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Using CAE & Optimisation Tools to Design Lighter and Safer ...NAFEMS World Congress NAFEMS UK...

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NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USA NAFEMS UK Conference 2016 | 15-16 June | Telford | UK Using CAE & Optimisation Tools to Design Lighter and Safer Train Seats Marine Favre Decloux GRM Consulting
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  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Using CAE & Optimisation Tools to

    Design Lighter and Safer Train Seats

    Marine Favre Decloux

    GRM Consulting

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Seats Background

    • M100 seat is a pedestal and wall mounted design, developed for Wabtec. Tested in

    2013 at MIRA and passed all requirements of GM/RT2100 Issue 5.

    • H200 is a development of M100 for HITACHI Rail Europe. Developed in 8 months,

    passing the injury and integrity tests in 2014.

    • M101 uses a combination of both previous designs and learnings from simulation and

    tests.

    • Each seat passed injury and integrity requirements of GM/RT2100 Issue 5 first time.

    M100

    H200

    M101

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    GM/RT 2100 Issue 5

    • New requirements for rail vehicle structures

    • Document mandates requirements for the design and integrity of rail vehicle

    structures for both primary and secondary structures, including interior

    crashworthiness.

    • Conflicting requirements between seat strength and passenger injury.

    • At time of development, no other seats had successfully met requirements.

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Previous test knowledge

    Material Data

    Concept CAD & CAE scoping

    studies

    Master CAE

    model

    Design Design Design

    Simulation Simulation Simulation

    Test

    Methodology

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Modal Analysis / Durability

    Rearward & Forward Integrity

    Forward Injury

    Abuse Load Cases

    Fatigue Load Cases

    Methodology

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    1.5kN Forward1.5kN Forward

    Injury

    50%ile Rearwards

    Integrity

    95%ile Rearwards

    100mm Lateral

    2kN down

    1.5kN Rear 1.5kN Rear

    2kN down

    1.5kN Grab Handle

    GM/RT 2100 Seat Load Cases

    Integrity

    95%ile Forwards

    Injury

    50%ile Forwards

    • All projects use finite design and

    simulation resources.

    • GRM’s approach has been to prioritise

    load-case development

    – Red – Checked & developed daily

    – Amber – Checked weekly

    – Green – Designed in from start

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Methodology

    Manufacturability

    Lightweighting

    Cost

    Strength & stiffness

    Concept Design

    Optimisation Tools

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Armrest Cover Ribs Optimisation

    Abuse load cases to represent

    150kg individual standing on trim

    Initial Aluminium

    armrest cover

    Creation of candidate material

    using RDM tool in Genesis

    Topology

    Optimisation Results

    Definition of

    manufacturing

    constraints

    Topology Optimisation

    for multiple load cases

    in Genesis

    Optimisation keeps

    solid element at the

    locations where

    reinforcements are

    required

    Initial Aluminium

    armrest cover

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Armrest Cover Ribs Optimisation

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Reinforcement Derivation Method

    • An existing FE structure is

    our starting point

    • The RDM® region is

    automatically created in

    Design Studio over the top at

    user-defined limits

    • Genesis carries out an

    optimisation for multiple load-

    cases, removing superfluous

    material and only leaving the

    most important parts

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Cantilever Pedestal Design

    Package Space

    DefinitionTopology

    optimisation Design

    Interpretation

    Folded Sheet

    Stiffness &

    Modal

    Final DesignSizing & Topology

    optimisation refinement

    Sheet thick. (mm)

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    • Forward and Rearward Integrity tested with two 95th percentile dummies on various

    pitch and seat configurations (single/double/triple, 1st & standard class) to determine

    the worst case scenario to be tested.

    • Axial and shear forces measured at wall fixing points for bolt design.

    • Plastic strain in pedestal and wall brackets recorded to ensure that the seat will remain

    attached to the carriage. Seat-back longitudinal deflection recorded.

    Crashworthiness & Seat Integrity

    Loads (kN)

    A B C D E F

    Axial 32 14 -16 -13 33 9

    Plastic Strain

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    • Injury values extracted from simulation of forward impact. Design changes were

    quickly implemented and the subsequent change on injuries determined.

    • Use simulation to determine the injury criteria closest to the legal standards defined in

    GM/RT2100 Issue 5.

    CriteriaGM/RT2100

    LimitSimulation

    Femur Load Left (kN)5.7

    4.8

    Femur Load Right (kN) 4.5

    Knee Shear Left (mm)16.0

    9.7

    Knee Shear Right (mm) 10.9

    Tibia Load Left (kN)8.0

    1.1

    Tibia Load Right (kN) 0.98

    Tibia Index Left1.3

    0.62

    Tibia Index Right 0.75

    Neck Tension (kN) 4.17 0.57

    Neck Compression (kN) 4.0 1.10

    Neck Flexion (Nm) 310 95

    Neck Extension (Nm) 135 26

    Neck Injury Criteria 1.0 0.61

    HIC 500 96

    3ms Clip 80 46

    Injury Prediction

    Peak force extracted

    Cross-section View

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    • Adhesive testing was carried out by 3M on various

    adhesive materials.

    • A model was built to replicate the adhesive test procedure

    with tiebreak contact between the aluminium sample and

    the adhesive, which allows the failure force to be specified.

    • The failure force value was set-up to achieve the same

    failure characteristic seen in the adhesive test.

    • Calibrated adhesive was then used to build accurate FE

    model with material failure.

    Adhesive Testing & Modelling

    Sample

    1

    Sample

    2

    Sample

    3

    Sample

    4Sample

    5

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Seat Back Design

    • Design sensitivity to seat-back shape / section profiles.

    • Aim is to use the seat-back shape to absorb the energy of a crash to reduce

    the leg injuries. Achieved through the unfolding behaviour of the section profile.

    • Different shapes were tested to meet visual aspect requirements as well as

    injury targets.

    CriteriaGM/RT2100 Limit

    CAE limit

    (80%)Design 2 Design 8 Design 11

    Femur Load Left (kN)

    5.7 4.565.7 6.5 5.3

    Femur Load Right (kN)

    5.3 6.2 5.0

    Knee Shear Left (mm)

    16.0 12.813.2 13.0 11.9

    Knee Shear Right (mm)

    16.8 16.4 14.1

    Design 2 Design 8 Design 11

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Seat Back Model

    • Variation of thickness due to stamping was mapped on the seat back, based

    on material thickness of 1.6mm.

    • Thickness results used in the injury and integrity impact simulations to improve

    the performance prediction.

    Thickness (mm)

    1.6mm based seat-back

    CriteriaGM/RT2100

    LimitCAE limit

    (80%)

    No Thickness mapping

    With thickness mapping

    Test Results

    Femur Load Left (kN)5.7 4.56

    5.3 4.8 4.6

    Femur Load Right (kN) 5.0 4.5 4.2

    Knee Shear Left (mm)16.0 12.8

    12.1 9.7 8.2

    Knee Shear Right (mm) 13.7 10.9 10.9

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Optimisation & Accurate

    Predictive Modelling• CAE led design to meet all targets 1st time

    • Optimisation tools to design lightweight, stiff and strong train seats

    - RDM based on Topology Optimisation for internal reinforcement

    - Topology Optimisation for cantilever pedestal design

    - Combined Sizing & Topology for additional weight saving

    • Test prediction highly depending on FE model quality

    - Accurate adhesive model with failure from physical test correlation

    - Stamping effect accounted for real seat-back thickness

    - Dummy injury knowledge from previous automotive projects

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Forward Injury Test

    CriteriaGM/RT2100

    LimitSimulation Test

    Femur Load Left (kN)5.7

    4.8 4.6

    Femur Load Right (kN) 4.5 4.2

    Knee Shear Left (mm)16.0

    9.7 8.2

    Knee Shear Right (mm) 10.9 10.9

    Tibia Load Left (kN)8.0

    1.1 0.93

    Tibia Load Right (kN) 0.98 0.72

    Tibia Index Left1.3

    0.62 0.72

    Tibia Index Right 0.75 0.99

    Neck Tension (kN) 4.17 0.57 1.19

    Neck Compression (kN) 4.0 1.10 0.18

    Neck Flexion (Nm) 310 95 127

    Neck Extension (Nm) 135 26 26

    Neck Injury Criteria 1.0 0.61 0.42

    HIC 500 96 150

    3ms Clip 80 46 62

    • Forward injury test shows good correlation with simulation. Differences are mainly due

    to dummy positioning.

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Rearwards Integrity Test• Rearwards integrity result is a pass as seat remains attached to rail structure and seat

    is also well within the survival space envelope as predicted.

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK

    Conclusions

    • CAE analysis and optimisation tools made it possible to design three

    generations of lightweight train seats, each passing both integrity

    and injury tests first time.

    • FE analysis saved time and money allowing the team to deliver a

    design 35% lighter than standard train seats.

  • NAFEMS World Congress 2015 | 21-24 June | San Diego | California | USANAFEMS UK Conference 2016 | 15-16 June | Telford | UK


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