Imagination at work.
Greg Morris
Page 3 7/27/2014
Pre-GE Acquisition
MTI & RQM
Founded 1994
Introduced DMLM to NA in 2003
135 employees
Services included:
Engineering & Design
Additive (Metals/Polymers) (25 additive machines)
Post-Processes (Machining, Thermal Processing, Finishing)
Collaborations/JV’s…i.e. MicroTek Finishing w/BinC, etc.
Page 4 7/27/2014
Additive
Development
Center
- GEA focus
- Other GE
- Select Externals
Additive
Lean Lab /
Pilot Production
- Low rate initial production
Page 5 7/27/2014
Manufacturing Technology Development
TRL / MRL 0
TRL / MRL 3
TRL / MRL 6
TRL / MRL 9
ID New
Technologies
Technical
Feasibility
Support
Production
Develop
Technologies
Mature
Technologies
GRC
Additive
Development
Center (ADC)
Additive
Lean Lab
(ALL)
Production
Material Development
Physics Models
Early Process Dev
Material Development
Machine Development
Process Development
---
Test Fixture/ Tooling Mfg
Prototype Manufacturing
Test Article Manufacturing
Pre-Production Mfg
Early Production Mfg
Product VSE
Production Process Dev
Low Rate Manufacturing
Final Production Site (Auburn, AL)
High Rate Manufacturing
Entitlement Cost
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3D CAD Model
AM Process
Thermal
Processing
Post Processing
and Inspection
Final Part
Prep for Process
Basic Process (DMLM)
Additive
Manufacturing
at GE | July
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Types of Additive
Rapid Prototyping? Additive Manufacturing? 3D Printing?
Photo Courtesy: EOS
Photo Courtesy: Stratasys Photo Courtesy: Stratasys
Photo Courtesy: Stratasys
Photo Courtesy: 3D Systems Photo Courtesy: Arcam
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Polymers - SLA
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Polymers - SLS
Photos Courtesy: EOS
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Polymers - FDM
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Polymers - PolyJet
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Metals
Photo Courtesy: ORNL
Photos Courtesy: Within Labs
Photo Courtesy: EOS
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Nano Additive Mfg.
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Other 3D Printing
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GE Aviation Additive:
SLA: (2) 500’s, (2) Vipers
(3) ProJet 3500
ARCAM: (8) A2(xx)
FDM: (1) Fortus 900
PolyJet: (1) Connex 500
EOS: (11) M270’s
(4) M280’s
SLM: (2) 250HL
Photos Courtesy: 3D Systems, Stratasys, EOS, SLM
C-L: (1) M2
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GE Aviation Additive Support:
Multi axis milling
Multi axis Turning
Airflow test stand
CMM/Laser Scan
5-axis EDM Hole Drill
Wire EDM
Extrude Hone
CAD Modifications
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Production Prep:
DMLM: (7) M270’s
Thermal Processing: (1)
Vacuum Stress, (1) HIP
Powder Size Analysis
Inspection
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Instrument Probe - 2007
• Successful builds (no crashes)
• Less cost to produce
• Higher test life
• More accurate probes
• Lower number of probes
required
• Better data collection
• Shorter fabrication time
GE Proprietary Information
Design For Additive
Makers Guild
Corporate initiative to gain exposure and
expertise in the world of 3D printing
Learn about:
•
Build orientation
•
Shape capability
•
Support structure
Original design
Example entry
Crowdsourcing Design Challenge
Public challenge
to find new
design strategies
for additive
manufacturing
150 entries in less
than 30 days
Top designs will
be manufactured
and tested by GE
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Design Challenge and the Potential of
Additive
Tapped into 750k+ online community
Over 700 entries received
Many submissions over 80% weight
reduction
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Parts Grown and Tested
7/27/2014
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Inco
718
Inco
625
316L
SS
W
Ti64
MS-1
Cu
AlSi10
Mg
6061
T6
CoCr
Hast
X
17-4
PH
SS
15-5
Ti 6242
• Super Alloys (2005)
• Many similar to wrought strengths
• Some materials characterized
• Large opportunity for novel alloy
development
Material Properties Drive Applications
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Material Properties Drive Applications
Wrought
DMLM
Horiz
ontal
V
ertic
al
Melt Pool Directionality Vertical Grain Growth
Similar to Wrought
Isotropic / Homogeneous
Typical Equiaxed
Grain Structure
Solution Heat Treatment 40 60 80 100 120 140 160 180 200 DMLS - V DMLS - H Wrought
Low WroughtHigh
YS (ksi) "UTS (ksi)"
18 22 26 30 34 38 42 DMLS - V DMLS - H Wrought
Low WroughtHigh
Elongation (%) "Hardness (HRC)"
ASTM
ASTM
ASTM
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Material Properties Drive Applications
Wrought
DMLS
Horiz
ontal
V
ertic
al
Typical Alpha + Beta Widmanstatten Structure
Finer than DMLS or EBM
EBM
Similar to DMLS Alpha on Deposition Layer
100 120 140 160 180
YS (ksi) "UTS (ksi)
ASTM
ASTM
0 5 10 15 20 25 30 35 Elongation (%) "Hardness (HRC)ASTM
ASTM
GE Proprietary Information
Machining
Special
Processes
Surface
Finishing
Metallurgical
Lab
Thermal
Processing
GE Proprietary Information
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EBM ‘Cake’ – Limit of Internals
How GE Aviation is Using Additive
Metals
GE Proprietary Information
Leveraging AM – NPI Hardware
Fuel Swirlers
7
th
set of HPT’s in 6 years
Substantial cost and lead time reduction
Design refinement options
Land-based Gas Turbine Engines
90 parts in (3) months
Met testing timetable
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DMLM Design Advantage
GE Proprietary Information
DMLM Fuel Nozzle Design History
Begin TAPS
Development
CoCr DMLM Material
Development
DMLM for
prototype testing
GEnx certifies
Traditional Mfg.
22 piece construc.
DMLM supply
chain acquisition
LEAP FETT
2000
2001
2002
2003
2004
2005
2006
2007
2008
2009
2010
2011
2012
2013
LEAP 1 piece
DMLM Nozzle
GE Proprietary Information
LEAP 56 Next Generation Fuel Nozzles
19 Fuel Nozzles in each engine
– 40K full production
20 pieces to 1
5x durability improvement
25% weight reduction
(compared to GEnx)
Fuel Nozzle is a very efficient
heat exchanger
GE Proprietary Information
Exploring Optimized Structures
Optimized Result: 30% less weight
Original
Re-designed (conceptual)
•
Combine parts to eliminate weight
•
Performance gains
•
Maintenance reduction
GE Proprietary Information
45
EXPERIENCE ON EBM - TiAl
Advantages of the EBM process:
low level of internal defects, no typical casting
defects, therefore low scatter in material properties
homogeneous microstructure
very fine grain size, leading to good material properties, in particular fatigue
properties, and no need for grain refinement
no limitations in chemical composition
no residual stresses due to high process temperature
little waste material: powder can be recycled as the oxygen pick-up is very
low
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Accelerating Adoption
Present 2014 2016 2018+Process
Variation
Validation
Tools
Surface Finish
Growing Acceptance with Continuous Innovation
Accepted Industry
Standards
Process
Monitoring
Diversified
Materials
Higher Capacity
Machines
Application
Specific Machines
Predictive
Analysis Tool
Gradiated
Materials
Accepted
Best Practice
Process
Automation
GE Proprietary Information
Gaps and Challenges
•
Rapid Qualification
& Materials Database
•
IP: Rights & Tracking
•
NDT / Internal Flaw detection
•
Supply Chain:
Development & Protection
•
Available Materials
•
Technician Skill Level
General
Process Specific
•
Surface Finish
•
Distortion
•
Build Volume
•
Throughput
•
Process Monitoring and
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Supply Chain Shift?
From
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More Local?
Field Operation
Substantial supply chain
challenge in remote locations
Spare / Repair parts on-site?
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Parts Inventory
Local ability to grow parts?
Controls inventory
Balance inventory with
needs/delivery
Flexibility for design changes (no
order minimum)
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Broad Trends
Challenging IP landscape
Further consolidation (all areas)
Increased adoption of technologies
Accelerating innovation
New business models
0 20 40 60 80 100 120 140 160 2012 2013 2014 2015 2016 Applications IP Alloys
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Creators &
Pioneers
Adopters
Early
Majority
Primary
Secondary
Majority
Holdouts
What Phase Are We In?
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