Alternatives to hexavalent Chromium in the aerospace .... Alternatives to Hex Chrome... ·...
Transcript of Alternatives to hexavalent Chromium in the aerospace .... Alternatives to Hex Chrome... ·...
Alternatives to hexavalent Chromium
in the aerospace supply chain
New ideas for CAA anodizing process replacement
TUESDAY 14 June 2011
A.Viola
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This document and the information contained are Safran property and shall not be copied or disclosed to any third party without Safran prior written authorization.
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AGENDA
1) INTRODUCTION
2) SAFRAN
3) ALTERNATIVE PROCESSES
4) ANODIZING
5) CONCLUSIONS
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AGENDA
Tier-1 equipment supplier
An international high-technology group
Safran
Aerospace
Defence
Security
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26 %
12 %52 %
10 %
Key
Revenues: 10.8 billion euros
Recurring operating income: 878 million euros
Net income – Group share: 508 million euros
2010 revenues
figuresAircraft Equipment
DefenceAerospacePropulsion
Security
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An international high technology group
Revenues of 10.8 billion euros*
More than 54,000 employees in over 50 countries
3 core businesses:
Safran
Aerospace
Defence
Security
at a glance* As of December 31, 2010
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Capital shareholdingAs of December 31, 2010
56 %
French State
30.2%
Areva
2%
Public
47.6%
Treasury shares
4.2%Employees
16%
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56 %
Europe
Morocco
Design
office
Industrial
site
HQ Office
United States
Mexico
Colombia
Brazil
Uruguay
Canada
South Africa United Arab Emirates
China
India
Japan
Malaysia
Services
Singapore
Australia
Safran worldwide
employees
54,000More than
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LARGE BROAD OF PRODUCTS (1)AEROSPACE ENGINES
Civil aircraft
helicopter
Military aircraft Spatial
Futur civil
engines
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LARGE BROAD OF PRODUCTS (1)AEROSPACE ENGINES
Civil aircraft
helicopter
Military aircraft Spatial
Futur civil
engines
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Ariane 5
Vinci®
(Under
development)
HM7B™Thrust:
22,000 lb
Vulcain®2
Thrust:
297,000 lb
Ariane 5
AEROSPACE ENGINES
HTE
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EQUIPEMENTS (1)AEROSPACE EQUIPMENTS and PARTS
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OUR CUSTOMERS
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« Ce document et les informations qu’il contient sont la propriété de Snecma. Ils ne doivent pas être copiés ni communiqués à un tiers sans l’autorisation préalable et écrite de Snecma. ».
Fan blades, booster and Fadec on GEnx engine
Landing gear
Wheels and carbon brakes
Electric brake actuation controller (EBAC)
Wiring
DREAMLINERBoeing 787
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« Ce document et les informations qu’il contient sont la propriété de Snecma. Ils ne doivent pas être copiés ni communiqués à un tiers sans l’autorisation préalable et écrite de Snecma. ».
XWBAirbus A350
Integrated landing and braking system
Main landing gear
Wheels and carbon brakes
Fuselage and engine pylon wiring
Components for onboard information system and flight control system
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« Ce document et les informations qu’il contient sont la propriété de Snecma. Ils ne doivent pas être copiés ni communiqués à un tiers sans l’autorisation préalable et écrite de Snecma. ».
Vulcain main stage engine
HM7B upper stage engine
Solid booster motors, via Europropulsion
Launch vehicle
ARIANE
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Safran and GE
71% share of engine market for single-aisle commercial jets
World’s largest fleet: 20,000 CFM56 engines delivered to date
A textbook case of a successful transatlantic partnership in the
aviation industry (and industry in general): the CFM56 is the world’s
best selling aircraft engine
Backlog of orders exceeding 5 years of production
A CFM56-powered plane takes off every 2.5 seconds
5,000 takeoffs between engine overhaul
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ALTERNATIVE PROCESSES
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GENERAL REQUIREMENTS
Choice criterias for a satisfactory aluminium surface treatment
• Fatigue properties
• Painted performances
• Corrosion resistance
• Process monitoring
• Patent rights
• Waste, pollution
• Bonding properties
• Chemicals resistance
Electrical properties
Touch up process
Supply chain diffusion
Cost
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SOME REPRESENTATIVE PARTS
Painted nacelle beam
Painted wheel
Painted nose wheel landign gear
Unpainted gear boxe housing
Painted piston housing
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ALTERNATES
• Conversion coatings
• E Coating (PPG)
• Electro Ceramic Coating (Henkel)
• Aquence Technology (Henkel)
• Micro Arc Oxydation (Ceratronic)
• Sol Gel Technologies ( Millidyne – ICS – NCT)
• Anodizing processes(SAA, PAA, TFSAA, DSA, TSA, SPA, BSAA, Duplex…)
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ALTERNATE (1)
Mainly chromium III based ( Surtec, Henkel 5923..)
Permanganate based (Sanchem)
Necessity to have an enhanced technology for 2000 and 7000
aluminium series (corrosion resistance equal to hexavalent
technology)
Conversion coating + inhibitor + eventually additional layer (Lanthane
613.3 +)
Conversion coatings
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ALTERNATE (1) Conversion coatings
This process finally reach the CCC corrosion resistance
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ALTERNATE (2) E Coatings
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ALTERNATE (2) E Coatings
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ECC CoatingsALTERNATE (3)
• Hardness: 600 - 800 vickers
• Abrasion resistance: cycles ( CS-10 Wheel, 10,000 cycles) TWI 1.5
• Flexibility, pass 1-2T bend (ASTM D 4145)
• Coefficient of Friction: 0.1-0.2 dry
• Thermal resistance, 600 ºC, 84 hours – no change in adhesion
• Titanium oxide coating (TiO2) Corrosion Resistance > 3000 hours
Alodine EC²
ECC Coatings
Electroceramic Coating
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ALTERNATE (3) ECC Coatings
Alodine EC²
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ALTERNATE (3) ECC Coatings
Alodine EC²
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ALTERNATE (4) E.A.U. CoatingsEpoxy Acrylic Urethane Coating
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ALTERNATE (4) Epoxy Acrylic Urethane Coating
Not available yet for aluminium
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ALTERNATE (5) MAO / PEO Coatings
Plasma Electrolytic CoatingI (t) [A]
IP
T
time
IN
Main parameters control :
• Treating duration
• Signal shape (cyclic ratio)
Qp / Qn
• Positiv intensity (5-210 A)
• Frequency (100 à 1000 Hz)
Electrolyte type (conductivity, composition, temperature…)
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ALTERNATE (5) MAO / PEO Coatings
Plasma Electrolytic Coating
Thickness range
Hardness
Fatigue properties
Corrosion resistance
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ALTERNATE (5) MAO / PEO Coatings
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ALTERNATE (6)
Degreasing
Rinsing Rinsing
1 . Pickling
Socosurf A1858 (25%)
+ A1806 (10%)
30°C 15min
Rinsing
2 . SAA
H2SO4 200g/L
18°C
Rinsing
3 . Sealing
Lanthane 613.3
part A (100mL/L)
+ part B (75mL/L)
40°C 10min
Post-sealing
H2O (dionised)
98°C 30min
Painting
Painting
Chromic acid Cr2O3Actually Chromic acid Cr2O3 K DIchromateCr2O3
Anodizing processes
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ALTERNATE (6)
Socosurf Socomore
Etch Coventya
Isoprep 161 Mc Dermid
Novaclean Al85 Henkel
Smut Go NC Henkel
295 GD Chemetall
Pickling
Tested on following alloys:
2024, 2014, 2016, 2017A, 2214, 2219, 2618A
5056, 5086
6061, 6063
7010, 7075, 7175, 7040, 7050, 7449
AU5NKZr, A357, AS7U1G
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7175 T73 Fatigue Properties Anodizing
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2219 T8 Fatigue Properties Anodizing
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2024 T3 Fatigue Properties Anodizing
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FATIGUE PERFORMANCES (oxyde layer) thicknesse
effect)
2 nd step : SAA oxide layer thickness on forged 2214 T6 and 7050 T74 aluminium alloy
Fatigue was performed under a imposed max stress
@ Kt=1.035, R=0.1 [etching Phospho-sulfonic solution]
There is no influence of the oxide layer thickness on fatigue performance in the range of 7 to 15 µm on this aluminium alloys
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Sulfuric Acid Anodizing
SAA is a promising and cost efficient solution for CAA replacement
• Fatigue properties : equal or better than CAA
• Painted performances : class 0 before and class 0-1 after ageing
• Corrosion resistance : no pit before 500 h on sealed SAA
• Process monitoring : easy process monitoring, widespread solution
• Patent rights : none
• Waste, pollution : less constraints than actual CAA (ex. no chromate treatment)
When a higher thickness (than CAA) is design acceptable
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IF NOT ACCEPTABLE
• CORROSION / UN PAINTED APPLICATIONS
• Sulfo Tartaric (Airbus)
• Sulfo Boric (Boeing)
• Thin Film Sulfuric (SAA or DSA)
• BONDING APPLICATIONS
• Phosphoric, Sulfo phosphoric
• SAFRAN TARGETS: Have a Properties Process Specification
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ALTERNATE (6)
Chrome III salts + HTW post dip
Sol Gel sealing (Alcoa Patented Process)
Ammonium or Sodium Molybdates salts
SEALING
Co - polymeric PTFE sealing
The most promising process is Lanthane 613.3 + post dip process
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ALTERNATE (7)
Millidyne – VTT (Finland)
NTC – ICS (Germany)
Socosurf (Socomore F)
NanoOxide™ Coating – (Alcoa US)
Sol Green (Cirimat F) -
SOL GEL
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CONCLUSIONS
End of this year we should have resolved our major issues
Dip Hex C.C. on aluminium alloys replaced by dip chromium III conversion
For the whole anodizing process
Sulfo chromic bathes issue is already resolved
CAA anodizing bathes quite also
Dichromate K or Na sealing bathes also as
• Adhesion promoter
• For a high corrosion resistance of non painted parts
Other new technologies are still in progress for the next generations of
aluminium alloy protections
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QUESTIONS