additive manufacturing at ge aviation · 2012-09-28 · • rapid tooling for production and...
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Additive Manufacturing at GE Aviation
TRAM 2012 Chicago, Il
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ADDITIVE MANUFACTURING (AM),
n – process of joining materials to make objects from 3D model data, usually layer upon layer, as opposed to subtractive manufacturing methodologies.
Synonyms: additive fabrication, additive processes, additive techniques, additive layer manufacturing, layer manufacturing and freeform fabrication
*ASTM E2792-009 Standard Terminology for Additive Manufacturing Technologies
LENS Process, Sandia National Labs
Definition:
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Benefits of Additive Manufacturing
•Reduced time to market
•Reduced manufacturing leadtimes and costs
•Improved buy:fly
•Enabling design capabilities
•Novel/Hybrid materials
•Weight reduction
•Sustainability
• Separate efforts initially.
• Typical AM applications:
• Plastic and metal models for design
validation.
• Rapid tooling for production and
inspection.
• Rig testing and engine testing.
• Now coordinating amongst the divisions
through our GE Global Research
Center.
• At Aviation:
• Low rate initial production 2015.
Across the corporation… Aviation
Appliances
Healthcare
Energy
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Fan
Metal Leading Edge
Blisk
Structures
Compressor case
Combustion case
HPT case
LPT case
Combustion
Liners
Fuel nozzles
HPT/LPT
Blades
Vanes
Shrouds
Installations
VSV bushing
Heat shield
Tubes & brackets
Assemblies
Booster/Compressor
Blades
Vane Segments
Candidate AM Applications for Aviation
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Advanced
Technology
Enhanced
Technology
Additive Manufacturing Maturation
Basic
Technology
• Limited Supplier Base
• Internal Standards vs. Industry
Specifications
• Limited Design Methodologies
• Metals
•Productivity Enhancements
•Design Allowables (mechanical
property database)
•Increased Build Volume
•Process Monitoring and Control
•Enabling Design Paradigm
•Topology Optimization
•Complete design freedom
•Polymer Composites
$$ $$$$ $$$$$$
•Autonomous Processes
•Novel Materials
•Adaptive Process Control
•Process Intelligence
•Hybrid Materials
•Rapid Qualification
•Ceramic/Nano Composites
Start
Technolo
gy D
evelo
pm
ent
10 years
10 years 20 years
2013 2015 2005
MRL 6 MRL 0 MRL 9 MRL 3
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Additive Manufacturing Methods
By Heat Source
Additive Mfg
Whole Features
Welding
Inertia, Flash,
Stud, other…
Layering Processes
By Methodology
Laser Electron Beam
(EB)
Plasma
Transfer Arc
(PTA)
Gas Tungsten
Arc
(GTA)
Powder
Feed Powder
Bed
Wire
Feed
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Direct Metal Additive Processes
Material -Feed Powder-Bed
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Material-Feed
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20+ years and going strong
•Production for surface
enhancement
•New-make Repair
• MRO
Parts flying today.
Laser and Electron Beam Additive Manufacturing
Powder and Wire Feed Processes
•Feature and whole part
•Simple geometry
•High dep rate
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Making the Business Case
• Many structural parts evaluated for AM in terms of cost savings.
• No cost benefit found
• Material savings offset by processing costs and additional post processing steps: Straightening
Heat treat
Inspection
• Potential carbon tax benefit.
Machining Fact:
•Average Buy:Fly = 8:1
•87% of raw material ends up as chips on the floor.
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Powder Bed
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Direct Metal Laser Melting (DMLM)
Part
Laser Beam
Powder
Leveler
Laser Window
Shield
Gas
Powder
Collector
Powder
bed
Build Platform
DMLM Part
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Direct Metal Additive Properties
Better than cast, approaching wrought.
Tensile
Fatigue
Cast
Spec
Min Cast
Wrought
Spec
Min
3 DMLM
1
2 4 5 6
Wrought
Bulk material properties.
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Major Gaps and Challenges
•Rapid Qualification
•NDI
•Materials Database
•Specifications
•Supply Chain
•Design Rules
General Process Specific
•Surface Finish
•Process Speed
•Distortion
•Build Volume
•Applicable Materials
•Process Monitoring and Control
DMLM Fact:
• Melt pool is 0.003” wide and traveling at 1 yard/sec
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Poor Surface Finish and Subsurface Porosity Reduce Life…
LCF
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Throughput - Simple Case Study P
art
Num
ber
Type
Layer
Spacin
g
(um
)
Quantity
/Build
Build
Tim
e (
hrs
)
Build
Cost
($/P
art
)
Quantity
/Build
Build
Tim
e (
hrs
)
Part
Build
Tim
e
(hrs
/part
)
Build
Cost
($/P
art
)
First P
art
Cost
($)
100th
Part
Cost
($)
2152M85 Casting 20 1 8.5 1.04 9 36 4.0 0.49 1 0.16
40 1 4.3 0.53 9 18 2.0 0.24
5151T61 Casting 20 1 10 0.52 12 50 4.2 0.22 1 0.07
40 1 5 0.26 12 25 2.1 0.11
ER4024 20 1 20 0.27 9 50 5.6 0.07 1 0.02
40 1 10 0.13 9 25 2.8 0.04
DMLM Single-Part
Build
DMLM Nested Build Conventional
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Higher laser power…
Cost Reduction Through Increased Throughput…
Dual
laser/scanhead.
…higher throughput.
Courtesy SLM-Solutions GmbH
2X improvement
without having to
requalify process or
material.
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Reduced part count.
Reduced number of braze cycles.
Reduced number of welds.
Cost Reduction Through Consolidation
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Distortion -> Stress Management Iterations increase leadtime and cost.
Mitigation strategies add time and cost.
Very repeatable.
Predictable?
Where to next?
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Lightweight Structures
Composites
MMC, PMC, CMC
Lattice Structures
• Recent study
indicates that over
90% of energy
footprint of an aero
engine part comes
from use in service.
Topology Optimization
Courtesy Within Technologies Ltd
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Status of Additive Mfg GE Aviation
• AM metal components are bill-of-material for advanced engine programs.
• Base of applications is expanding as technology is excepted and exploited by design engineers.
• Major issues remain in terms
of surface finish, dimensional tolerances and throughput (and more).
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Near-term Needs
• Proven, robust manufacturing processes (FTY=1)
• Healthy supply chain
• Improved business case
• Mechanical property database for common alloys
• Continued integration between design, equipment and manufacturing
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