ADDITIVE MANUFACTURING METHOD FOR MAKING COMPLEX FILM HOLES

ADDITIVE MANUFACTURING METHOD FOR MAKING COMPLEX FILM HOLES

A method of forming a cooling hole structure on a turbine component. The turbine component has a component wall with inner and outer surfaces. A bore passes through the component wall and fluidly connects the inner surface and the outer surface. The method includes the steps of: A) forming a recess...

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1. Verfasser: BUNKER, RONALD SCOTT
Format: Patent
Sprache:eng ; fre
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ADDITIVE MANUFACTURING TECHNOLOGY
ADDITIVE MANUFACTURING, i.e. MANUFACTURING OFTHREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVEAGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING,STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
BLASTING
CASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MAKING METALLIC POWDER
MANUFACTURE OF ARTICLES FROM METALLIC POWDER
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
PERFORMING OPERATIONS
POWDER METALLURGY
STEAM ENGINES
TRANSPORTING
WEAPONS
WORKING METALLIC POWDER
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description A method of forming a cooling hole structure on a turbine component. The turbine component has a component wall with inner and outer surfaces. A bore passes through the component wall and fluidly connects the inner surface and the outer surface. The method includes the steps of: A) forming a recess communicating with the bore and the outer surface; and B) using an additive manufacturing process to form an exit region in the recess. Une méthode servant à former la structure dun trou de refroidissement pour une composante de turbine. La composante de turbine comprend un mur de composantes ayant une surface interne et une surface externe. Un orifice de passage traverse le mur de composantes et fournit une connexion fluidique entre la surface interne et la surface externe. La méthode comprend les étapes suivantes : a) former une cavité qui touche lorifice de passage ainsi que la surface externe; b) utiliser un procédé de fabrication additive pour former une région de sortie dans la cavité.
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A bore passes through the component wall and fluidly connects the inner surface and the outer surface. The method includes the steps of: A) forming a recess communicating with the bore and the outer surface; and B) using an additive manufacturing process to form an exit region in the recess. Une méthode servant à former la structure dun trou de refroidissement pour une composante de turbine. La composante de turbine comprend un mur de composantes ayant une surface interne et une surface externe. Un orifice de passage traverse le mur de composantes et fournit une connexion fluidique entre la surface interne et la surface externe. 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subjects ADDITIVE MANUFACTURING TECHNOLOGY
ADDITIVE MANUFACTURING, i.e. MANUFACTURING OFTHREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVEAGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING,STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
BLASTING
CASTING
ENGINE PLANTS IN GENERAL
HEATING
LIGHTING
MACHINES OR ENGINES IN GENERAL
MAKING METALLIC POWDER
MANUFACTURE OF ARTICLES FROM METALLIC POWDER
MECHANICAL ENGINEERING
NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES
PERFORMING OPERATIONS
POWDER METALLURGY
STEAM ENGINES
TRANSPORTING
WEAPONS
WORKING METALLIC POWDER
title ADDITIVE MANUFACTURING METHOD FOR MAKING COMPLEX FILM HOLES
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