TOOL AND METHOD FOR MOLDING A DUCT FOR AN AIRCRAFT TURBINE ENGINE

Abstract: a tool is configured for molding a duct for an aircraft turbine engine, wherein the duct is made of a fiber-based composite material and includes a curved tubular portion, one end of which is connected to a peripheral flange. the tool has a base and a generally elongate and curved body. the body is formed by an assembly of first parts which are fitted tightly together and which include a first central release key which extends from one end of the body to the other and which is configured to be removed first upon release of the body.

Inventor(s): Steven Gérard Joseph BIENVENU

CPC Classification: F01D25/24 (Casings (modified for heating or cooling ); Casing parts, e.g. diaphragms, casing fastenings (casings for rotary machines or engines in general {; special arrangements in stators dealing with breaking-off of part of rotor }))

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