Method for producing a metal reinforcement for a turbine engine blade
AssigneeSnecma
InventorsBernard José Michel Cattiez, Thierry Jean Emile Flesch, Jérôme Guinois, Stéphane André Leveque, Philippe Marolle
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Abstract
A method for making a metal reinforcement for the leading edge or trailing edge of a turbine engine blade, including: positioning a preform using an equipment positioning the preform in a position such that the preform, at one end thereof, has an area which is capable of receiving a filler metal; and, after the positioning, constructing a base for the metal reinforcement by hard-surfacing with filler metal in the area, in the form of metal beads.
Claims14
A method to produce a metal reinforcement for a leading edge or a trailing edge of a turbine engine blade, the method comprising:
- positioning a preform using an equipment that positions said preform in a position such that said preform presents, at one end, an area which is capable of receiving a filler metal;
- subsequent to said positioning, constructing a base for said metal reinforcement by hard-surfacing with filler metal in said area, in the form of metal beads.
Dependencies are inferred from the claim text.