Metallic-coated polymer thrust reverser cascades
Abstract:
A thrust reverser cascade for a gas turbine engine is disclosed. The thrust reverser cascade may comprise a plurality of turning vanes. One or more of the turning vanes may comprise a core formed from a polymer and a metallic coating applied to at least a portion of an outer surface of the core. The metallic coating may comprise nickel or a nickel alloy.
Public/Granted literature
Information query
Patent Agency Ranking
0/0