optimisation in aerospace
TRANSCRIPT
GKN Aerospace Proprietary and Confidential
Optimisation in Aerospace Design Farnborough Airshow 2014
Wilson Wong | 14 July 2014
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GKN Aerospace Proprietary and Confidential
Author
Wilson Wong
Design & Analysis Lead – Additive Manufacturing Centre
Background:
− MEng Aeronautical Engineering, U of Bristol
− Phd Composite Buckling, U of Bristol
− Design / Structural / FEA engineer
− Assystem, Atkins
− GKN Aerospace – Additive Manufacturing Centre
Interests:
− Novel methods on design and analysis
− Exploration of advance D&A techniques
− Incorporating latest IT advancement in the D&A process
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Definition of optimisation
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The act of making something as good as possible
Cambridge dictionary:
“Make the best or most effective use of (a situation or resource)”
Oxford dictionary:
From Latin optimus (best)
What does it really entail?
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We carry out optimisation in different scenarios
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http://jacquesallrich.com/
Online presence optimisation (inc. Search Engine
Optimisation & Social Media Optimisation)
Route optimisation (Travelling
salesman problem)
Task planning / resource optimisation
(Source: http://www.iprod-project.eu/)
Priority identification Process optimisation
Project planning Space optimisation
(Source: CiS)
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Outcome
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http://jacquesallrich.com/
Online presence optimisation (inc. Search Engine
Optimisation & Social Media Optimisation)
Route optimisation (Travelling
salesman problem)
Task planning / resource optimisation
(Source: http://www.iprod-project.eu/)
Priority identification Process optimisation
Project planning Space optimisation
(Source: CiS)
Optimisation
Cost
Performance
Time
Quality
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GKN Aerospace Proprietary and Confidential
Outcome
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http://jacquesallrich.com/
Online presence optimisation (inc. Search Engine
Optimisation & Social Media Optimisation)
Route optimisation (Travelling
salesman problem)
Task planning / resource optimisation
(Source: http://www.iprod-project.eu/)
Priority identification Process optimisation
Project planning Space optimisation
(Source: CiS)
Optimisation
Cost
Performance
Time
Quality
No tooling – Reduce
cost, time
Reduce waste
New design freedom to
increase performance
Rapid response to
modification
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AM and Optimisation – Relationship
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Current State of the Art – 2D/2.5D Structural Optimisation
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Source: Airbus, Altair
Source: Airbus, Technische Universität München
Source: Boeing, Desktop Engineering
Source: Eurocopter, Altair
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Current Examples – 3D Structural Optimisation (Enabled by AM)
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Source: EADS Apworks GmbH, Altair
Source: GE, GrabCAD
Source: EADS Innovation Works, Altair
Source: Airbus, Altair
Source: GE
Source: GKN, Airbus
Source: GKN
Source: Within Lab
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AM Facilitates Optimisation
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With machining
constraints
Without machining
constraints
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Structural Optimisation - Macro
Topology, Size, Shape
Lattice + Skin (Size, Shape)
Concept Refine
Topology
Topography
Free-Size
Size
Shape
Free-Shape
Source: GE, GrabCAD
Source: LimitState
Source: DTI
Source: Within Lab
Source: USTC, DUT, MRA
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Structural Optimisation - Meso
Combine features of topology and lattices
Reduces mass of topology optimised structure
further
Provide robustness of features in topology
optimised structure
Source: DTI, Compolight Source: Altair
Source: Delta 7
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Structural Optimisation - Micro
Mimic nature (bio-mimetic), e.g. bone
Design material at micro scale to cater for properties required
Source: HRL Laboratories LLC
Source: MIT, LLNT
Source: BBC, 3ders.org
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Optimisation Unleashes Potential of AM
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With machining
constraints
Without machining
constraints
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Challenges
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Design More
integrated/easy modelling
software required
Software to handle
exponential amount of geometries
Analysis New analysis methods needed
Significantly better solver capability
Manufacturing Speed Reliability
Inspection New techniques required
Post processing
New techniques required
Testing New test
methodology needed
Culture change
•P
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•M
ind
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•D
eve
lop
ment o
f n
ew
me
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•IT
ba
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one to
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ort
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Development Process Flow
Conventional
Future
Concept Detail DesignDetail Analysis (Stress, F&DT)
Final DesignCustomer
Requirements
Global
Local Customer
Requirements Optimisation
Design
Analysis
Concept
Detail Design
Detail Analysis (Stress, F&DT)
Final Design
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Current
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CFD optimisation Configuration optimisation Topology optimisation
Source: GE, GrabCAD
Multi-physics optimisation
Source: RR Source: Airbus, Altair
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Different aspects of aircraft design
Source: McGill University
Source: Linflow
Source: Technishe Universitat
Braunschweig
Source: MOOG, NI
Source: ANSYS Source: MSC
Source: Antonio Silva
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GOAL - Holistic optimisation
MDO for Aircraft Configurations with High-fidelity (MACH)
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GOAL - Holistic optimisation
Multi-level of details
•Top level approximate system modelling
•Low level detail modelling
Accessible to every stakeholder
•Bidding team
•Detail analyst
Allow quick what-if scenarios at any time offline
•Impact analysis on changes
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Challenges
Big data – data management
Computing power
Physics coupling complex
Different software platforms
Paradigm shift in mindset, culture, working
procedures
Barriers
Specialist software
Very specific technical skills needed
Much greater complexity of problems
Steep learning curve
Embedded culture
Why are we not using global optimisation more?
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Possible solutions
Analytics method
− Multivariate analysis
− Design of Experiment
− Design Structural Matrix
− Parallel Coordinate
HPC, distributed computing, Cloud
Multi-scale analysis
Custom code to interconnect different platforms
Simplistic software for quick approximate answer
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Source: EnterpriseTech Cloud Edition
Source: NASA
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In Brief
AM Optimisation
What is optimisation
Emphasis on structural optimisation (Now & Future)
Challenges ahead for implementing future structural optimisation
Importance of culture
Local & Global optimisation
Challenges on global optimisation
Quick peek to future
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Future & Questions
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Source: Altair
Source: Emerging Objects
Source: EDAG, 3ders Source: Aerojet Rocketdyne
Source: Airbus
Source: Concept Laser
Source: MIT
Source: Dame Zaha Hadid
Source: Henri Freiherr von Freyberg