Protection of components from corrosion
AssigneeApplied Materials, Inc.
InventorsDavid Britz, Pravin K. Narwankar, David Thompson, Yuriy Melnik, Sukti Chatterjee
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AssigneeApplied Materials, Inc.
InventorsDavid Britz, Pravin K. Narwankar, David Thompson, Yuriy Melnik, Sukti Chatterjee
Estimating the term…
Using the systems and methods discussed herein, CMAS corrosion is inhibited via CMAS interception in an engine environment and/or is prevented or reduced by the formation of a metal oxide protective coating on a hot engine section component. The CMAS interception can occur while the engine is in operation in flight or in a testing or quality control environment. The metal oxide protective coating can be applied over other coatings, including Gd-zirconates (GZO) or yttria-stabilized zirconia (YSZ). The metal oxide protective coating is applied at original equipment manufacturers (OEM) and can also be applied in-situ using a gas injection system during engine use in-flight or during maintenance or quality testing. The metal oxide protective coating contains a rare earth element, aluminum, zirconium, chromium, or combinations thereof and can have a thickness from 1 nm to 3,000 nm.
A multilayered coating structure, comprising:
A multilayered coating structure, comprising:
A multilayered coating structure, comprising:
A multilayered coating structure, comprising:
Dependencies are inferred from the claim text.