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METHODOLOGICAL ASPECTS FOR NUMERICAL ANALYSIS OF LID SYSTEMS FOR SNF AND HLW
TRANSPORT PACKAGES
Konrad Linnemann, Viktor Ballheimer Jens Sterthaus
Frank Wille
BAM, Germany
Package Analysis: Structural Analysis Special Topics
METHODOLOGICAL ASPECTS FOR NUMERICAL ANALYSIS OF LID SYSTEMS FOR SNF AND HLW
TRANSPORT PACKAGES
Konrad Linnemann Viktor Ballheimer Jens Sterthaus
Frank Wille
BAM Federal Institute for Materials Research and Testing Berlin, Germany
PATRAM 2013 3 BAM / 3.3 / Linnemann
Outline
General aspects about Type B(U) lid systems
Numerical assessment of lid systems according to guideline
BAM-GGR 012
Finite element modeling strategy
Numerical Solutions • 9 m vertical drop test • 9 m lateral drop test
Concluding Remarks
PATRAM 2013 4 BAM / 3.3 / Linnemann
General Aspects
protective plate
pressure sensor
secondary lid
primary lid
basket
trunnion cask cooling fin neutron moderator
Transport and Interim storage Casks for Spent Fuel and HAW 2 bolted lids (primary and secondary)
as part of the containment system Lid system as barrier
• Lid + bolts • Inner metallic gasket
(aluminum or silver) • Outer elastomeric gasket • Orifice Lids
PATRAM 2013 5 BAM / 3.3 / Linnemann
General Aspects / Assessment of lid systems
Activity release criteria specified by IAEA regulations SSR-6 under routine, normal and accident condition of transport (RCT, NCT, ACT)
BAM-GGR012 Guideline for numerical assessment of bolted lid and trunnion systems
Drop tests Gasket performance tests Numerical analyses
Combined methods of assessment
Assessment of lid system by ensuring Integrity Leak tightness
PATRAM 2013 6 BAM / 3.3 / Linnemann
Numerical Assessment According to BAM-GGR012
General criterion for lid • Assessment with local stresses:
e.g. to exclude local plastic deformations
• Brittle fracture assessment: BAM-GGR 007, FKM-Guideline
Displacements / deformations in gasket area (e.g. opening, sliding) • Assessment of sealing function based
on results of drop tests and gasket performance tests
• Assume minimum pretension for bolts
Bolt assessment • Nominal stress concept • Assume pretension range for bolts
PATRAM 2013 7 BAM / 3.3 / Linnemann
Numerical Assessment According to BAM-GGR012
Load steps
Loading (RCT, NCT, ACT)
Unloading (Assessment openings gasket)
Assembly (Tightening of bolts)
Criteria for bolts BAM-GGR012
tens
ile
equi
vale
nt
PATRAM 2013 8/18 BAM / 3.3 / Linnemann
Dynamic FEA (explicit time integration)
Advantages Modeling of whole packages Realistic application of loads Disadvantages Material modeling e.g. of wooden
shock absorbers Time increment’s dependency on
characteristic element length
Modeling Strategy / Explicit vs. Implicit
Quasi-static FEA (implicit time integration)
Advantages Detailed stress assessment
Disadvantages Constant and homogeneous
acceleration field Requires extra load factors for
considering dynamic effects
Mechanical System Dynamic problem, multiple mass effects Accelerations and thermal loads (NCT, ACT) + interior pressure Contact problem: Lid cask body + bolt head lid Tightening of bolts minimum and maximum pretension
PATRAM 2013 9 BAM / 3.3 / Linnemann
Modeling Strategy / Lid Systems
Quasi-static implicit analysis with homogeneous acceleration field Extra load factors considering internal impacts Elastic material model for bolt assessment Elastic-plastic material for assessment of deformations in gasket area
9m lateral drop test thermal test 9m vertical drop test
Reduction of modeled components
PATRAM 2013 10 BAM / 3.3 / Linnemann
Modeling Strategy / Numerical Evaluation
Calculation of according to VDI 2230
section Evaluation of axial forces N and bending moments M
along clamping length
For each section: Integration of nodal forces
Calculation of nominal stresses
BAM-GGR012: Nominal stress concept for bolts
(tensile) (bending) (equivalent)
PATRAM 2013 11 BAM / 3.3 / Linnemann
Calculation Results / 9 m Vertical Drop
FE-Model Quasi-static analysis of primary lid system considering 9 m vertical
drop test Symmetry circular sector with 1 bolt of strength grade 10.9 Incrementally increased homogeneous acceleration until 100 g Reaction forces of metallic gasket as constant surface loads
PATRAM 2013 12/18 BAM / 3.3 / Linnemann
Calculation Results / 9 m Vertical Drop
s
PATRAM 2013 13 BAM / 3.3 / Linnemann
Calculation Results / 9 m Vertical Drop
Evolution of bolt stresses
Sensitivity of bolt stresses with respect to requirements
69 (decisive load case)
PATRAM 2013 14 BAM / 3.3 / Linnemann
Calculation Results / 9 m Vertical Drop
Low penetrations of contact surfaces, but influence on remanent values Cumulative assessment of irreversible displacements for the gasket groove
under consideration of all ACT tests (especially 30 min. fire test)
Evolution of maximum opening during loading and unloading
PATRAM 2013 15 BAM / 3.3 / Linnemann
Calculation Results / Dynamic Analysis
FE-Model Dynamic model (LS-DYNA) Initial velocity and pressure impulse p(t) No multiple mass effect Comparison with quasi-static solution
PATRAM 2013 16 BAM / 3.3 / Linnemann
Calculation Results / Dynamic Analysis
Bolt stresses relative to static solution (tensile and bending)
Dynamic amplification factor 1.9 for assumed load
PATRAM 2013 17 BAM / 3.3 / Linnemann
Calculation Results / 9 m Lateral Drop
Quasi-static implicit analysis for assessing 9 m lateral drop Half-model of primary lid system based on symmetry Incrementally increased acceleration field until 180 g 22.5 bolts of strength grade 10.9
180 g
PATRAM 2013 18 BAM / 3.3 / Linnemann
Calculation Results / 9 m Lateral Drop
Evolution of bolt stresses
A
B C
D
A, B: Begin of sliding between lid and cask
C, D: Begin of sliding between bolt head and lid
PATRAM 2013 19 BAM / 3.3 / Linnemann
Concluding Remarks
Modeling strategies • Quasi-static (implicit) and dynamic (explicit) FEA • Aspects of implicit modeling
Assessment methods for lid systems of Type B(U) packages • BAM GGR012 Guideline • Criteria of bolts
Presented Solutions • 9 m vertical and lateral drop • Bolt assessment based on nominal stress concept • Displacements in gasket area • Sensitivity of assessment criteria with respect to applied load • Evaluation of dynamic amplification with a simplified dynamic
model for the 9 m vertical drop