Powertrain Applications

OptiStruct provides industry-leading capabilities and solutions for Powertrain applications. This section aims to highlight OptiStruct features for various applications in the Powertrain industry. Each section consists of a short introduction, followed by the typical Objectives in the field for the corresponding analysis type.

Additionally, the typical Inputs, Outputs and Key Features are highlighted to allow for a deeper understanding of the features in an application-oriented layout. Links to Examples and Tutorials are provided, which allow you to download the models and setup in HyperMesh or just directly run in OptiStruct and analyze the results.


Figure 1. Engine Block Stress Post-processing Example

This document will allow you to understand OptiStruct solution sequences in an application-oriented approach, and effectively try to bridge the gap between powerful powertrain solutions and their adaptation within the industry.

The detailed solution-specific information is available in the corresponding User Guide pages. Here you will look at application-specific information for Powertrain.

Nonlinear Steady-State Heat Transfer Analysis

Nonlinear Steady-State Heat Transfer on the engine block made of the cylinder head, valve guides, valve seats, valves, cylinder head screws, cylinder block, bearing caps, and bedplate.

Theory

Calculate the temperatures in the engine block for subsequent durability analysis.

Best Practices

SimLab can be used to map temperatures and HTC that result from a CFD/combustion analysis onto the mesh used for the Nonlinear Steady-State Heat Transfer Analysis.

Input

Loads and boundary conditions are:
  • Temperatures and HTC in the water-jacket that result from a CFD analysis
  • Temperatures and HTC in the cylinders that can result from a combustion analysis


Figure 2. Boundary Conditions in the Cylinders

Output

Temperatures in the engine block.


Figure 3. Temperature Results

Thermal Fluid Structure Interaction

Thermal Fluid Structure Interaction Analysis on the engine block made of the cylinder head, valve guides, valve seats, valves, cylinder block, bearing caps and bedplate.



Figure 4. Domain Information

Theory

Evaluate temperatures in the engine block by considering the coupling effect with the fluid domain. These temperatures could then be used as inputs during a subsequent durability analysis.

Calculate pressure drop and the flow uniformity in the fluid domain, i.e. the water jacket.

Input

Initial conditions and boundary conditions for the fluid domain.

Temperatures and HTC in the cylinders that can result from a combustion analysis.
Note: Temperatures and flux at the interface between the fluid and the structural domain are managed automatically by AcuSolve and OptiStruct.

Output

Temperatures in the water jacket and the engine block.


Figure 5. Temperature Results in the Water Jacket and Engine Block

Pressure drop and the flow uniformity in the fluid domain.

Coupled Thermal Structure Analysis

Contact based thermal analysis on the engine block made of the cylinder head, valve guides, valve seats, valves, gasket, cylinder head screws, cylinder block, bearing caps and bedplate. In this model, all parts are in sliding contact or tied contact.

Theory

Evaluate temperatures in the engine block by considering the effect of the contact clearance/pressure on the conductivity. These temperatures could then be used as inputs during a subsequent durability analysis.

Sequence of Subcases:

Nonlinear static analysis where pretensions are applied in the cylinder head screws. The aim of this subcase is to put all the parts in contact and then model the assembly of the engine block with the ambient temperature.

Contact-based Thermal Analysis where the conductance depends on the contact pressure/clearance. In this subcase the cylinder head bolt pretensions are locked. The objective of this subcase is to model the assembly of the engine blocks with “hot” conditions.

Best Practices

As contact pressure and conductance will influence the heat transfer solution it is important to model the contact between the gasket and the surrounding parts properly. SimLab has many specific tools dedicated to gasket modeling that can help here. For more information, refer to the gasket tools available from the Advanced menu of SimLab.


Figure 6. Coincident Mesh

In Figure 6, the gasket mesh have been imprinted onto the mesh of the cylinder head with SimLab to have coincident mesh between these two parts. This has been done to have a better contact modeling in this area.

Input

  • Pretension in the cylinder head screws
  • Clearance and pressure based conductance values


    Figure 7. Thermal Conductance Based on Contact Clearance and Pressure
  • Temperatures and HTC in the water-jacket that result from a CFD analysis
  • Temperatures and HTC in the cylinders that can result from a combustion analysis

Output

Temperatures in the engine block.


Figure 8. Contact Pressure Results

Nonlinear Static Analysis

Nonlinear Static Analysis with small deformation and with/without thermal loads. This kind of analysis can be run on most of the PWT components.

Theory

Predict stresses in almost all the PWT components.
Distortions
Bore distortions, bearings out-of-round
Contact Pressures
Gasket pressure for sealing
Relative Displacements
Openings between the two gearbox cases to estimate the sealing, relative sliding between the engine mount and the engine block.

Best Practices

For bore deformation use regular mesh to mesh the cylinders (so called R-tria mesh in HyperMesh and isomesh in SimLab).


Figure 9.
To calculate bore deformation in a cylinder, add a cylinder coordinate system.


Figure 10. Meshing and Coordinate System

Use the domain decomposition method to reduce time for calculation, especially for the largest models like the model used to calculate bore deformation.

Imprint functionalities available in SimLab can be used to have coincident meshes in contact areas.

Input

Models can involve Thermal loads. In this case, thermal loads that can be constant per components or they may also result from a heat transfer analysis.

Static loads such as the pretension loads, the pressures in the combustion chamber, loads applied on the crankshaft or the bearings that result from a MBD analysis.
  • Bolt pretensioning
  • N2S and S2S contacts with contact options such as CLEARANCE, ADJUST, SMOOTH
  • Gasket material
  • Plastic material
  • Continue nonlinear solution sequence from a preceding nonlinear subcase (CNTNLSUB)
  • Nonlinear Expert System (PARAM,EXPERTNL,YES)
  • Restart of Nonlinear Analysis Bore deformation

Output

Stresses, Bore distortions, and Contact Pressures


Figure 11. Gasket Pressure Results

Fatigue Analysis

Theory

Predict life of most of PWT components. Depending on the components different approaches are used.
  • Low Cycle Fatigue Analysis (E-N)

    Cylinder Head

  • High Cycle Fatigue Analysis (S-N)

    Engine block, especially the water jacket of the cylinder head, cylinder block, bedplate and bearing caps.

    Rotating parts, like the connecting rods and crankshaft.

  • Infinite Life (Dang Van)

    Engine block, especially the water jacket of the cylinder head, the cylinder block, bedplate and bearing caps.

    Rotating parts, like the connecting rods and crankshaft.

    Engine mounts.

    Gearbox cases.

Best Practices

Use the domain decomposition method to reduce the calculation time for the biggest models.

Fatigue results are only available at element centers. To have results on the external faces of solid components, add shell elements by extracting external faces of these components and calculate fatigue on these shell elements.

In OptiStruct different element types can be mixed with TIED contact. In Figure 12 used to calculate fatigue in the fillets of the crankshaft, the fillets have been meshed with HEXA elements to capture stress more precisely while the rest of the part has been meshed with TETRA elements. The connection between this two element types is made with TIED contact.


Figure 12. Connection between HEXA and TETRA Elements Made with TIE Contact

Input

Models can involve Thermal loads. In this case, thermal loads that can be constant per components or they may also result from a heat transfer analysis.

Static loads such as the pretension loads, the pressures in the combustion chamber, loads applied on the crankshaft or the bearings that result from a MBD analysis.

Output

  • Fatigue Damage and Life
  • FOS


    Figure 13. von Mises Stress Results

Noise Vibration and Harshness (NVH) Analysis

Theory

Predict response to modal analysis and frequency-dependent loading of most of PWT components. Depending on the components different approaches are used. Includes Radiated Sound and Equivalent Radiated Power Analysis.

Models with different levels of complexity can be used for NVH analysis:
  • Single parts or sub-systems

    The engine trunk made of the cylinder-head, cylinder block, bedplate and gearbox.

    The whole PWT model, as in the engine trunk and all the accessories.

  • In these models assemblies can be done through

    Bolts modeled with 1D elements.

    Bolts modeled with 1D or 3D elements and pretension sections in order to run a prestressed analysis. In this case a Nonlinear Static Analysis has to be performed prior to the NVH analysis.

    Sliding contact in order to run a prestressed analysis. In this case a Nonlinear Static Analysis has to be performed prior to the NVH Analysis.

    Freeze or Tied contacts

  • Typical NVH Analysis that can be performed with OptiStruct

    Superelement Generation

    Normal Modes

    FR analysis

    ERP and Radiated Sound Analysis

Best Practices

Use AMSES for large models and/or the number of modes to extract is significant.

Use the domain decomposition method to extract modes with the Lanczos solver on large models.

Input

  • Dynamic reduction with CMSMETH
  • AMSES
  • FASTFR
  • Radiated Sound analysis and ERP
  • Prestressed normal modes analysis

Output



Figure 14. Influence of Frequency on Prestressed Results

Coupling OptiStruct with Third Party Solvers

Theory

OptiStruct can be coupled with a variety of third-party solvers. Here is a quick review of Powertrain-based coupling availability. For detailed information, refer to Create Output for Third Party Software.

Fatigue analysis with FEMFAT, Design Life, FE-Fatigue and FE-SAFE.

Creating the condensed CMS Superelement information for AVL/EXCITE, SIMPACK, ROMAX, ADAMS, Ricardo and Virtual Lab.

Residual run after running AVL EXCITE to recover displacement, velocity, acceleration, ERP, stress, and strain results for interior grids and elements in the CMS Superelement based on the modal participation results from AVL/EXCITE.

Topology Optimization on a Cylinder Block with Bore Distortion Responses

Design space on the external faces of the cylinder block to add ribs.

Setup

Minimize the mass of the cylinder block, bore distortion constraints.

Or,

Minimize bore distortions, constraint on the mass of the cylinder block.

Input

Models can involve Thermal loads. In this case, thermal loads that can be constant per components or they may also result from a heat transfer analysis.

Static loads such as the pretension loads, the pressures in the combustion chamber, loads applied on the crankshaft or the bearings that result from a MBD analysis.

Topology Optimization of the Bedplate

Design space inside and outside the bedplate.

Setup

Minimize the mass of the bedplate, stress constraints and Eigen-frequency constraints.

Input

Models can involve Thermal loads. In this case, thermal loads that can be constant per components or they may also result from a heat transfer analysis.

Static loads such as the pretension loads, the pressures in the combustion chamber, loads applied on the crankshaft or the bearings that result from a MBD analysis.

Output

To run this kind of optimization problem, two different models have to be used with the MMO feature:
  1. One for Nonlinear static analysis.
  2. One for NVH analysis.

Topology Optimization of the Gearbox Housings

Design space on the external faces of the gearbox housings to add ribs there.

Setup

Minimize the mass of the gearbox, bearings misalignment, engine mount dynamic stiffness, and Eigen-frequency constraints.

Input

Models can involve Thermal loads. In this case, thermal loads that can be constant per components or they may also result from a heat transfer analysis.

Static loads such as the pretension loads, the pressures in the combustion chamber, loads applied on the crankshaft or the bearings that result from a MBD analysis.

Output

To run this kind of optimization problem, two different models have to be used with the MMO feature:
  1. One for Nonlinear static analysis.
  2. One for NVH analysis.

Shape Optimization on a Cylinder Block with Bore Distortion Responses

Shape or Free Shape variables to modify the geometry of the water jacket.

Setup

Minimize the mass of the cylinder block, bore distortion constraints.

Or,

Minimize bore distortions, constraint on the mass of the cylinder block.

Input

Models can involve Thermal loads. In this case, thermal loads that can be constant per components or they may also result from a heat transfer analysis.

Static loads such as the pretension loads, the pressures in the combustion chamber, loads applied on the crankshaft or the bearings that result from a MBD analysis.

Shape Optimization on a Cylinder Head with Fatigue Responses

Shape or Free Shape variables to modify the geometry of the water jacket.

Setup

Minimize the mass of the cylinder block, constraints on Life or Damage (HCF).

Or,

Maximize Life or Minimize Damage, constraint on the mass of the cylinder block.

Input

Models can involve Thermal loads. In this case, thermal loads that can be constant per components or they may also result from a heat transfer analysis.

Static loads such as the pretension loads, the pressures in the combustion chamber, loads applied on the crankshaft or the bearings that result from a MBD analysis.

Shape Optimization of the Connecting Rod with Fatigue, Contact Pressure and Out-of-Round Responses

Shape or Free Shape variables to modify the geometry of the connecting rod.

Setup

Minimize the mass of the connecting rod.

Constraints on responses:
  • Life of Damage (HCF)
  • Out-of-round of bearings
  • Contact pressure

Input

Models can involve Thermal loads. In this case, thermal loads that can be constant per components or they may also result from a heat transfer analysis.

Static loads such as the pretension loads, the pressures in the combustion chamber, loads applied on the crankshaft or the bearings that result from a MBD analysis.

Topography Optimization of Heat Shields with Frequency and/or ERP Constraints

Topography variables to reinforce the heat shield.

Setup

Minimize ERP, constraint on eigen-frequencies.

Input

Models can involve Thermal loads. In this case, thermal loads that can be constant per components or they may also result from a heat transfer analysis.

Static loads such as the pretension loads, the pressures in the combustion chamber, loads applied on the crankshaft or the bearings that result from a MBD analysis.