Method of making a piece of metal reinforcement

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United States of America Patent

PATENT NO 9120189
SERIAL NO

13978809

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Abstract

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The invention provides a method of making a piece of metal reinforcement for mounting on the leading or trailing edge of a composite turbine engine blade, the method comprising the steps consisting in positioning two metal sheets (1) on either side of a core (2), in shaping the sheets (1) on the core (2) by hot isostatic compression, and in cutting the sheets (1) in order to separate the reinforcement along at least one line of cut and in order to release the core. The core (2) has projecting sacrificial zones (13), with the sheets (1) being cut along the sacrificial zones (13) without degrading the remainder of the core (2).

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Patent Owner(s)

Patent OwnerAddress
SAFRAN AIRCRAFT ENGINES75015 PARIS

International Classification(s)

Inventor(s)

Inventor Name Address # of filed Patents Total Citations
Franchet, Jean-Michel Patrick Maurice Paris, FR 38 138
Klein, Gilles Charles Casimir Mery sur Oise, FR 30 124
Leconte, Gilbert Michel Marin Ozoir la Ferriere, FR 10 53
Magnaudeix, Dominique Yerres, FR 18 100

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