Cold spray duct for a gas turbine engine
Abstract:
A component for a turbine engine may be formed by spraying particulate with a nozzle toward a substrate. The particulate may be deposited to form one or more annular layers and a reinforcing structure. The component may be a closed loop annular component having a reinforcing structure of specific dimensions enabled by the methods described.
Public/Granted literature
Information query
Patent Agency Ranking
0/0