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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1017
Virtual Durability Simulation for Chassis of Commercial vehicle
Mahendra A Petale
M E (Mechanical Engineering) G S Moze College of Engineering Balewadi Pune -4111025
Prof. Manoj J Sature
Asst. Professor G S Moze College of Engineering, Balewadi Pune, India - 411 045
---------------------------------------------------------------------***--------------------------------------------------------------------------
Abstract – In conventional virtual validation by
Computer Aided Design of truck chassis was based on the
static analysis based. Load cases derived was by
Experience. This led to some of the critical areas being
unnoticed. Hence, it was necessary to rely on physical
testing for the validation of the design, which is costly and
time consuming. In order to fast track the development &
cut short the validation time and cost , validation of new
product or design a technique is required that depends on
virtual prototype testing at the design stage of
development. The use of multi body dynamics and finite
element method makes this task simple and accurate
taking into account the road load data ( RLD ) stress
history and multi axial stress field, thus making the
durability predictions moreaccurate. In thispaperVirtual
validation Methodology using RLD approach for a typical
heavy truck Chassis is presented with good correlation
with Physical validation reducing overall design and
development cost and time to deliver first time right
product.
Key words—RLDA , CAE, MBD, Rig Testing,Fatiguelife,
Design optimisation
1. INTRODUCTION
In the past, the CAE validation of truck cabin and
chassis was based on the conventional static analysis
based on the load cases derivedbyexperience.Thisledto
some of the critical areas being unnoticed. Hence, it was
necessary to rely on physical testing for the validation of
the design.
The physical prototype testing is a time and cost
consuming activity. In order to reduce the development
period, development cost and number of prototypes, a
technique is required that depends on virtual prototype
testing at the design stage of development. Thanks to
recent improvements in computer performance and the
availability of the commercial finite element & fatigue
softwares. Using these commercially availably codes ,
engineers can conduct fatigue analysis that take into
account the road load data ( RLD ) stress history and
multi axial stress field, thus making the durability
predictions moreaccurate.
The accelerated testing is done on a multi poster test rigs
on cab and chassis separately. The acceleration history to
the multi-poster test rigs is derived from proving ground
(torture track) history. The truck cabin is fitted on part of
chassis frame along with its suspension for testing.
Similarly, the chassis is suspended at its front and rear
suspension area. In order to predict the durability by
fatigue analysis, the multi axial stress fields are required
for the entire load history. The use of multi body
dynamics and finite element method makes this task
simple andaccurate.
The case study of a typical heavy truck (both chassis
& cabin) ispresentedwithdetailedsimulationprocedure.
2. MULTI POSTER DURABILITY TESTING &
SIMULATION
The fatigue strength of Frame is generally assessed
through the proving ground (torture track) testing
and accelerated tests like four-poster testing. In a
four-poster test, the displacementhistoryofthefour
hydraulicshakersisfirstdeterminedusingtheframe
accelerations determined from the experimental
rough road driving, and input accelerations
experienced by an actual vehicle in field. In multi
poster test, the load history is reduced by reducing
non damaging events in order to shorten the test
time. This is done through the damage correlation
between the rough road driving, torture track test-
driving & multi poster test. The typical multi poster
test setups are shown in Fig. 1 and 2
Chassis FatigueTestingisacceleratedtestprocedure
similar to 4-poster test, which is used for chassis
durability. In this testing alongwithZ-directionroad
inputs, X and Y (Longitudinal and Lateral) direction
inputs, braking torque loads are considered. In case
of chassis, the Longitudinal and lateral forces are
significant in addition to Z forces. A 22-poster test
rig used for 6 x 4 tractor – 49T Tractor
- all direction road excitations
- braking effects
- Cabin and engine excitations to Chassis.
- Fifth wheel reactions
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1018
Fig 1- Typical Multi Poster set up
Fig 2- Multi Poster Test Rig for Frame
Fig 3- Fifth Wheel constraint arrangement
The cabin weight, Powertrain weight, fifth wheelloads
are applied by actuators with suitable fixtures. The effect
of above aggregates in vehicle running condition is
simulated. Refer fig. 2 &3
Fig 4 –Power Train arrangement
Methodology adopted
 Review present conentional system of design
optimisation
 Identify the aggregates requiring optimisation
 Build initial 3 D CAD model of the vehicle
aggregates in Pro-e or CATIA software
 Do initial Finite Element analysis for the built
CAD model with analyiss softwares like
hypermesh , NASTRAN
 Find out the critical zones or areas related to
maximum stress / deflection in order to decide
intrumentation points on the physical parts
 Identify the referance vehicle model for
intrumentation and capturing road load data
 Identify the service routes where new model will
be subjected to usage for desired target life of
product
 Intrument the referance vehicle at various
locations as identified in the earlierstep withthe
help of various devices like straingauging,LVDT,
WFT, Accelerometer, RPM meter, Rosette as the
requirment of capturing output like strain ,
displacment , Forces along XYZ, Moments about
XYZ for damage analysis,damageeditandcontrol
 Do physical running of the instrumented vehicle
on identified with the desired payload and
application speed , grade and acceleration
 Data acquisition by use of data acquisition
system like eDAQ plus (SOMAT) which is having
64 Channel analog, 500 Hz sampling rate , GPS
channels , Digital inputs
 Analysis of the measured data using analysis
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1019
software like ICE-flo GlyphWorks, Plotting
amplitude time history , rainflow analysis with
respect to number of cycles and rainflow change
histogram
 Development of correlation with service usage
and proven ground (torture track) in order to
decide number of cycles for service life usage ,
Signal processing and damage edit , drive file
generation
 Kinematic model building in ADAMS based on
drive file and extraction of forces
 Durability analysis (Virtual simulation)of the3D
CAD model Fatigue calculation software like
FEMFAT, Design Optimisation usingoptistruck &
Hyperstudy
Below are below two major steps followed
2.1 Transformation of rig test signals to
load time histories at chassis attachment
points through ADAMS
On- road / torture track testing of vehicle for
predefined cycles is the general way to evaluate
durability of frame mountings. Performing on-
road testing, as number of vehicle variants
increases, is time consuming and costly affair.
Hence, with the objective to perform vehicle
frame durability evaluation at laboratory level
and to accelerate testing activity, this full Frame
fatigue test evaluation has been planned. Drive
files for the rig using the strain, LVDT and WFT
data is collected by instrumenting reference
vehicle and running on service road.
Frame Fatigue analysis test rig set up there is
actuators (J1 to J19) are used for giving axle
vertical motion, axle longitudinal force, axle
lateral force and cab vertical force input. One end
of all above-mentioned actuators is connected to
rigid structure. Two rubber bush are provide
between frame and fifth wheel assembly. Axles
are excited through adapter assembly, which are
fixed together.
Fig 4 – Frame Fatigue test ADAMS Model
The test activity is performed in the virtual world
throughsimulationsusingADAMSandNastran,FE
fatigue. Equivalent ADAMS model is made
replicates test setup. This ADAMS multi body
simulation is performed giving the displacement
input drive file at the four-poster leg locations. The
multi body dynamic analysis output is the force
history at all the mounting locations on the cab.
Dynamics analysis is performed to get the load
historyatvariousfrontandrearsuspensionmount
locations.
Theattachmentpointloadtimehistoriescalculated
through ADAMS are then used to calculate fatigue
life. These time histories is taken as input for
durability simulation
2.2 Durability simulation for fatigue life
simulation
Fig 5 & 6 shows the flowchart of simulation method
used for the prediction of fatigue strength of frame.
This method makes use of various CAE solvers like
MSC-ADAMS, MSC-NASTRAN & MSC-FATIGUE. The
brief description of the process is as given below.
First, a finite elementmodel of the Chassis is created
using CAD data and then an eigen value analysis is
performed using NASTRAN. The results of the eigen
value analysis are then converted into an ADAMS’s
modal model using ADAMS/FLEX.
After this detailed modelling, ADAMS multi body
simulation as per earlier process performed giving
the displacement input drive file at the four-poster
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1020
leg locations. The multi body dynamic analysis
output is the force history at all the mounting
locations on the cab. This history is then combined
with the NASTRAN’s static unit load inertia relief
analysis results to obtainastresshistoryinthecabin
for the entire multi poster cycle using linear
superposition method.
Fig 5 –Chassis Simulation process flowchart
Fig 6 –Fatigue analysis process in MSc Fatigue
This process of linear superposition method
followed by rain flow cycle counting & finding the
cumulative damage by Miner’s rule&finallyarriving
at fatigue life of cabin isperformedinMSC-FATIGUE.
Refer fig.6 for the schematic model of the analysis
process.
Fig 7- Rear Cross member Gusset Location
Fig 8- Engine Mounting cross member location
Table 1 shows the detailed durability simulation
results for the Chassis. Based on this it’s concluded
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056
Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072
© 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1021
that Chassis is meeting target fatigue life cycles as
required
TABLE 1 (Durability Simulation Result Summary)
3 CONCLUSION
This virtual simulation methodology for durability
life prediction can be effectively used at the design
stage for evaluating the fatigue durabilitychassisfor
eliminating expensive physical prototype testing. A
virtual simulation methodology was developed for
finding out the vehicle durability, which has a
correlation with physical testing in terms of the
sequence of failure and locations, and number of
cycles. This simulation methodology makes use of
input test data, multi-body dynamics & finite
element method. This methodology eliminates the
use of static assumed service load cases, which do
not represent the full dutycycle to which the vehicle
will be subjected. This is very effective simulation
tool which can be used during design and
development of new products reducing overall
development time and cost of Design iteration and
physical validation.
ACKNOWLEDGMENT
I would like to express my special thanks of
gratitude to my superiors who gave this golden
opportunity to do this wonderful project which also
helped me in doing lot of Research and I came to
know about so many new things.Iamreallythankful
to them. Secondly I would also like to thank my
family and Friends who helped to complete this
project in limited time period.
REFERENCES
[1] Automotive Structures". SAE Technical Paper950711,
1995.
[2] MSC/PATRAN User's Manual, 2005, The MacNeal
Schwendler Corporation, Los Angeles, CA, March 2005
[3] Morrow, J. D. Fatigue Design Handbook, Section 3.2,
SAE Advances in Engineering,Vol. 4,
[4] Society for Automotive Engineers, Warrendale, PA,
1968, pp.21–29.
[5]Alex Porter “Accelerated testing and validation”
BIOGRAPHIES
Mahendra A Petale is working in
Leading Automotive Industry. He
is leading DesignandDevelopment
of future generation commercial
vehicles starting from concept to
launch. He has wide experience in
Key aggregate designs, Product
finalization and ValueEngineering.

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Virtual Durability Simulation

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1017 Virtual Durability Simulation for Chassis of Commercial vehicle Mahendra A Petale M E (Mechanical Engineering) G S Moze College of Engineering Balewadi Pune -4111025 Prof. Manoj J Sature Asst. Professor G S Moze College of Engineering, Balewadi Pune, India - 411 045 ---------------------------------------------------------------------***-------------------------------------------------------------------------- Abstract – In conventional virtual validation by Computer Aided Design of truck chassis was based on the static analysis based. Load cases derived was by Experience. This led to some of the critical areas being unnoticed. Hence, it was necessary to rely on physical testing for the validation of the design, which is costly and time consuming. In order to fast track the development & cut short the validation time and cost , validation of new product or design a technique is required that depends on virtual prototype testing at the design stage of development. The use of multi body dynamics and finite element method makes this task simple and accurate taking into account the road load data ( RLD ) stress history and multi axial stress field, thus making the durability predictions moreaccurate. In thispaperVirtual validation Methodology using RLD approach for a typical heavy truck Chassis is presented with good correlation with Physical validation reducing overall design and development cost and time to deliver first time right product. Key words—RLDA , CAE, MBD, Rig Testing,Fatiguelife, Design optimisation 1. INTRODUCTION In the past, the CAE validation of truck cabin and chassis was based on the conventional static analysis based on the load cases derivedbyexperience.Thisledto some of the critical areas being unnoticed. Hence, it was necessary to rely on physical testing for the validation of the design. The physical prototype testing is a time and cost consuming activity. In order to reduce the development period, development cost and number of prototypes, a technique is required that depends on virtual prototype testing at the design stage of development. Thanks to recent improvements in computer performance and the availability of the commercial finite element & fatigue softwares. Using these commercially availably codes , engineers can conduct fatigue analysis that take into account the road load data ( RLD ) stress history and multi axial stress field, thus making the durability predictions moreaccurate. The accelerated testing is done on a multi poster test rigs on cab and chassis separately. The acceleration history to the multi-poster test rigs is derived from proving ground (torture track) history. The truck cabin is fitted on part of chassis frame along with its suspension for testing. Similarly, the chassis is suspended at its front and rear suspension area. In order to predict the durability by fatigue analysis, the multi axial stress fields are required for the entire load history. The use of multi body dynamics and finite element method makes this task simple andaccurate. The case study of a typical heavy truck (both chassis & cabin) ispresentedwithdetailedsimulationprocedure. 2. MULTI POSTER DURABILITY TESTING & SIMULATION The fatigue strength of Frame is generally assessed through the proving ground (torture track) testing and accelerated tests like four-poster testing. In a four-poster test, the displacementhistoryofthefour hydraulicshakersisfirstdeterminedusingtheframe accelerations determined from the experimental rough road driving, and input accelerations experienced by an actual vehicle in field. In multi poster test, the load history is reduced by reducing non damaging events in order to shorten the test time. This is done through the damage correlation between the rough road driving, torture track test- driving & multi poster test. The typical multi poster test setups are shown in Fig. 1 and 2 Chassis FatigueTestingisacceleratedtestprocedure similar to 4-poster test, which is used for chassis durability. In this testing alongwithZ-directionroad inputs, X and Y (Longitudinal and Lateral) direction inputs, braking torque loads are considered. In case of chassis, the Longitudinal and lateral forces are significant in addition to Z forces. A 22-poster test rig used for 6 x 4 tractor – 49T Tractor - all direction road excitations - braking effects - Cabin and engine excitations to Chassis. - Fifth wheel reactions
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1018 Fig 1- Typical Multi Poster set up Fig 2- Multi Poster Test Rig for Frame Fig 3- Fifth Wheel constraint arrangement The cabin weight, Powertrain weight, fifth wheelloads are applied by actuators with suitable fixtures. The effect of above aggregates in vehicle running condition is simulated. Refer fig. 2 &3 Fig 4 –Power Train arrangement Methodology adopted  Review present conentional system of design optimisation  Identify the aggregates requiring optimisation  Build initial 3 D CAD model of the vehicle aggregates in Pro-e or CATIA software  Do initial Finite Element analysis for the built CAD model with analyiss softwares like hypermesh , NASTRAN  Find out the critical zones or areas related to maximum stress / deflection in order to decide intrumentation points on the physical parts  Identify the referance vehicle model for intrumentation and capturing road load data  Identify the service routes where new model will be subjected to usage for desired target life of product  Intrument the referance vehicle at various locations as identified in the earlierstep withthe help of various devices like straingauging,LVDT, WFT, Accelerometer, RPM meter, Rosette as the requirment of capturing output like strain , displacment , Forces along XYZ, Moments about XYZ for damage analysis,damageeditandcontrol  Do physical running of the instrumented vehicle on identified with the desired payload and application speed , grade and acceleration  Data acquisition by use of data acquisition system like eDAQ plus (SOMAT) which is having 64 Channel analog, 500 Hz sampling rate , GPS channels , Digital inputs  Analysis of the measured data using analysis
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1019 software like ICE-flo GlyphWorks, Plotting amplitude time history , rainflow analysis with respect to number of cycles and rainflow change histogram  Development of correlation with service usage and proven ground (torture track) in order to decide number of cycles for service life usage , Signal processing and damage edit , drive file generation  Kinematic model building in ADAMS based on drive file and extraction of forces  Durability analysis (Virtual simulation)of the3D CAD model Fatigue calculation software like FEMFAT, Design Optimisation usingoptistruck & Hyperstudy Below are below two major steps followed 2.1 Transformation of rig test signals to load time histories at chassis attachment points through ADAMS On- road / torture track testing of vehicle for predefined cycles is the general way to evaluate durability of frame mountings. Performing on- road testing, as number of vehicle variants increases, is time consuming and costly affair. Hence, with the objective to perform vehicle frame durability evaluation at laboratory level and to accelerate testing activity, this full Frame fatigue test evaluation has been planned. Drive files for the rig using the strain, LVDT and WFT data is collected by instrumenting reference vehicle and running on service road. Frame Fatigue analysis test rig set up there is actuators (J1 to J19) are used for giving axle vertical motion, axle longitudinal force, axle lateral force and cab vertical force input. One end of all above-mentioned actuators is connected to rigid structure. Two rubber bush are provide between frame and fifth wheel assembly. Axles are excited through adapter assembly, which are fixed together. Fig 4 – Frame Fatigue test ADAMS Model The test activity is performed in the virtual world throughsimulationsusingADAMSandNastran,FE fatigue. Equivalent ADAMS model is made replicates test setup. This ADAMS multi body simulation is performed giving the displacement input drive file at the four-poster leg locations. The multi body dynamic analysis output is the force history at all the mounting locations on the cab. Dynamics analysis is performed to get the load historyatvariousfrontandrearsuspensionmount locations. Theattachmentpointloadtimehistoriescalculated through ADAMS are then used to calculate fatigue life. These time histories is taken as input for durability simulation 2.2 Durability simulation for fatigue life simulation Fig 5 & 6 shows the flowchart of simulation method used for the prediction of fatigue strength of frame. This method makes use of various CAE solvers like MSC-ADAMS, MSC-NASTRAN & MSC-FATIGUE. The brief description of the process is as given below. First, a finite elementmodel of the Chassis is created using CAD data and then an eigen value analysis is performed using NASTRAN. The results of the eigen value analysis are then converted into an ADAMS’s modal model using ADAMS/FLEX. After this detailed modelling, ADAMS multi body simulation as per earlier process performed giving the displacement input drive file at the four-poster
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1020 leg locations. The multi body dynamic analysis output is the force history at all the mounting locations on the cab. This history is then combined with the NASTRAN’s static unit load inertia relief analysis results to obtainastresshistoryinthecabin for the entire multi poster cycle using linear superposition method. Fig 5 –Chassis Simulation process flowchart Fig 6 –Fatigue analysis process in MSc Fatigue This process of linear superposition method followed by rain flow cycle counting & finding the cumulative damage by Miner’s rule&finallyarriving at fatigue life of cabin isperformedinMSC-FATIGUE. Refer fig.6 for the schematic model of the analysis process. Fig 7- Rear Cross member Gusset Location Fig 8- Engine Mounting cross member location Table 1 shows the detailed durability simulation results for the Chassis. Based on this it’s concluded
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395 -0056 Volume: 03 Issue: 02 | Feb-2016 www.irjet.net p-ISSN: 2395-0072 © 2016, IRJET | Impact Factor value: 4.45 | ISO 9001:2008 Certified Journal | Page 1021 that Chassis is meeting target fatigue life cycles as required TABLE 1 (Durability Simulation Result Summary) 3 CONCLUSION This virtual simulation methodology for durability life prediction can be effectively used at the design stage for evaluating the fatigue durabilitychassisfor eliminating expensive physical prototype testing. A virtual simulation methodology was developed for finding out the vehicle durability, which has a correlation with physical testing in terms of the sequence of failure and locations, and number of cycles. This simulation methodology makes use of input test data, multi-body dynamics & finite element method. This methodology eliminates the use of static assumed service load cases, which do not represent the full dutycycle to which the vehicle will be subjected. This is very effective simulation tool which can be used during design and development of new products reducing overall development time and cost of Design iteration and physical validation. ACKNOWLEDGMENT I would like to express my special thanks of gratitude to my superiors who gave this golden opportunity to do this wonderful project which also helped me in doing lot of Research and I came to know about so many new things.Iamreallythankful to them. Secondly I would also like to thank my family and Friends who helped to complete this project in limited time period. REFERENCES [1] Automotive Structures". SAE Technical Paper950711, 1995. [2] MSC/PATRAN User's Manual, 2005, The MacNeal Schwendler Corporation, Los Angeles, CA, March 2005 [3] Morrow, J. D. Fatigue Design Handbook, Section 3.2, SAE Advances in Engineering,Vol. 4, [4] Society for Automotive Engineers, Warrendale, PA, 1968, pp.21–29. [5]Alex Porter “Accelerated testing and validation” BIOGRAPHIES Mahendra A Petale is working in Leading Automotive Industry. He is leading DesignandDevelopment of future generation commercial vehicles starting from concept to launch. He has wide experience in Key aggregate designs, Product finalization and ValueEngineering.