Conformal Inkjet Direct Write on Aerospace Components · Linking DW and existing hardware Connector...
Transcript of Conformal Inkjet Direct Write on Aerospace Components · Linking DW and existing hardware Connector...
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
Conformal Inkjet Direct Write on Aerospace Components
Industrial Doctorate Centre and BAE Systems
Mau Yuen Chan
Prof. Alan Champneys
Dr. Jagjit Sidhu
Dr. Paul Warr
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• What is direct write (DW)?
• Differences in method to traditional lithography
• Benefits of DW?
• What advantages it brings
• The challenges faced during the study
• The DW system
This Presentation
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
A freeform patterning and deposition technique
• Completes patterning and deposition simultaneously
• Encompasses different deposition techniques
• Droplet
• Laser
• Flow
• Tip
• No single ‘perfect’ technique
• Innovative applications
Direct Write
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
Comparison to Convention
Lithography
• Requires the use of masks
• Large material wastage
• Changes to designs costly
• Etch step limits substrate material type
• Substrates must be relatively planar
• High capital cost
Direct Write
• Freeform patterning
•Low material wastage
• Mass customisation
• Variety of substrate materials possible
• Substrates can be non-planar
• Lower capital costs
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• Benefits:
• Higher material efficiency
• Mass customisation
• Increased design freedom
• Integrated functionality
• COPE Project
• Replacing electronic wiring
with DW solution
Benefits for
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• Aerospace Helmet used by pilots
• Recognised as the most advanced helmet in the world
• Undergoes further development to keep competitiveness • Even during the project study
The Helmet Shell
• Features: • Complex concave Shape • Carbon fibre substrate • Head tracking system; composed of LEDs and flexible connectors for wiring
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
The DW Process
Design
Execution
Evaluation
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
Challenges
Challenge Solution Enabled by
Complex shaped structures Conformal printing 5-axis motion controller
Low thermal tolerance of substrate Localised post-processing iCure
Lower than bulk electrical conductivity Electrodeposition of conductive metal Electroplating head
Linking DW and existing hardware Connector Connector tab
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
Multi-discipline
Printing
system Inks and
substrates
Post-
processing
DW printed component
Electroplating
Mechatronics
Thermal Science &
Physical Chemistry
Physical Chemistry
Electrochemistry
Business
Multi-layers
Electrical Engineering Mechanical Engineering Computer Science Control Systems
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• The ‘creative brain’
• MasterCam is a CAD/CAM design software
• Originally a software program for milling applications
• Used to manipulate CAD models and design DW tracks
• Output: Movement scripts for the
motion controller
MasterCam®
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• The ‘arm’
• A motion control robot with five degrees of freedom giving it a large work envelop
• All tools mounted onto working face • Required mechanical integration
• Precision controlled (0.001mm accuracy)
5-axis Motion Controller
150µm
100µm
50µm
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• The ‘pen’
• Single nozzle jetting device (MicroFab)
• Inks used • Polymer dielectric ink • Silver conductive nanoparticle ink
• Can jet many materials
• May require post-processing to functionalise
Inkjet Printer
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• UV energy delivery system • Required for curing polymer dielectric ink
• Controllable and localised output
• Curing regime affects silver behaviour
Bluewave® System
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• Thermal spot delivery system for sintering • Delivers focussed broad-band optical
energy
+ Controlled thermal exposure + Superior electrical properties than oven sintering - Difficulty on thermally conductive substrates - Inks needed to be modified to match process
iCure™ System
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• 4-point bend test used to investigate possible thermal damage caused by iCure process
• Sintering requires at least 2.0W of energy • Speeds kept constant
• Failure modes: • Compression – Resin failure • Tension – Fibre pull out
• Significant loss in mechanical stability
at more intense exposures
Thermal Damage
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• Chosen as a method of improving electrical conductivity of DW tracks • Improvement to DW track conductivities (reaching ~50-70% bulk Cu)
• Uses brush plating method to deposit copper
• Several designs iterated:
• Improvement to electrolyte flow • Higher current density • Lower surface damage to copper deposit • Be able to navigate around complex 3D structures • Automatic feed/extract system for fluid
• Further improvements:
• Use of local cathode ‘ring’ for local connection
Electroplating
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• Communications with the manufacturer • Requirements capturing • Resolving needs and expectations • Suitable for existing processes
• Several designs created for manufacturer’s approval
• Final design: Connector tab (c)
• Soldered into place • Flexible
Connector Tabs
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
• Aim: To replace chunky wiring in helmet shell with an integrated DW solution
• DW elements successfully fabricated onto a section of the helmet shell • Hardware and DW elements were connected • DW elements passed preliminary round of aerospace durability tests
The DW Helmet
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
DW electronics demonstrated on an aerospace component
• Developed a process that can fabricate DW electronics onto complex 3D structures
• Future work:
• Innovative full DW solutions to electronic applications • Repair work on damaged DW components • Scaling of process for full manufacturing environments
Conclusions
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This work is part of the COPE collaborative project co-funded by the UK Technology Strategy Board (TSB) and EPSRC.
Questions?
The End