Method for coating a tip of an aerofoil and aerofoil
AssigneeROLLS-ROYCE plc
InventorsAndrew HEWITT, Matthew HANCOCK
Life of this patent
Estimating the term…
Loading patent…
AssigneeROLLS-ROYCE plc
InventorsAndrew HEWITT, Matthew HANCOCK
Estimating the term…
A method (400) for coating a tip (106) of an aerofoil (100) is provided. The method (400) includes depositing a layer of nickel-based gamma/gamma prime chemistry (112) on the tip (106) of the aerofoil (100). The method (400) further includes depositing plurality of abrasive particles (114) on the layer of nickel-based gamma/gamma prime chemistry (112) to form a coating matrix (116). The method (400) further includes heating the tip (106) of the aerofoil (100) at a predetermined temperature in order to perform heat treatment of the coating matrix (116) and increase the strength of the coating (110) on the tip (106) of the aerofoil (100).
A method for coating a tip of an aerofoil for a gas turbine engine, the method comprising:
An aerofoil for a gas turbine engine, the aerofoil comprising:
Dependencies are inferred from the claim text.