food and chicken
TRANSCRIPT
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Laser Drilling of Cylindrical
and Shaped Holes
NCMS/CTMA Symposium: Track 1b
Terry L. VanderWertPRIMA North America, Inc.
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Outline
Laser drilling technology overview
Capability Applications Recent developments benefits of integration
Repair applications Potential benefits
Potential projects
Summary
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Customers
Serving Turbine Engine Manufacturers
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Laser Drilling - An Enabling Te chnology
Incremental improvements have led to substantial increases in
the number of cooling holes in new engine designs.
Laser drilling is fast relative to competing methods for smallholes translates into substantially lower cost.
No tooling means lower cost, faster turnaround the tool isa focused beam of light
Flexible single part lot sizes Easily interfaced with CAD/CAM
Drills/machines a wide range of materials At shallow angles Complex shapes
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Laser Drilling of Cylindrical Cooling Holes
Typical applications Cooling holes in blades, vanes,combustors, and afterburners
0.3 to 1 mm diameter holes at 15-90 in cast, sheet, andmachined components, uncoated and with TBC
Rates 0.25to 5holes per second
Airfoil
Air flow
Film cooling holes
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Laser Drilling of Shaped Cooling Holes
0.8 - 1.2mm
0.8 - 1.2mm
10-30 degrees
Wine Glass Shape
(Fan in, Fan out)
Race Track Shape
(Fan in, straight out)
Top View
1. Pierce undersized through hole2. Trepan fan shape- through hole
3. Finish through hole to size(trepan to exit hole diameter)
Top View
1. Pierce undersized through hole2. Trepan fan shape- through hole
3. Finish through hole to size(trepan to exit hole diameter)
Film cooling holes increase efficiency ofcooling air by 30%, reducing the amountof air required for cooling.
Used sparingly today because of their
cost when produced using EDM.
0.4-1.2 mm
1.5-3.0 mm12-20degrees
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Recent Developments by PRIMA North America
for New Part Manufacturing and Repair
Process control for improved airflow consistency Optimum laser process parameters for cylindrical shaped
holes Drill at focus
Breakthrough detection
Optical focus control (for TBC)
Simple shaped hole drilling
Distribution of Exit Hole Diameter
0.50 0.60 0.70 0.80 0.90
Hole Diameter, mm
Without Breakthrough Detection
Breakthrough Detection
The bottom line? More consistent holes
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Repair Applica t ions for Laser Drilling
Re-drilling of cooling holes.
Some cooling holes become blocked during repairs bywelding or brazing
Holes must be re-drilled to restore component airflow.
Blades and vanesrepaired by
welding orbrazing.
Cooling holesbecome blockedand component
suffers somedistortion
Cooling holes re-drilled by laser
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Repair Applica t ions for Laser Drilling
Removal of TBC overspray
Coatings must be removed before any repairs can takeplace.
Re-coating partially fills cooling holes and this mustbe removed to restore component airflow.
Coating must bestripped from
componentsbefore repair.
Repaired componentsmust be re-coated.The new coating
covers existingcooling holes
Coating overspray
removed by Laser
Issue: Amount of
new coating in thehole varies
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Potential benefits of laserdrilling for repa ir depots
Reduced costs
Reduced turnaround time - keep aircraft flying
Provides a method for producing engines
having increased engine performance Thermal barrier coatings Film cooling shaped and cylindrical
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Potential Projects
Laser source technology for combined machining and
drilling in uncoated as well as thermal barrier coated (TBC)
components
Automation of set-up and drilling Probe repaired components to compensate for
deviations in shape and position
Identifyactual hole locations
In process gauging - improve process efficiency andquality by automating part inspection
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Laser source technology for
combined machining and drilling
Objective- Develop laser source capable of both pulseddrilling of cylindrical holes and ablative machining ofshaped holes.
Challenges Produce laser source having both ms (deephole drilling) and s (machining) pulse widths, with highbeam quality.
Potential return Improve productivity andreduce cost for laser drilling by takingadvantage of the speed of laser machining and
producing complete shaped holes in a singlesetup.
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Laser Drilling Capability is Source Dependent
Throughput holes/second minutes/hole
Feature size f (wavelength, lens focal length, beam diameter, beam quality)
Debris 10s m negligible
HAZ/recast tens to hundreds m less than 10 m
Depth control inversely related to removal rate
4 FBeam = M
2
D4 F
Beam = M2
D
CW fs
Melt expulsionVaporization Ablation
ColdAblation
PulsedNd:YAG(ms/s)
Q-switchedNd:YAG
(ns)
Ti:Sapphire(fs)
Nd:YVO4(ps)
Cu vapor(ns)
Excimer(ns)
Coarse to fine
CW fs
Melt expulsionVaporization Ablation
ColdAblation
PulsedNd:YAG(ms/s)
Q-switchedNd:YAG
(ns)
Ti:Sapphire(fs)
Nd:YVO4(ps)
Cu vapor(ns)
Excimer(ns)
Coarse to fineMechanism
1.E-04
1.E-03
1.E-02
1.E-01
1.E+00
1.E+01
1.E-12 1.E-09 1.E-06 1.E-03 1.E+00
Pulse duration, sec
Removalrate,mm^3/sec
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Automation of Setup and Drilling
Objective Develop vision and probing tools to gauge theshape and hole location of repaired components.
Challenges - Parts aredeformed; shape will not match that
of the new component. However, the repair holes mustbe coincident with the original holes.
Potential return Improved productivity by automating
time-consuming setup steps.
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In Process Gauging
Objective Actively monitor component airflow to
determine which holes should be re-drilled.
Challenges Integration of gauging tools with lasermachines.
Potential return Higher quality components.
Greater machine utilization byavoiding inefficiencies ofremoving/resetting the part into thedrilling system.
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Summary
Improvements in laser drilling technology for modern,
new component manufacturing can benefit repair whether at the repair depot or commercial partner.
Additional technology development is needed to improveproductivity, reduce dependence on skilled operators, andimprove consistency in repair operations.
PRIMA North Americas 20+ years history of innovationin lasers for turbine engine manufacturing and repair willreduce risk and cost of these developments.