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BOEING is a trademark of Boeing Management Company.Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 1
Steps to Improve Direct ManufacturingReadiness Levels
Jeffrey DeGrangeSenior Manager – Advanced Manufacturing Research & DevelopmentSt. Louis, Missouri USA
EuroMold 2006Frankfurt, GermanyDecember 1st, 2006
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 2
Digital Manufacturing Technologies
SelectiveLaser
Sintering
Stereo-lithography
R.E. – ATOSScanning
LaserTracking
FusedDepositionModeling
LaserProjection
EBM-DirectMetal
SLG50031993-043.ppt
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 3
Use of Digital Information to Grow Parts
Selective Laser Sintering (SLS) Uses a Computer Controlled Laserto Construct Physical Objects Directly From a 3-D Solid Model Using Powdered Materials.
Process Overview1. Create 3-D Model Base Definition (Unigraphics, CATIA, ProEngineer)2. Electronic Delivery of the 3-D Model to SLS System. 3. 3-D Model Sliced Into Ultra-Thin 2-D Layers and Part Program Created.4. Laser Will Sinter Loose Powdered Material Together by Drawing and Filling the Cross-
sectional Cut for Each 2-D Layer.5. Repeat Process for Each Individual Layer Until Object Is Complete.6. Remove Objects From Bed of Powder.
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 4
Stereolithography Applications
Wind Tunnel Test Articles
Fit Check Articles
•High Accuracy (+/-0.003”)•Materials ranging from high modulus to Elastomer replicates•Loaded materials available : Ceramics, Metallic•Known wind tunnel scaling factors
Copyright © 2006 Boeing. All rights reserved.
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Stereolithography Development Work
• Supplier Material Development• Low Cost Metal Plating
Flight Simulator Control Sticks
Metal Plated SLA
Copyright © 2006 Boeing. All rights reserved.
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Selective Laser Sintering Applications
FABRICATED SLS DETAILS3D CAD MODEL
ASSEMBLED DRILL PLATE
POWER FEED DRILLING USING SLS DRILL PLATE
Copyright © 2006 Boeing. All rights reserved.
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Selective Laser Sintering Applications
Environmental Control System Ducting on military aircraft
Copyright © 2006 The Boeing Company. All rights reserved
• Reduced Part Count• Flexible Design• Reduced Cost• No Tooling• Increased Cycle Time
Copyright © 2006 Boeing. All rights reserved.
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Selective Laser Sintering Development Work
• Larger Build Chamber Machines• Flame Retardant Material for FAA Requirements
Copyright © 2006 The Boeing Company. All rights reserved
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 9
Fused Deposition Modeling Applications
• Quick Turn-around of Polycarbonate, ABS, and PPSF components• Sparse Fill feature offers rigid, lightweight components• PPSF is a high-temperature plastic (HDT=372° F)
Assembly tool for short run repair workLarge Scale Trim Tool
and Holding Fixture
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 10
Fused Deposition Modeling Applications
Ground support equipment and toolsBox Subsystem Simulators
Copyright © 2006 The Boeing Company. All rights reserved
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 11
Fused Deposition Modeling Applications
Composite FabricationTooling
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 12
Electron Beam Melting
Electrons are emitted from a filament which is heated to > 2500° CThe electrons are accelerated through the anode to half the speed of lightA magnetic field lens brings the beam into focusAnother magnetic field controls the movement of the beamWhen the electrons hit the powder kinetic energy is transformed to heat.The heat melts the metal powder
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 13
Electron Beam Melting Development
• Low cost Titanium powder• Better control systems• Heat Transfer modeling techniques
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 14
Where Is the Technology Going?
Evaluation of Direct Nylon Components for Commercial Applications
Meet Flame & Toxicity Requirements
Continue the Advancement of Direct Manufacturing of Thermoplastic and Metal Materials
Production to Additional Programs and Applications
Mainstream the Use for Rapid Tooling and Post-Production Support Applications
Enables the Ability to “Design Anywhere, Build Anywhere”
Direct Manufacturing Technology will Fundamentally Change How WeThink About Design, Manufacture and Support
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 15
Example for Production Applications Multi-Functional Designs
New (SLS) Configuration
Previous (Kevlar/Rotomold)Configuration
Attach Straps Eliminated• Part Count Reduction• Quick & Easy Installation
Multiple Ducts Combined to Single-Piece Duct
Conformal Shapes Achieved and Internal Flow Features Added
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 16
Example for Production Applications The Value of Direct Manufacturing
• Engineering Design:• Direct from 3-D Model Base Definition• Design and Build Flexibility
• Production:• Eliminate non-recurring tooling costs• Lower recurring unit part costs• Faster part delivery times• Supplier flexibility• Direct Fabrication:
• 50% Cost Reduction• 67% Cycle Time Reduction at
Minimum• Product:
• Reduced part count and weight• Lower inventory and transportation
costs• Improved Life Cycle Product Costs
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 17
Production On Demand
Out Production Parts
Reproduced(Prototype)
Dynamic Supply
Chaining
Coexistence of Typical Productionand Production On-Demand
DevelopedBuild-toPackage
Re-Modeled
Scanned Results
Sample Part
Return to Agenda
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 18
Qualification & Certification Definitions
• Qualification- Focus on Controlling Variables Within Acceptable Limits- Includes Materials- Included Processing
- Also Covers Equipment Certification- Intent is Demonstrating a Stable Material and Process for Use on Applications
- Three to Five Batch Qualifications for Each Test to establish B-Basis Material Allowables
• Certification Focus is on the Application- Point Insertion- General Insertion
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 19
Candidate Application Selection
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 20
Platform Evaluation Methodology
Step 1
Step 2
Step 3
Step 4
• Tailor AIM-C Readiness Level Guides Towards Direct Digital Manufacturing
• Process/Equipment• Materials
• Establish More Specific Questions to Translate Exit Criteria Into Relative Items
• Process/Equipment• Materials
• Assess Maturity In Each of the Categories/ Groups/Items
• Process/Equipment• Materials
• Establish The Specifics For Conformance Activities to Meet Maturity Exit Criteria with the Selected Technologies and Applications
• Process, Equipment, Matl’s, Structures
TRL’sxRL’s
Questionnaire
TechnologyAssessment
ConformancePlanning
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 21
Initial Overall Technology Readiness Level (TRL) Guide
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 22
Key Areas- Education of Design Communities
• Remove the ‘Cuffs’ of Design For • Manufacturing & Assembly (DFMA)
• Complexity is Ok.. Even Good!
• Propagate the Design For Function (DFF) Design Mentality
• Encourage the Adaptation of Designing Multi-Functional Parts• Encourage sub-systems teams to work together
• Industry Service Specifications (SAE, ISO, AMS, etc.)
• Universities Must Begin to Teach the Principles of Direct Manufacturing
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 23
Key Areas- System Development Needs
Platform Up-time Must Approach 90%
Product/Process Consistency• Thermal Consistency• Dimensional Consistency
Production Capable Operational StrategiesOff-line Cool Down/Warm UpPallet Shuttle System Approach
Platform Modularity to Improve ServiceabilityShaping Sub-systemsEnvironmental Control Sub-systems
Software CapabilitiesProcess Monitoring/Data Acquisition SoftwareSelf Calibrating CapabilitiesOpen Architecture Code (Not Necessarily Control algorithms)
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 24
Required Materials Advancements
• Incoming Product Consistency• Batch and lot traceability• Contaminant free material
• Reasonable Product Cost • The product must be available in bulk buys• Sellers must add value to the product
• Supply Chain Capable of Delivering Production Quantities• Pounds Consumed Substantially Increased with the
Number of Applications
• Improved Performance Materials• Temperature, Stiffness, Strength, Toughness, Etc.
• Base Level Standardization of Property Reporting
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 25
Required Materials Advancements
• Improved Performance Materials• Isotropic properties• Stiffness (at elevated temperatures)• Strength (at elevated temperatures) • Toughness (at low/room temperatures)• UV Resistance
• Base Level Standardization of Property Reporting• Tensile• Impact• Hardness
• Scientific Understanding of Material Characteristics and Processing Characteristics• Explanations of empirical phenomena• Develop materials performance prediction tools
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 26
Key Areas- Industry Short-Comings
• Reliable, Prompt Maintenance• Machines cannot be down for extended periods• Selected spares stock on-site to reduce delays• Train on-site maintenance personnel on some
recurring calibrations or repairs to eliminate down time
• Reasonable Cost of Maintenance Contracts• On-site spares stock included in the maintenance
contract• Bulk buy contracts for vendors with multiple
machines
• Develop Concise Troubleshooting Procedures• Eliminate the ‘Shot Gun’ approach to repairs• Reduce down time as well as cost for the OEM
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 27
Process Repeatability
• Dimensional Accuracy and Repeatability
• Requirements for Acceptance:
• Build test article (shown left) in 9 locations within build chamber; diagonally across the x-y top, middle and bottom. All measurements between cubic facets must be within ±.007”.
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 28
Development of World Wide Supply Base
Revenues from rapid prototyping / rapid manufacturing industry reached $705.2M in 2004 and is growing
Direct manufacturing for Boeing depends on collaboration with supplier networks across national borders
Over (1170) SLS machines currently installed world wide
High-speed and large-frame machines enhance productivity and reduce part cost
Boeing standards for SLS manufacturing and quality control are well established
Certification of SLS manufacturing centers in USA, Europe, and Asia is feasible for production
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 29
Certain Challenges Remain
Bigger Batch Sizes Logistics Flow
New Part`s Designs
Higher AutomationLarger Part Sizes
Part‘s Homogenity
Faster Production New Designs
Have to be reflected in ....
……………
Machine Design
Quality Control & Standards
Material Properties
Process Technology
Production Process &
Control
Parts Design & Engineering
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 30
Strategic Vision for Direct Manufacturing
Capable
Broader Marketplace
ReliableRepeatable
Reduce Cost & Part CountContinuous
Improvement
Production Capable Direct Manufacturing System
Copyright © 2006 Boeing. All rights reserved.
11/17/2006Filename.ppt | 31