- EU joint project
TOPPCOAT
wards design and rocessing of advanced, cometitive thermal barrier ing systems
Aerodays2011 Matthias Karger, Robert Vaßen
IEK(1, Forschungszentrum Jülich GmbH
TOPPCOAT wards design and rocessing of advanced, com etitive - - PowerPoint PPT Presentation
EU joint project TOPPCOAT wards design and rocessing of advanced, com etitive thermal barrier ing systems Aerodays2011 Matthias Karger, Robert Vaen IEK(1, Forschungszentrum Jlich GmbH Outline Short
IEK(1, Forschungszentrum Jülich GmbH
Basics Management Technical specifications, material procurement Powders and materials
Development Interface modification Advanced technology for manufacture of strain tolerant coatings Screening of key properties and full characterisation Evaluation Transfer & application of technology Final evaluation under close(to(service conditions
Increase temperature capability Increase engine efficiency Provide cost effective alternative to EB(PVD
Improve APS coating lifetimes comparable to those of EB(PVD (segmentation, 3D interface) Introduce gas phase processes for industrial application (coating of complex shaped specimen)
with conventional feedstock
to induce seg.cracks /stop horizontal cracks !
phase deposition
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sized feedstock or alternative TBC material
agglomerated nano particles
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#"$$%
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Milestones: Coatings on bond(coated substrates
500Im
Triplex II technology Feedstock: 8YSZ fused & crushed (TIAG) Porosity: Overall: ~6% (Mercury porosimetry) Crack density: ~9 cracks/mm @500Im thickness F4 technology Feedstock: 8YSZ spray dried (SM) Crack density: ~9 cracks/mm @500Im thickness with conventional feedstock
Further development of Taylor (1991), Bengtsson et.al. (1999), state of the art were 3(4 cracks/mm
500Im
Surface modified by application of laser(cladded 3D structures to induce seg.cracks /stop horizontal cracks PVD(LPPS (fka LPPS(TF)
#/)0 "1
Suspension plasma spraying Triplex II
sized YSZ particles in ethanol
with high porosity values (~35%)
SPS coating SPS plasma jet injecton
2 21 bondcoat/topcoat systems (~250 specimen) tested "2 Microstructure Furnace cycling 1st Burner rig test
commercial PtAl+EB(PVD reference Bondcoat: Thickness 150–200Im Ra 12(14 Pm
3"$
Reference systems
Cyclix oxidation Erosion Burner Rig Corrosion Mechanical response Thermography
~250 CMSX4 specimen with different geometries were needed
Test conditions: TBC thickness FT Cycling 150Im 1100 23hFT,1h RT 300Im(400Im 1050 23hFT,1h RT 500Im 1000 23hFT,1h RT Test results 3D APS LPPS(TF F4 APS Triplex II APS APS Ref. EB(PVD Ref.
0)4 %5
Test conditions: CMSX4 pipes, 150x16mm Surface Temp. 1200°C
>100°C Cycle 210s hot 75 cooling (<100°C) Test Results 3D APS LPPS(TF F4 APS Triplex II APS APS Ref. EB(PVD Ref.
3$+%6 0+7
4"$20)4
Test temperature 700°C Impingement angles 30°, 90° Erosive Material Quartz Particle feeding rate 2g/min Impaction speed 25(40m/s Test Results 3D APS LPPS(TF F4 APS Triplex II APS APS Ref. EB(PVD Ref.
0)4 %5
8$ 0)4
Test conditions: Test temperature 900°C Test medium 75% NaSo4, 25% NaCl Test specimen massive Pins CMAS(like test Test Results 3D APS LPPS(TF F4 APS Triplex II APS APS Ref. EB(PVD Ref.
"' 4"$ 8/9%*/$$ 4$
Test conditions: Dwell temperature 1050°C/‘ 1100°C(*) Cycle duration 2h Heating/cooling 15min
%5*':
Test Results 3D APS LPPS(TF (*) F4 APS Triplex II APS APS Ref. EB(PVD Ref.(*)
83)#/;'<= 0)4'<=
0,00 0,25 0,50 0,75 1,00 3D new FZJ LPPS(TF SM (~300Im) APS SM204BNS HTU APS f&c FZJ APS ref TUC EB(PVD ref SNS NLR Burner Rig VAC Burner Rig ALSTOM FCT AVIO corrosion Cesi Erosion
3D APS LPPS TF F4 APS TriplexII APS APS ref. EB(PVD ref
0,5 1 1,5 2 2,5 3 200 400 600 800 1000 1200 $6=7 '5$>6:?7
3D + seg APS 2.5 Porous APS (ref) 0.6 Triplex 2 APS seg. 1.9 EB(PVD (ref) 2.0 F4 APS seg. 2.1 LPPS(TF 1.6 Measured via Laser Flash Technology [ W/mK
#.$"'" 0@." " ", (%'">% 0)4 "$ 4 (%'">%
TBC thickness
+ + 08
08 :08
:8
08 :08
TBC thickness and porosity on real components
Laser Luminescence
Sensor Coatings Repair technology
EB(PVD coating LPPS(TF coating Defect
Modelling / FEM analysis of 3D modifications Monitoring the process
)5 )5 )5 )5 )5 )5 5
linear fit
"6>7 '&6
YSZ Thickness Intensity Ratio
Mechanical tests