Fabrication additive par procédé CLAD® : principes ...
Transcript of Fabrication additive par procédé CLAD® : principes ...
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Fabrication additive par procédé CLAD® : principes, performance et exemples d’applications
Additive Manufacturing with CLAD® process: principles, performances and application examples.
Didier BOISSELIER – Jérôme WURSTHORN
– Philippe ACQUIER / IREPA LASER
NOGENT - 29 Novembre 2016
Laser Technological centre in France
Industrial laser applications and developments in the field of material processing
IREPA LASER
More than 30 years of experience. 42 people.
Products : feasibility, technical and economic studies,
training, industrialization, R&D, …
≈ 20 lasers in the lab : YAG, Fiber, diode, Femto, …
•with multiaxis workstations and robot
• analysis means: laser beam analyzer, 3D
profilometer (ALICONA), metallographic, …
Expertise and fine characterization :
Main activities:
Welding and surface treatment
Micro-machining
Training
…. And additive manufacturing
3 CLAD machines
+ future SLM machine
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KEY COMPONENTS OF CLAD® PROCESS
Track width 1 – 2,2mm
Accuracy ±0,2mm
Build up rate 120 cm3/h
Machine
Software
Process
CLAD® Process
Construction by Laser with Additive and Direct Process
MACHINE : MAGIC
5 axis machine :
XYZ + BC
Working space :
3D (CLAD) : 1500x840x800 mm3
Max load : 300 kg
Gas enclosure :
Volume : ≈ 12 m3
O2<40 ppm, H2O<60 ppm
2 lasers :
Fibre 500 W + Diode 2 kW
2 CLAD® heads
FALAFEL FUI Project (Fabrication Additive Laser et Faisceau d’Electrons)
MAGIC = "Machine Aeronautique Gaz Inert CLAD®"
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XY
Z
C
B
MACHINE : BIOCLAD
BioCLAD:• Enceinte gazeuse (1m3)
02 < 40 ppm et H2O < 50 ppm
• 5 axes continus:X400 x Y250 x Z200 + B±110°, Cn360°
• Charge maxi: 50 kg
• CNC : Power Automation 5 axes
• 1 buse
• Laser QCW 600/6000 (mode continu ouimpulsionnel)
• Système de distribution de poudreà plateau vibrant
LASER CLADDING
Layer thickness 0,5 2 mm
Track width 3 5mm
Efficiency > 90%
Dilution < 5%
Layer thickness 0,2 0,7 mm
Track width 0,3 3 mm
Efficiency 20 - 90%
Dilution 5% 20%
CLAD®VS
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APPLICATION POTENTIAL OF THE CLAD® TECHNOLOGY
materials grade State of CLAD® developmentCLAD®
results
Steels
Low carbon steel Parameters ok
Alloy steel (low Ceq) Parameters ok
Tool steel (CPM10V, M2) Cladding ok
Stainless
steels
SS304L, 316L Parameters ok
APX4 Parameters ok
17-4 Ph Parameters ok
SS440, … Setup in progress
Ni base
alloys
Inco 718, 713 Qualified on aero parts
Inco 625, 738 Parameters ok
Nimonic C263, 75 Parameters ok
Rene 77, 142 Parameters ok
Waspalloy Qualified on aero parts
CMSX4 Setup in progress
Ti base
alloys
Ti6Al4V Parameters ok
Ti6Al2Sn4Zr2Mo (6242) Qualified on aero parts
CpTi Parameters ok
Co base Stellite 6, 12, 21, 25 Cladding ok
Al alloys Al alloys (Si, Mn, Mg …) Difficult to process
Cu alloys Cu alloys (Zn, Sn, Al, Ni, …) Difficult to process
Au alloys Au alloys Difficult to process
Others
W Difficult to process
WC Ok with Ni matrix
Mo Setup in progress
MATERIALS …… WELDABILITY
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METALLURGICAL AND MECHANICAL PROPERTIES
• Very low level of pores (<0,01%)
• Fine microstructure (rapid solidification)
• Mainly for weldable materials (Ti and Ni alloys, SS, …)
• Local or global gas shielding for oxidization prevention,
mainly on Ti alloys
• Low dilution of the first layer on substrate
Very few pores detected: Ø 50 – 70 µm
NDT TOMOGRAPHY
1025 November 2016
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115
830900
100111
780
860
50115
9931041
99115
929
1027
100
0
200
400
600
800
1000
1200
E (Gpa) R0,2 (Mpa) Rm (Mpa) A% (x10)
Tensile testing results
forging(AIMS 03-20-002)
casting(IGC 04.40.11)
longitudinal direction Z direction
Ductile failure mode – no significant defect
Mechanical properties: tensile testing of Ti6Al4V
Repairing of worn or damagedparts
Fonctionality adding on existing valued parts
Manufacturing of functionnalparts
Preform manufacturing to bemachined
CLAD®
POTENTIAL OF CLAD® PROCESS
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EXAMPLE : PART REPAIRING
Repairing of the worn knife edges of sealing parts
Collaboration with a company specialized in engine maintenance
Company : Chromalloy France
100 people
Essentially repairing for Pratt & Wittney : PW100/ PT6/ JT15 APU (901)
SEALING RINGROTATION SPEED: 30 000 TR/MIN
6 references of parts repaired and qualified
> 1200 parts repaired and returned to flight
First piece began its second cycle repair in August 2012
REPAIRING
With courtesy
≤400µ
m
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Repairing of worn or damagedparts
Fonctionality adding on existing valued parts
Manufacturing of functionnalparts
Preform manufacturing to bemachined
CLAD®
POTENTIAL OF CLAD® PROCESS
EXAMPLE: FUNCTIONALITIES ADDING
Screw rotor Flange
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Repairing of worn or damagedparts
Fonctionality adding on existing valued parts
Manufacturing of functionnalparts
Preform manufacturing to bemachined
CLAD®
POTENTIAL OF CLAD® PROCESS
TRUMP : PREPARATION
Material : Nickel Based alloy (Nimonic C263)
Manufacturing started on SLM subpart
Part adaptation to the process:
Thickness variation eliminated
Modification of the cones geometry
Corner radius added for the mounting lugs
Subpart built upwith SLM process
by
Subpart built upwith CLAD® process
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TRUMP: PRODUCTION
Material Ni based alloy (Nimonic C263)
Wall thickness 0.8 mm
Construction duration Total : 3h46min(2h46 + 1h)
Deposited mass of Nimonic 520 g
Powder catchment efficiency 21%
Average build up rate 18 cm3/h
Roughness Ra5
Powder to be recycled 1900 g
Industrial demonstrator: airduct Ti64 FUI FALAFEL 2014 – IREPA LASER
Dassault Aviation Courtesy
Hybrid process
SLM + CLAD
Feedback:
Part model evolution
Dialogue: Designer manufacturer
SLM subpartmade by
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BIG PART MANUFACTURING
Technical data:
Material : stainless steel 316L
Weight : 25kg (with 11kg baseplate)
Øext tube : 430mm – wall thickness : 2.5mm
Deposited material : 14kg
Manufacturing time : ≈ 20H
Before machiningAfter machining
Repairing of worn or damagedparts
Fonctionality adding on existing valued parts
Manufacturing of functionnalparts
Preform manufacturing to bemachined
CLAD®
POTENTIAL OF CLAD® PROCESS
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Mounting bracket
EXAMPLE : PREFORM + MACHINING
Material : TA6V
Manufacturing
Start with a plate : 250x60x10 mm3
Wall dimension : 250x55x7 mm3 (460g)
Cycle duration : 49min – PCE = 64% - 120cm3/h
Machining
Minimum machined thickness : 0.3mm !
Overthickness VS distortion
EXAMPLE : PREFORM + MACHINING
Traditional machining14 364 cm3
104.7 Kg
Features added by CLAD4 543 cm3
33.2 Kg
Final part27 Kg
Application example:
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CONCLUSIONSConstruction by laser of parts in true material
additive process : material feeding
direct process : from CAD to part
high quality : no cracks, extra low level of porosities,
high mechanical resistance : fine microstructure
control of the deposited materials:
Multi-material construction
Localized deposition of expensive materials
set up possible for fine repairing, on high value added parts
No size limitation
Able to build up on complex surface (not only flat)
Slicing 3D
Powder to be used = injected powder
Performance of the process:
MesoCLAD : 1 up to 10 cm3/h
MacroCLAD : 10 up to 200 cm3/h
Didier [email protected]
THANK YOU FOR YOUR ATTENTION