Method for producing a protective reinforcement for a blade (P) having a curved leading edge or trailing edge
AssigneeSafran Aircraft Engines
InventorsRemi Philippe Guy Onfray, Maxime Briend, Didier Pelletier
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AssigneeSafran Aircraft Engines
InventorsRemi Philippe Guy Onfray, Maxime Briend, Didier Pelletier
Estimating the term…
The invention proposes a method for producing a protective reinforcement for the leading edge (BA) or trailing edge of a blade (P), the leading edge (BA) or trailing edge being curved, the method comprising steps of flattening (102) a hollow tube (1) so as to form at least one fold line (6) extending along the tube (1), opening (104) the flattened tube (1) by cutting the tube (1) along a cutting line (8) opposite the fold line (6) with respect to the tube (1), so as to form two flanks (16, 18) linked at the fold line (6) and intended to be mounted on the pressure side and the suction side of the blade (P), the method being characterised by a preliminary step (100) of bending the hollow tube (1) carried out before the flattening (102) and adapted such that the fold line (6) after flattening (102) is curved and substantially matches the curved leading edge (BA) of the blade (P).
A method for manufacturing a protective reinforcement of a leading (BA) or trailing edge of a blade (P), wherein the leading (BA) or trailing edge is curved, wherein the method comprises:
Dependencies are inferred from the claim text.