Perspective on Aero Propulsion Needs for Micro-Nano-Technologies Robert Schafrik GE Aircraft Engines...
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Transcript of Perspective on Aero Propulsion Needs for Micro-Nano-Technologies Robert Schafrik GE Aircraft Engines...
Perspective on
Aero Propulsion Needs for
Micro-Nano-Technologies
Robert SchafrikGE Aircraft Engines
Presented at:
CANEUS 20042 November 2004
Monterey, CA
2 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Overview
Context & Drivers for Innovation
New Product Introduction (NPI) Process
Potential MNT Applications in Jet Engines
Summary & Take Aways
Context & Drivers for Innovation
4 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Drivers for Innovation
Improve Customer Value
Performance
Reliability
Cost of ownership
Mitigation Strategies for Implementation Risk
Technical, Schedule, Cost
5 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Performance Improvement
1956 1958 1961 1962 1968 1974 1981 1986 1992 1992 19960.00
1.00
2.00
3.00
4.00
5.00
6.00
7.00
8.00
9.00
Th
rust
-to
-Wei
gh
t
1956 1958 1961 1962 1968 1974 1981 1986 1992 1992 1996
Year
J57
J79
J85
J58
F10
0
TF
34
F40
4
F11
0-10
0
F11
0-12
9
F10
0-22
9
M88
Ref: Aviation Week
6 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Conceptual Cycles and Temperatures
Cruise
ClimbSupersonic
(Future)Supersonic
(Future)
Time
T41 Land
Take-off
Existing Sub-sonicExisting Sub-sonic
Cruise
Climb
7 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Engine Departure Rate
99.0
99.2
99.4
99.6
99.8
100.0J
an
-88
Ja
n-8
9
Ja
n-9
0
Ja
n-9
1
Ja
n-9
2
Ja
n-9
3
Ja
n-9
4
Ja
n-9
5
Ja
n-9
6
Ja
n-9
7
Ja
n-9
8
Ja
n-9
9
Rat
e
99.97%
8 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Pro
cess
Co
ntr
ol &
ND
E
Improved Engine Materials
NewNewMaterialMaterial
Mat
eria
l Co
mp
osi
tio
n &
Str
uct
ure
Pro
ces
sin
g
Introducing a New Material RequiresMuch More Than Material Development
9 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Interplay of Process and Material Development
Titanium
Stainless Steel
Cobalt
Nickel Superalloys
Polymer Matrix Composites
Thermal Barrier Coatings
Vacuum Induction Melting
Arc Melting
Investment Casting of Complex Shapes
Powder Metal Superalloys
Turbine Coatings
TIM
E
Directionally Solidified and Single Crystal Airfoils
Multiple Vacuum Melting Cycles
Intermetallics
Ceramic Matrix Composites
1950
s19
60s
1970
s19
80s
1990
s20
00s
EB-PVD
Large Structural Castings
Iso-Thermal Forging
SiC Melt Infiltration
Laser Deposition
MNT Materials
10 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Typical Development Times for a New Material
I. Modification of an existing material for a non-critical component Approximately 2-3 years
II. Modification of an existing material for a critical structural component Up to 4 years
III. New material within a system that we already have experience Up to 10 years
• Includes time to define the chemistry and the processing details
IV. New material class Up to 20 years, and beyond
• Includes the time to • Develop design practices that fully exploit the performance of the
material
• Establish a viable industrial base
GRAND CHALLENGEDrastically Reduce Development Times for New Materials
…Without Reducing Application Risk!
11 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Competing Implementation Pressures
New Materials Development
Business NeedRisk
Development Cost Technical Maturity
Business Need Is Driven by Customer Needs and by Competitive Market Forces
Higher efficiency, higher performance, lower cost are important within this context
The Business Process Is Iterative
Adapt to changing conditions and requirements
Constancy of funding to full maturity is seldom available
12 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Dilemmas
A Designer Is Reluctant to Select a New Material Until it is Evaluated in Service
BUT a New Material Cannot be Evaluated in Service Until a Designer Selects it
New Materials Will Not Gain Market Acceptance Before their Costs Decrease
BUT Costs Will Not Decrease Until the Material Gains Market Acceptance
Ref: Arden Bement, Purdue Univ, at National Materials Advisory Board Forum, Feb 2000, Washington, DC
13 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Past Materials Transition Approach
Customer for Materials Development: Materials & Processes (M&P) Organization
Push technology
Tendency to over-sell what a new material will do
Development Approach
Empirical and heuristic-based
Lots of characterization
In actuality, can’t test everything
Bottomline: Required Many, Many Trials Over Many Years
14 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Development Sequence (PAST)
Development Iterations
Make It Test It
Improve It Test It
Cost Reduce It Test It
Materials Development
Idea and Initial Feasibility
Design Practice
Real Component Application
Production Scale-Up
Committed Component Application
15 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Today’s Materials Transition
Customer: Systems Engineering
Set top level requirements
M&P determines specific materials requirements
Development Approach
Beginning to apply M&P modeling and simulation
Use fundamental knowledge to develop models that predict behavior beyond current experience base
Fewer and more focused iterations
Disciplined Design-of-Experiments
16 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Development Sequence (CURRENT)
Development Iterations
Design It Analyze It
Make It Test It
Optimize & Cost Reduce It Test It
Materials Development
Design Practice
Production Scale-Up
Integrated Teams Guided by a Disciplined
Development Process
Manufacturing
17 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Vision for the Future
Customer: Systems Engineering
Materials Development Team integral member of the Systems Engineering Team
Materials development cycle matches design cycle
Perform design study trade-offs with estimated properties
Evolve design practices in parallel with materials development
Development Approach
Fully exploit Materials Modeling and Simulation
Accurately estimate properties with Modeling and Focused Testing
Understand sources of variation
18 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Development Sequence (FUTURE)
Single Development Iteration
Optimized Analysis Validate It
Materials Development
Design Practice
Production Scale-Up
Integrated Teams Guided by a Disciplined
Development Process
Manufacturing
Integrated, Seamless Computational Environment
Across all Disciplines & Objectives
New Product Introduction (NPI) Process
20 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Feasibility Demonstration MaturationTTG3 TTG6 TTG9
Feasibility Demonstration MaturationTG3 TG6 TG9
Product Creation
Initial evaluation-lab scale
Estimates of key characteristics
Sub-scale demonstration
Components
produced to prelim specs
Production windows estim
Process capability fully established -Production specifications in place -Supply chain established
All necessary property data obtained
Computer simulations, sub-scale testing of concepts
Performance estimates made
Full scale testing
Product performnce validated
Technologies at maturation.
Production components designed
Product engines certified
Products enter service
Development StagesProducts launched when
technologies are mature
TOLLGATE
KEY REVIEW
STAGE 0:PREPLANNING
Identify TeamLeader andChampion 0-2
Define InitialScope of theProgram 0-3
EstablishBusiness Need
0-1
Review ScopingPlan with theCustomer 0-4
Select andAssembleCore Team 0-5
STAGE 1:MATERIAL/PROCESSFEASIBILITY
Review Planwith Customerand CommitFunding 1-4
ResearchPrior Work
1-5
Formulate theDetailed Plan
1-3
Conduct Basicor AppliedResearch 1-6
IdentifyCandidateMaterials/Processes 1-7
DefineProgramObjectives 1-1
Define andQuantifySuccess 1-2
EstablishMaterial/ProcessFeasibility 1-8
PLAN
DO
CHECK
Get Feedback,Measure Success andCompare to CustomerRequirements 1-9
Identify andCompileLessonsLearned 1-10
CommunicateLessonsLearned 1-11
DefineFollow-onWork 1-12
DocumentResults 1-13
ACT
STAGE 2:MATERIAL/PROCESSDEMONSTRATION
Review Planwith Customerand CommitFunding 2-4
SelectCandidateSolutions 2-5
Formulate theDetailed Plan
2-3
EvaluateCandidateSolution 2-6
Select theApproach
2-7
DefineProgramObjectives 2-1
Define andQuantifySuccess 2-2
Establish FundamentalMaterial/ProcessUnderstanding andControl Strategy 2-8
PLAN
DO
DemonstrateMaterial/Process andControl 2-9
CHECK
Get Feedback,Measure Success andCompare to CustomerRequirements 2-10
Identify andCompileLessonsLearned 2-11
CommunicateLessonsLearned 2-12
DefineFollow-onWork 2-13
DocumentResults 2-14
ACT
STAGE 3:PILOT ORPRODUCTIONSCALE-UP
Review Planwith Customerand CommitFunding 3-4
Formulate theDetailed Plan
3-3
DefineProgramObjectives 3-1
Define andQuantifySuccess 3-2
PLAN
DefineProductionScale-up Issues 3-5
AddressProductionScale-up Issues 3-6
Define andDocument theProcess and ControlMethods 3-7
DOTransition andTrain
3-8
CHECK
Get Feedback,Measure Success andCompare to CustomerRequirements 3-11
Pilot orProductionDemonstrationRun 3-10
ApproveProductionProcess (SSE) 3-9
Release toProduction
3-12
Identify andCompileLessonsLearned 3-13
CommunicateLessonsLearned 3-14
DefineFollow-onWork 3-15
DocumentResults
3-16
ACT
1
2
3
4 5
6
7
8 9 10
Material/Process Development Cycle
Potential MNT Applications
in Jet Engines
23 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Important Material Characteristics
Thermal and Mechanical Stability Maintain desirable micro/nano features during processing
and in-service use
Meet all Mechanical Property Requirements Understand variation Specific requirements depend on the application
Price & Life Cycle Cost Customer Value
Ability to Scale-up for Actual Components Production capacity
Need High Reliability & Availability at Production Rates
24 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Potential Applications in Jet Engines
Nano-structured Coatings
Achieve desired balance of properties that previously were not obtainable
Wear resistant, lubricious coatings
Damping with no substrate debit
Environmental protection coatings with no substrate debit
Polymer Matrix Composites
Enhanced mechanical properties with micro-nano-particles
Carbon nanotubes & clay nano-particles
• Challenges with dispersion, texturing/orientation, bonding to the
matrix, reproducibility of properties, cost, availability
In-situ chem formation (self-assembly) of micro-nano-sized structures
Adhesives important as well
25 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Potential Applications in Jet Engines
Intelligent Materials and Structures
Micro-sensors and actuators
Shape changing polymer matrix composite structure
Structural health and monitoring systems
Challenges with system architecture, feasibility, durability in
severe environmental conditions, etc.
Functional Materials
Novel nano-engineered soft magnetic materials
Permanent magnets for light weight electric motors,
actuators, magnetic bearings
26 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Potential Applications in Jet Engines Monolithic Ceramics
Fine grained silicon nitride for hybrid bearings
Use in applications in which bearings are highly loaded under
severe operating conditions
Challenges with synthesis and consolidation
Metals
Nanophase aluminum alloys with increased strength and toughness
Challenges include synthesis and consolidation, balance of
properties, environmental resistance
Modeling and Simulation of M-N-Materials
Predict properties for different scale lengths
Estimate long time performance in service environment
Optimize materials to achieve desired properties
Summary & Take Aways
28 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Summary
Transition of new materials technology can take considerable time Difficult to “push” materials technology into applications Must understand and mitigate risks
Little experience base for nano materials
Structural applications have the longest development time Consequence of failure is high Nano coatings and functional materials more attractive for early
introduction
Must continue to develop and implement materials modeling and simulation tools
Perhaps only realistic way to reduce number of iterations and long, drawn out time sequence
Goal: Gain “experience” through high fidelity simulations
29 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Sprague’s Law
The first information you hear about a new material is
usually the best thing you’ll ever hear about it
Basis
Initial claims based on scant property data
Early data generated from laboratory quantities
Little consideration given to effects of processing
variations
Lack of understanding that defects ultimately control
usable properties
30 Perspective on AeroPropulsion Needs for MCTCaneus 2004, Nov 2, 2004
Take Aways New material should have a significant performance advantage to
displace existing material
Enthusiasm for CNT high…developing most appropriate applications will take further significant effort
CNT has the potential to impact nearly every component in the engine
Focus on highest impact applications to gain acceptance and experience
Transition of CMT is following conventional long drawn-out process for many applications
R&D needs include the following areas:
Modeling of materials behavior at nano length scales for high fidelity simulations of service performance
Manufacturing methods, including synthesis and consolidation