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COBALT CHROMIUM PLATING KIT PORTABLE

to 0.0008 in.) thickness of AeroNikl® 250 7280 for prebraze at the repair facility.

TURBINE STATOR: Inner and outer stator and seal diameters are plated with 5µm to 20µm (0.0002 in.

The SIFCO Process is approved by multiple primes, including Bell, Sikorsky, Boeing and more. Find out more about 6 real-life applications of critical aerospace repairs here. Selective anodizing touch-up is also offered for OEM applications. Repair applications can replace worn or damaged coatings with a new anodizing seal. MRO applications use nickel or sulfamate nickel for dimensional restoration of an inside or outside diameters of the component. OEM applications use nickel or a nickel alloy to improve hardness and wear resistance of the component. In the case of exotic alloys, such as Renes and Inconels, selective plating is the preferred method of pre-brazing. Selective plating for pre-braze also provides an atomic bond and superior wettability as compared with nickel shot blasting. Compared to other methods of applying the intermediate nickel layer, selective plating is faster, more consistent, and more cost effective. Turbine blades, turbine vanes, turbine stators and frames are nickel plated to ensure proper wetting of the surfaces to be brazed.

COBALT CHROMIUM PLATING KIT PORTABLE

SIFCO ASC offers portable touch-up kits for AOG repairs of cadmium, nickel, zinc-nickel, and tin-zinc. This is where on-site touch up coatings for corrosion protection with Cadmium LHE®, Cadmium No Bake and Zinc-Nickel LHE® can make a real impact. To help you save on downtime, being able to make repairs in place and with minimum to no disassembly required is key. Here are five common uses of selective and brush plating found in aerospace manufacturing and repair:

AeroNikl® – a sulfamate nickel which provides a defect-free, adherent, high quality nickel deposit that is available in three hardness levels (250, 400, and 575 Hv).Ĭommon Aerospace Manufacturing Process Applications.Cobalt Chromium Carbide provides superior wear resistance and high temperature oxidation protection on engine components.Type I, II and III anodizing touch-up coatings are used to process components of engines, actuators, landing gear and airframes, increasing their ability to perform and extending overall in-service life.Zinc-Nickel and other alloys are available as alternatives to cadmium coatings.Cadmium coatings for corrosion protection are available as LHE® (Low Hydrogen Embrittlement) formulations that do not require post-baking.Nickel is used for pre-braze operations, wear resistance, dimensional restoration and corrosion protection.

Common deposits utilized in aerospace manufacturing repair: