Applications for Aerospace Components
Without question, high performance equipment is a necessity in the aerospace industry. Aerospace components need to be able to withstand friction, high temperatures and corrosive environments while continuing to operate at optimum levels.
SIFCO ASC works closely with you to offer practical, cost-effective options for repairing and enhancing the surfaces of your components. The technologies offered are utilized on OEM components to enhance performance and on MRO components in need of refurbishment.
See our video – The SIFCO Process® for Aerospace
Deposits utilized on aerospace components include:
- Nickel for pre-braze operations, wear resistance, dimensional restoration and corrosion protection.
- Cadmium coatings for corrosion protection are available as LHE® (Low Hydrogen Embrittlement) formulations that do not require post-baking.
- Zinc-Nickel and other alloys are available as alternatives to cadmium coatings.
- Type I, II and III Anodizing coatings used to process components of engines, actuators, landing gear and airframes, increasing their ability to perform and extending overall in-service life.
- Cobalt Chromium Carbide provides superior wear resistance and high temperature oxidation protection on engine components.
- AeroNikl sulfamate nickel provides defect-free, adherent, high quality nickel deposits in three hardness levels (250, 400, and 575 Hv).
Common Process Applications
On-site touch up coatings for corrosion protection with LHE® and No Bake® Cadmium and Zinc-Nickel LHE™ (low hydrogen embrittlement) allow repairs to be made in place and with minimum to no disassembly required.
Turbine blades, turbine vanes, turbine stators and frames are nickel plated to ensure proper wetting of the surfaces to be brazed. Compared to other methods of applying the intermediate nickel layer, selective plating, is faster, more consistent, and more cost effective.
OEM applications use nickel or a nickel alloy to improve hardness and wear resistance of the component.
MRO applications use nickel or sulfamate nickel for dimensional restoration of an inside or outside diameter on the component.
Repair applications replace worn or damaged hardcoat with a new, anodized hardcoat coating.
Application Examples for Aerospace Components
- TURBINE STATOR: Inner and outer stator and seal diameters are plated with 5µm to 20µm (0.0002 in. to 0.0008 in.) thickness of AeroNikl 250 (Code 7280) for prebraze at the repair facility. The ability to selectively apply the prebraze deposit in-house, without the need for immersion tanks saves time, money and minimizes any potential environmental issues associated with large tank plating operations.
- TURBINE FRAMES: These components have been plated with 5µm to 15µm (0.0002 in. to 0.0006 in.) thickness of AeroNikl 250 (Code 7280) for prebraze on a contract basis by SIFCO ASC for over 5 years, providing a quick turnaround time for the customer. These parts were originally tank plated and required an extensive and time consuming masking operation. The use of selective plating on these parts has eliminated the need for complicated masking and significantly reduced the turnaround time for each part.
- TURBINE BLADES: SIFCO ASC’s Contract Service Department has processed well over 11,000 OEM second stage blades, which previously were tank plated. Utilizing selective plating for this prebraze application provided considerable savings to the customer and a much faster turnaround time.
- COMPRESSOR SPACERS AND TORQUE CONE FLANGES: Repair of worn bolt holes with a nickel buildup of 125µm (0.005 in.) using product code 2088. This material was selected because it matches the hardness of the substrate material.
- LANDING GEAR: Touch-up with Cadmium LHE® and Cadmium No Bake® for corrosion protection can be done at the customer site, saving disassembly cost.
- MAIN LANDING GEAR OUTER CYLINDER: CVGP (Controlled Velocity Gap Plating) has made it possible for orifice tube boss ID’s to be repaired with thicknesses ranging from 250µm to 750µm (0.010 to 0.030 in.), with a tolerance range of 50µm (0.002 in.). Deposits of 750µm (0.030 in.) can be applied in approximately two hours. Tank plating, for the same repair, requires the part to be immersed for extended periods (24 to 72 hours is common) for the required deposit thickness. Machining is then required because of the excessive edge build-up. Immersion tank plating requires very time consuming and careful masking.
Plating on Titanium
The SIFCO Process® enables you to selectively plate deposits onto Ti 6-4 and Ti 6-6-2 to improve the surface properties of localized areas on aerospace components for either OEM or repair applications. The technology optimizes the adhesion of the deposit to titanium alloys by effective removal of titanium’s passive oxide and micro-roughening to increase surface area.
This micrograph shows a Ti 6-4 Grade 5 base plated with 0.0014″ of nickel, followed by 0.014″ of copper that is capped with 0.0023″ of nickel. Selective plated deposits consistently meet the adhesion requirements of AMS 2451 and ASTM B 571 (bend test method), with no hydrogen embrittlement per GM 3661P. Additionally, selective plated deposits exhibit adhesion in excess of 6000 psi in tensile pull tests.
Specific deposits can be selectively plated to a precise thickness to meet your engineering requirements.
With an adherent base layer of nickel, many additional deposits can be selectively plated to a precise thickness for:
These additional deposits include: soft and hard nickels, copper, tin, zinc, silver, gold, and platinum.