© Rolls-Royce plc 2009The information in this document is the property of Rolls-Royce plc and may not be copied or communicated to a third party, or used for any purpose other than that for which it is supplied without the express written consent of Rolls-Royce plc.This information is given in good faith based upon the latest information available to Rolls-Royce plc, no warranty or representation is given concerning such information, which must not be taken as establishing any contractual or other commitment binding upon Rolls-Royce plc or any of its subsidiary or associated companies.Published by NATO Research and Technology Organization (RTA) with permission
Lecture Series AVT-167
Case Study 3: ComponentsHigh Pressure Compressor and Turbine Disk, Structural Casings
A. Karl, Rolls-Royce
NATO/PFP
2
October 2009
Outline
5 steps for Robust DesignBasic approach for automated DesignExamplesSummaryQuestions
NATO/PFP
3
October 2009
Design for Six Sigma Toolset
Integrated Frameworks
5 steps to achieve Robust Design Automate Process
execute design / analysis process without human interaction Process Integration
build up of integrated processes between various disciplines Design Exploration
getting an understanding of the design space characteristic Optimisation
achieve the best compromise regarding all requirements Robust Design
make sure that the design performs for variable conditions
NATO/PFP
4
October 2009
Basic Process
NATO/PFP
5
October 2009
Integrated Frameworks
Enable the linking of simulation tools to Achieve a considerable speed-up of the simulation task Achieve multidisciplinary processes across teams and business units Achieve a standardisation of the used simulation processes
NATO/PFP
6
October 2009
Examples – Component Level
Turbine Blade – Disc attachmentTurbine Disc life assessmentEffect of Manufacturing tolerances on
compressor discsRobustness Assessment of a structural
casing
NATO/PFP
7
October 2009
Blade – Disc connection example: Process Definition
integrated process
Geometry model
Analysis model 2
Analysis model 1
NATO/PFP
8
October 2009
Blade – Disc connection example: Results of Optimisation
Pareto front (best possible combinations)
manual optimisation
improvement possibilities
Criteria 1
Crit
eria
2
NATO/PFP
9
October 2009
Turbine Disc Life Prediction:Variability Assessment and Weight Reduction
heat transfer/ nominal heat transfer
Dia
phra
gmLi
fe/N
omin
alD
iaph
ragm
Life
1 1.25 1.5 1.75 20.5
0.6
0.7
0.8
0.9
1
1.1
1.2
1.3
1.4
1.5
Variability assessmentfor disc life
Disc weight minimisation
NATO/PFP
10
October 2009
Compressor Disc Design:Monte Carlo Simulation
Manufacturing tolerances are transformed into
Mass variability Movement variability Stress variability Etc.
Proper assessment of the design becomes possible
MCS using ResponseSurface Methods
NATO/PFP
11
October 2009
Structural Casing example: Process Definition
STEP Translator
STEP File
Cost ModelsUnit Cost
FE AnalysisLifing Parameter
Process IntegrationDesign Parameters & Tolerances
Boundary Conditions
Check Objectives to
Exit Loop
GeometryCreation
Analysis Model
Part File
Part Parameter & Expressions
Derived Manufacturing
Parameters
Design Parameters
Manufacturing
Scrap & Rework Cost
Manufacture Cost
Process Capability
NATO/PFP
12
October 2009
Structural Casing example: Robustness Results
NATO/PFP
13
October 2009
SummarySeveral examples have shown the
benefit of using automated design approaches
Important info can be gained by these methods making the design decisions more focused
Using the info from the automated design approaches the risk in the execution of development programs for complex systems can be reduced
NATO/PFP
14
October 2009