Process for manufacturing a one-piece axisymmetric metallic part from composite fibrous structures
View Patent ↗A process for manufacturing a one-piece axisymmetric part includes: superposition, around a rotating cylindrical mandrel of at least respectively inner and outer metal-coated composite fibrous structures, wound in first and second crossed directions on the mandrel; arranging, between the crossed inner and outer fibrous structures, at least one layer of metallic wire; then placing a blank of the part, formed by the fibrous structures and the layer of metallic wire, in a tool to apply to the blank a hot isostatic pressing treatment, and to obtain the part.
1. A method for manufacturing an integral rotationally symmetrical part by superposition, around a rotary cylindrical mandrel, of at least two metal-coated composite fibrous structures, respectively inner and outer, wound in first and second winding directions crossed on the mandrel, the method comprising:
winding the inner fibrous structure around the mandrel, fibers of the inner fibrous structure being arranged in the first winding direction;
arranging a first layer of metal wire around the inner fibrous structure constructed on the mandrel;
winding the outer fibrous structure around the first layer of wire such that the first layer of metal wire is arranged between the inner fibrous structure and the outer fibrous structure, fibers of the outer fibrous structure being arranged in the second winding direction different from the first winding direction;
placing a preform of the part, formed by the fibrous structures and the layer of metal wire, in a receiving outfit;
applying a hot isostatic compaction or isothermal forging treatment to the preform placed in the receiving outfit; and
extracting a treated preform from the outfit.
2. The method as claimed in claim 1 , wherein the metal wire is obtained by wire drawing.
3. The method as claimed in claim 1 , wherein the superposed winding layers of the metal wire and of the fibrous structures are made cold, at ambient temperature.
4. The method as claimed in claim 1 , wherein the layer of metal wire is wound substantially orthogonally to the longitudinal axis of the rotary cylindrical mandrel.
5. The method as claimed in claim 1 , wherein a second layer of metal wire, on which the inner fibrous structure is subsequently wound, is arranged around the cylindrical mandrel, before the winding the inner fibrous structure.
6. The method as claimed in claim 1 , wherein a third layer of metal wire is arranged around the outer fibrous structure.
7. The method as claimed in claim 1 , wherein the first winding direction of the inner fibrous structure is oriented at an angle relative to the longitudinal axis of the cylindrical mandrel, the second winding direction of the outer fibrous structure being oriented symmetrically to the first relative to a direction at right angles to the longitudinal axis of the mandrel.
8. The method as claimed in claim 7 , wherein the inner and outer fibrous structures are in a form of individual and parallel fibers wound in succession around the mandrel, or in a form of laps or strips of parallel fibers, or in a form of fabrics of parallel fibers, the structures being arranged crossed on the mandrel.
9. The method as claimed in claim 1 , wherein the first winding direction of the inner fibrous structure is parallel to the longitudinal axis of the cylindrical mandrel, the second winding direction of the outer fibrous structure being oriented at an angle relative to the longitudinal axis of the mandrel.
10. The method as claimed in claim 9 , wherein the inner fibrous structure is in a form of a fabric of mutually parallel fibers wound around the cylindrical mandrel parallel to its longitudinal axis, the outer fibrous structure having the fibers oriented at an angle relative to those of the inner structure which are parallel to the mandrel.