of cooling the internals structure and the bolts

sector of 45 degrees

Former Baffle

6 cm

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1300 MWe Geometry description – solid part

SYRTHES is a general purpose thermal code using afinite element approach on tetrahedra in 3D. Here the difficulty has been to take into account both a large global geometry and very fine details.

Solid mesh counts 47 million tetraedra

Bolt

Former with bolts

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1300 MWe Geometry description – Fluid part

fluid domain is very complex to mesh because of the cylindrical holes around each bolt

Finite volume approach is used to solve Navier-Stokesaveraged equations. The fluid is assumedincompressible, Newtonien with mass only temperature dependent.Turbulence model used is a classical k-eps model.

Fluid mesh counts 7 million cells

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Energy deposit induced by gamma radiation

The 3D heat source in the solid is calculated thanks to the neutroniccode TRIPOLI IV using a monte-carlo approach on a standard fuel pattern case. As expected the maximum deposit is located around corner near the core in a limited area.Then the deposit field is interpolated on the SYRTHES mesh

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Calculation methodology

Solid32 parts

Fluid256 parts

A coupling between the parallel CFD code Code_Saturneand the parallel thermal code SYRTHES is usedNumber of processors for each domain is chosen to keep a good CPU load balance

Calculation expense : 70 hoursPartitionning is done thanks to METIS

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Results – Fluid flow

Dynamic jets are coming from simple holeswhere small jets are induced by cooling passages around the bolts

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Results – Fluid temperature

The fluid temperature increases when the flow goes upward. But the temperature increase stays moderate.

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Results – Solid temperature

Global temperature

Temperature inside former 6

High temperatures are locatedaround the corner close to

the assemblies

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Former 9

Thickness of former 9 induces high temperatures due to the lack of cooling inside the structure

Results – Solid temperature

F. 6

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High parallel computation with SYRTHESThermal temperature for 6 formers and full 360 degreesHigh parallel computation with SYRTHESThermal temperature for 6 formers and full 360 degrees

Geometry :• Internal baffle• 6 formers (where temperature is much higher)• full 360 degrees• 1128 bolts

View with the core barrel removed

View with the vertical sheets removed

Upside view

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Thermal temperature for 6 formers and full 360 degreesThermal temperature for 6 formers and full 360 degrees

Mesh : 1.1 billion of linear tetrahedra partitionned in 2048 parts

Due to the size, the mesh has been generated by blocks (here by Simail).

Then, “home-made tools” based on octree approaches have been used to join the different blocks and eliminate the common nodes.

METIS 5 has been used to partition each block

Global mesh with the 2048 parts represented

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Calculation has been performed on BlueGene L• 2048 processors used• 100 Mo memory used by processor• Steady state reached in 1h30 CPU time

Temperature field

Thermal temperature for 6 formers and full 360 degreesThermal temperature for 6 formers and full 360 degrees

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Postprocessing with Ensight

Softwares Simail : mesh generatorMetis : mesh partitionningSYRTHES : thermal calculationCode_Saturne : CFD codeEnsight : postprocessing

Mesh file = 72 GbResult file = 3 Gb

EnsightGold file format is required

Minimal configuration required for this case4 processorsBetween 64 Gb and 128 Gb RAM depending on the visualization (cut plane, shadows, iso-values,…)

No particular problem encountered !