RTM injection method and mould using symmetric anti-pinching sectors

Patent metadata

Field	Value
Publication number	US-12552114-B2
Application number	US-202118000482-A
Country	US
Kind code	B2
Filing date	May 26, 2021
Priority date	Jun 4, 2020
Publication date	Feb 17, 2026
Grant date	Feb 17, 2026

Abstract

An injection mold for the manufacture of an axisymmetric part of composite material comprising a mandrel supporting a fibrous preform and comprising an annular wall, and a plurality of counter-mold angular sectors assembled to the mandrel and intended to close the mold and to compact the fibrous preform wound on the mandrel. Each angular sector comprises an annular base intended to come into contact with the fibrous preform. The plurality of angular sectors includes a first series of angular sectors and a second series of angular sectors, first and second lateral edges of the first series of sectors each including a protruding lower portion, the first and the second lateral edges of the second series of sectors each including a recessed lower portion.

First claim

The invention claimed is:

1 . An injection mold for the manufacture of an axisymmetric part of composite material comprising:
a mandrel configured to support a fibrous preform formed by winding, the mandrel comprising an annular wall having an outer surface and an inner surface, a profile of the outer surface corresponding to a profile of the inner surface of the part to be manufactured, a plurality of counter-mold angular sectors assembled on the mandrel and intended to form the mold and to compact the fibrous preform wound on the mandrel, each angular sector comprising:
an annular base intended to come into contact with the fibrous preform, the annular base extending between first and second longitudinal edges in an axial direction and between first and second lateral edges in a circumferential direction,
the first lateral edge of the annular base of one of the angular sectors being in contact with the second lateral edge of the annular base of the adjacent angular sector,
wherein the plurality of angular sectors comprises a first series of angular sectors and a second series of angular sectors, the first and second lateral edges of each angular sector of the first series of sectors each including a protruding lower portion forming a first nonzero angle relative to a radial direction, the first and second lateral edges of each angular sector of the second series of sectors each including a recessed lower portion forming a second nonzero angle relative to a radial direction, the first angle and the second angle having the same extent, wherein the plurality of angular sectors further includes a first lateral face parallel to the radial direction and present in the continuation of the first lateral edge of each angular sector, and a second lateral face parallel to the radial direction and present in the continuation of the second lateral edge of each angular sector.

2 . The injection mold according to claim 1 , wherein each angular sector includes a first groove and a second groove present respectively on the first lateral face and the second lateral face, the first groove and the second groove extending in the axial direction, a gasket being housed between the first groove of the first lateral face of the angular sector and the second groove of the second lateral face of the adjacent angular sector.

3 . The injection mold according to claim 1 , wherein the first nonzero angle relative to the radial direction formed by the protruding lower portion of the first and second lateral edges of an each angular sector of the first series of sectors is between 18° and 45°.

4 . A method of closing an injection mold for the manufacture of an axisymmetric part of composite material, the mold comprising:
a mandrel supporting a fibrous preform obtained by winding a fibrous strip, the mandrel comprising an annular wall having an outer surface and an inner surface, a profile of the outer surface corresponding to a profile of the inner surface of the part to be manufactured, a plurality of angular sectors comprising an annular base intended to come into contact with the fibrous preform, the annular base extending between first and second longitudinal edges in an axial direction and between first and second lateral edges in a circumferential direction, wherein the plurality of angular sectors each comprises a first series of angular sectors and a second series of angular sectors, the first and second lateral edges of each angular sector of the first series of sectors each including a protruding lower portion forming a first nonzero angle relative to a radial direction, the first and second lateral edges of each angular sector of the second series of sectors each including a recessed lower portion forming a second nonzero angle relative to a radial direction, wherein the plurality of angular sectors further includes a first lateral face parallel to the radial direction and present in the continuation of the first lateral edge of each angular sector, and a second lateral face parallel to the radial direction and present in the continuation of the second lateral edge of each angular sector, the first angle and the second angle having the same extent and wherein the method comprises successive positioning and attachment of each angular sector on the mandrel, the annular base of each sector compacting the fibrous preform portion facing the annular base, the lateral edges of the annular base of an angular sector of the first series of sectors during positioning being held in contact with the lateral edges of the annular base of the angular sectors of the second series of sectors already attached to the mandrel.

5 . The method according to claim 4 , wherein the angular sectors of the second series of sectors are first positioned and fixed on the mandrel at a predetermined distance from one another so as to provide a space between two angular sectors of the second series of sectors, the angular sectors of the first series of sectors then being positioned and attached to the mandrel in the spaces provided between the angular sectors of the second series of sectors.

6 . The method according to claim 4 , wherein the first nonzero angle relative to the radial direction formed by the protruding lower portion of the first and second lateral edges of an each angular sector of the first series of sectors is between 18° and 45°.

Assignees

• Safran Aircraft Engines

Inventors

• Jaussaud Raoul
• Fabre Hubert Jean Marie
• Jensen Brian

Classifications

• B29L2031/7504

  Turbines · CPC title

• B29C70/48

  and impregnating the reinforcements in the closed mould, e.g. resin transfer moulding [RTM] {, e.g. by vacuum} · CPC title

• B29K2995/0094

  Geometrical properties · CPC title

• B29C33/306

  Exchangeable mould parts, e.g. cassette moulds, mould inserts (moulds with exchangeable mould parts for injection moulding B29C45/2673; mounting of exchangeable mould inserts for injection moulding B29C45/2675) · CPC title

• B29C33/22

  by rectilinear movement · CPC title