METHOD FOR MAKING A METAL REINFORCEMENT FOR A TURBINE ENGINE BLADE

The present invention relates to a method for making a metal reinforcement (30) for the leading edge or trailing edge of a turbine engine blade, comprising in sequence: a step (44) for positioning a preform (26, 70) by means of equipment (60) positioning said preform (26, 70) in a position such that...

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Hauptverfasser: MAROLLE, PHILIPPE, LEVEQUE, STEPHANE ANDRE, FLESCH, THIERRY, JEAN, EMILE, CATTIEZ, BERNARD, JOSE, MICHEL, GUINOIS, JEROME
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creator MAROLLE, PHILIPPE
LEVEQUE, STEPHANE ANDRE
FLESCH, THIERRY, JEAN, EMILE
CATTIEZ, BERNARD, JOSE, MICHEL
GUINOIS, JEROME
description The present invention relates to a method for making a metal reinforcement (30) for the leading edge or trailing edge of a turbine engine blade, comprising in sequence: a step (44) for positioning a preform (26, 70) by means of equipment (60) positioning said preform (26, 70) in a position such that said preform (26, 70), at one end thereof, has an area (28, 72) which is capable of receiving a filler metal; and a step (46) for constructing a base (39) for said metal reinforcement (30) by hard-surfacing with filler metal in said area (28), in the form of metal beads. La présente invention concerne un procédé de réalisation d'un renfort métallique (30) de bord d'attaque ou de bord de fuite d'aube de turbomachine comportant successivement: - une étape (44) de positionnement d'une préforme (26, 70) au moyen d'un outillage (60) positionnant ladite préforme (26, 70) dans une position de sorte que ladite préforme (26, 70) présente à une extrémité une zone (28, 72) apte à recevoir du métal d'apport; - une étape (46) de construction d'une base (39) dudit renfort métallique (30) par rechargement de métal d'apport dans ladite zone (28), sous la forme de cordons de métal.
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and a step (46) for constructing a base (39) for said metal reinforcement (30) by hard-surfacing with filler metal in said area (28), in the form of metal beads. La présente invention concerne un procédé de réalisation d'un renfort métallique (30) de bord d'attaque ou de bord de fuite d'aube de turbomachine comportant successivement: - une étape (44) de positionnement d'une préforme (26, 70) au moyen d'un outillage (60) positionnant ladite préforme (26, 70) dans une position de sorte que ladite préforme (26, 70) présente à une extrémité une zone (28, 72) apte à recevoir du métal d'apport; - une étape (46) de construction d'une base (39) dudit renfort métallique (30) par rechargement de métal d'apport dans ladite zone (28), sous la forme de cordons de métal.</abstract><oa>free_for_read</oa></addata></record>
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subjects BLASTING
CLADDING OR PLATING BY SOLDERING OR WELDING
COMBINED OPERATIONS
CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINE TOOLS
MACHINES OR ENGINES IN GENERAL
MECHANICAL ENGINEERING
METAL-WORKING NOT OTHERWISE PROVIDED FOR
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
NON-POSITIVE DISPLACEMENT PUMPS
OTHER WORKING OF METAL
PERFORMING OPERATIONS
POSITIVE DISPLACEMENT MACHINES FOR LIQUIDS
PUMPS FOR LIQUIDS OR ELASTIC FLUIDS
SOLDERING OR UNSOLDERING
STEAM ENGINES
TRANSPORTING
UNIVERSAL MACHINE TOOLS
WEAPONS
WELDING
WORKING BY LASER BEAM
title METHOD FOR MAKING A METAL REINFORCEMENT FOR A TURBINE ENGINE BLADE
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