FREUDENBERG OIL & GAS TECHNOLOGIES
HAVING A BLAST! SIMULIA UK RUM 2015 Park Royal Hotel, Cheshire 3rd November 2015 Dr. David Winfield & John Stobbart
OIL & GAS TECHNOLOGIES
Contents
Introduction The Blast Chamber
FEA Simulation Methodology Material Model Development Simulation Limitations & Validation
FEA Simulation Results Conclusions & Future Work
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Introduction
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Introduction Project Scope FO> have moved into a larger upgraded facility.
FO> to bring all component qualification programs inhouse for the first time (subsea, topside, onshore, offshore).
Provision of a bespoke testing program for individual, high profile clients.
Blast chamber and auxiliary support equipment (pumps, monitors, piping etc…); £350,000.
Design a blast chamber to contain 0.2 MJ of energy.
Initial developmental ‘Stage 1’ FE simulation of the blast chamber in conjunction with a physical test program. OIL & GAS TECHNOLOGIES Page 4
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The Blast Chamber
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The Blast Chamber Construction & Key Features Steel Girder Polyurethane
Pine
Dampers
(95x250 mm)
Disc Springs
6 mm Blast
Plate
L-Frame Vertical Steel
Concrete Base 20 mm
Column & Base
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Oak
Blast
(120x250 mm)
Plate
The Blast Chamber ….because size is everything!
~450 m3
x4 OIL & GAS TECHNOLOGIES Page 7
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x 643,000 x 11,250,000
FEA Simulation Methodology
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FEA Simulation Methodology Engineering Hurdles
Difficult to design a blast chamber due to the lack of available performance data for materials subjected to ballistic tests.
Assumptions made in hand calculations are extremely specific and do not consider elasto-plastic material properties.
Interaction of components under flexure is difficult to predict.
Blast chamber design must be conservative. High safety factors are required to account for unexpected events.
0.2 MJ; family car travelling at ~40 mph.
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FEA Simulation Methodology ….How to get from A to B
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FEA Simulation Methodology Sub-modelling Architecture
Series of simple sub-models benchmarking factory tests to develop material properties. Series of less complex sub-models of interacting parts with damage and erosion. Single panel impact on nominal geometry to check speed of the solution.
Creation of 3 panel simulation with exact geometries and component positioning. Multiple simulation runs considering projectile position, mass and velocity.
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FEA Simulation Methodology Mesh Discretization
1.02x106 Nodes 795x103 Elements 91 % C3D8R 9 % S4R
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FEA Simulation Methodology Boundary Conditions
Friction co-efficient 0.15 on all contacting surfaces. Ambient temperature (20°C). Eroding surface contact specified. Projectile fired 1 m above ground level at panel center.
6in OD
8.5 kg @ 217 ms-1
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26in OD
0.2 MJ
1,778 kg @ 15 ms-1
Material Model Development
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3 Point Bend Test Rig Physical Testing vs. FEA; Pine & Oak
Test; 57 mm, FEA; 61.6 mm, + 8.1 % OIL & GAS TECHNOLOGIES Page 15
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Test; 173 mm, FEA; 194 mm, + 12.6 %
Ballistic Testing Steel Blast Plates [7]
3D solid plate
3D shell plate
19.3 mm thick
26.7 mm thick
19.8 kg projectile
19.8 kg projectile
80 ms-1
102 ms-1
[7] Health & Safety Executive, Pressure Test Safety; Contract Research Report 168/1998, Department of Chemical Engineering & Chemical Technology and BJS Research.
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Further Sub-Modelling Dampers & Disc Springs Polyurethane 80shoreA Standard ASTM D412-06a test methods. Elastomer material models developed further by Freudenberg GmbH to ensure highly accurate dynamic response.
Δ Dynamic travel (50 mm) 4 (spring) beam elements connecting 2 solid bodies. k = 250 N/mm. ASME VIII Div.2 ANNEX 3-D.
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Simulation Limitations & Validation
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Simulation Limitations
Random nature of grain direction and presence of knots in wooden sleepers means material models are based on average data obtained from 3 point bend test.
Ballistic testing of steel blast plates benchmarked with limited available test data (BRL [7]).
Material models for oak, pine and steel are purposefully kept as simplistic as possible for initial stages of simulation development.
Mass scaling used in very small sections of specific part geometries to improve overall solution timescale (further investigation required to assess impact on final solution).
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FEA Validation Key Features
DATA
THEORY
FEA
(+/-) %
NOTES
Deflection of polyurethane damper
18 mm
9.08 mm
-49 %
Average of 18 dampers around the steel plate before disc spring is energized.
Average bolt force
23,125 N
22,347 N
-4 %
To resist column moment at maximum deflection
Deflection of column
3.31 mm
7.83 mm
+137 %
Recorded at height 1 m above ground before disc spring is energized.
Stress in main support column
519.7 MPa
373.2 MPa
-28 %
Theory limited to elastic properties only
Less flexure in dampers than expected. Greater flexure in steel plate(s). Hand calculations consider elastic material performance only.
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FEA Simulation Results
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FEA Simulation Results 1,778 kg @ 15 ms-1 @ Panel
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FEA Simulation Results 1,778 kg @ 15 ms-1 @ Panel
Dynamic response of dampers Compression of disc springs Flexure of blast plates Free movement in pine/oak sleepers Sway in complete panel(s) Recovery of panel(s)
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FEA Simulation Results 1,778 kg @ 15 ms-1 @ Panel
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FEA Simulation Results 1,778 kg @ 15 ms-1 @ Main Column
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FEA Simulation Results 1,778 kg @ 15 ms-1 @ Main Column
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FEA Simulation Results 1,778 kg @ 25 ms-1 ……THE SHOW STOPPER!!!
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FEA Simulation Results 1,778 kg @ 25 ms-1 ……THE SHOW STOPPER!!!
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Conclusions & Further Work
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Conclusion Detailed ‘Stage 1’ explicit simulation model generated to represent the impact of a projectile into the walls of a custom blast chamber design.
Implementation of simplistic and detailed dynamic material models derived based on physical tests for oak, pine, steel and elastomers.
Blast chamber integrity is maintained up to a total impact energy of 0.2 MJ at multiple impact locations.
Blast chamber can contain a range of projectile geometries and velocities.
Sacrificial failure of multiple components ensures containment integrity. OIL & GAS TECHNOLOGIES Page 30
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Further Work
Based on flexure seen from ‘Stage 1’ simulation, additional design changes and reinforcement will be made.
Factory testing to be scheduled on a mock-up single panel wall section in the guise of a drop test.
Model developed and correlated further based on the dynamics of the drop test.
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Acknowledgements
I would like to thank the following individuals and companies for their invaluable support during the project:
Mr. John Stobbart (Technical Director)
Mr. Laurence Marks & Support Team
Abaqus UK Headquarters, CSE
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OIL & GAS TECHNOLOGIES
Dr. David Winfield
FEA & CFD Development Engineer, R&D Freudenberg Oil & Gas Technologies Ltd – Metal Sealing Solutions - Vector Products
[email protected]
+44(0) 7952 055 963 +44(0) 1639 822 555 ext. 723
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