Safran Aircraft Engines

Snecma

Safran

Raoul Jaussaud

Hubert Jean Marie Fabre

Dominique Michel Serge Magnaudeix

Marc-Emmanuel Techer

Richard Mathon

Nicolas Cambyse Ashtari

Paul E Terry

Marc-Emmanuel Jean François Techer

Dominique Magnaudeix

Thierry Patrick Chauvin

Olivier Foussard

Adrien Touze

Denis Pingon

Richard Nord

Benoit Bazin

Nate Gravelle

A mold for manufacturing a turbomachine fan casing of composite material, includes a mandrel around which a fibrous preform of the fan casing is to be wound; counter-mold angular sectors assembled on the external contour of the mandrel which are intended to close the mold and to compact the fibrous preform wound on the mandrel; wherein each angular sector includes a first lateral flange positioned at the first end of the angular sectors and a second lateral flange positioned at a second end of the angular sectors, the first and second lateral flanges cooperating respectively with the second and first lateral flanges of the adjacent angular sectors. An angular sector includes a first groove formed in the first of second lateral flange, a first seal being positioned in the first groove, the first seal to be compressed between the first and second lateral flanges of two adjacent angular sectors.

Mold for manufacturing a turbine engine fan casing from a composite material

A tooling for injecting a polymer resin into a fibrous preform for the manufacture of a revolution part in composite material including a barrel shape with an inside diameter of smaller diameter delimiting the revolution part into an upstream portion and a downstream portion of the inside diameter, the upstream portion including a back-draft intermediate portion, injection tooling wherein, to allow a demolding of the barrel-shaped part once the injection and the polymerization of the polymer resin are carried out, the injection tooling includes on the one hand a frustoconical drum comprising a first drum portion in direct contact with an inner surface of the portion of the revolution part downstream of the inside diameter and a second drum portion and on the other hand a segmented insert whose outer surface matches an inner surface of the portion of the revolution part upstream of the inside diameter.

Injection tooling for barrel-shaped rotating part

Mold intended to be used for the manufacture of a gas turbine fan casing made of composite material including: a mandrel on which a fibrous preform of a fan casing is intended to be wound said preform comprising an annular wall the profile of the outer surface of which corresponds to that of the inner surface of the casing to be manufactured and two side flasks the profiles of which correspond to those of outer flanges of the casing to be manufactured; a plurality of angular counter-mold sectors assembled in a sealed manner on the mandrel and intended to close the mold and to compact a fibrous preform wound on the mandrel; and at least one compacting wedge, the wedge being placed between the fibrous preform wound on the mandrel and the associated angular counter-mold sector.

Compacting block for a fan casing mould

A method for impregnating a fibrous preform by injection or infusion, the method including the steps of providing a mold having at least two portions, said mold presenting an inlet orifice and a vent orifice placed on opposite sides of the mold; placing a fibrous preform in a portion of the mold; placing a seal in a passage formed between an inside wall of the mold and the fibrous preform, said passage extending substantially along the direction extending between the opposite sides of the mold; closing the mold so that the two portions of the mold co-operate with the seal in such a manner as to shut off said passage; and impregnating the fibrous preform with an impregnation material.

Method for impregnating a fibrous preform using a seal, and a method for manufacturing a matrix reinforced by a fibrous preform

A mold for manufacturing a turbomachine fan casing made of composite material, includes a main axis mandrel around which a fibrous preform of a fan casing is intended to be wound; a plurality of counter-mold angular sectors assembled on the outer contour of the mandrel which are intended to close the mold and to compact the fibrous preform wound on the mandrel; wherein a flat seal with a main elongation axis directed along the main axis is arranged between each angular sector, the flat seal being compressed between two adjacent angular sectors, a first angular sector including a sealing portion passing below a lower face of the flat seal while a second angular sector including a sealing portion passing above an upper face of the flat seal.

The invention relates to a resin injection regulator for a resin injection circuit in a mould for producing a composite part, in particular a turbine engine composite part, characterised in that it comprises at least one vessel which is connected to said circuit and inside of which a movable wall means can be moved in a sealed manner, said movable wall means defining in said vessel a first cavity which forms a container for accumulation of resin and is designed to be connected to at least one part of said circuit, and a second cavity which is designed to be connected to a source of pressurised fluid, said movable wall means being designed to be urged by the pressurised fluid with which the second cavity is supplied in order to exert a pressure on the resin contained in the first cavity by isolating said resin from said fluid.

Resin injection regulator, resin injection circuit and associated methods

A device for applying abradable material to a surface of an annular casing of a turbine engine, wherein the casing extends along a longitudinal axis, comprises a support equipped with first guiding means capable of guiding the support in relation to the casing in a radial direction in relation to the axis of the casing. The support is equipped with second guiding means capable of guiding the support in relation to the casing in an axial direction. The device further includes an application roller pivotally mounted in relation to the support in the axial direction and adjustment means allowing adjustment of the position of the roller in relation to the first guiding means, in the radial direction.

Device for applying abradable material to a surface of a turbine engine casing

A mold for use in fabricating a gas turbine fan casing out of composite material includes a mandrel for having wound thereon a fiber preform of a fan casing and an annular wall with an outside surface of profile corresponding to the profile of the inside surface of the casing that is to be fabricated and of two lateral rims of profiles corresponding to the profiles of outer flanges of the casing that is to be fabricated; a plurality of mold cover angular sectors that are assembled in leaktight manner on the mandrel and that are to close the mold and to compact the fiber preform wound on the mandrel; and a plurality of locking keys configured to lock together in leaktight manner neighboring mold cover sectors. A method of closing such a mold, and a method of fabricating a fan casing are included.

Mold for fabricating a turbine fan casing out of composite material, and a method of closing such a mold

A method of molding a thermosetting resin, in particular of the epoxy resin type, in which a first mold is filled with the resin while causing the temperature of the resin to vary in application of a first temperature program, without exceeding the Tg of the resin. After the first mold has been filled, the resin is put under pressure while causing the temperature of the resin to vary in application of a second temperature program, without exceeding Tg, and a drop in the pressure exerted by the resin on the mold is detected with the instant at which this pressure presents a break of slope being identified as the instant t1. A second mold is filled with the thermosetting resin in application of the first temperature program. After the second mold has been filled, the resin is put under pressure in application of the second temperature program until an instant t2 close to t1. As from t2, the temperature of the resin is increased to exceed Tg.

Process for molding a thermosetting resin

An injection tooling is configured to inject a polymer resin into a fiber preform for fabricating a part in the form of a body of revolution out of composite material, the part having an internal cavity with back-draft. In order to enable the part to be unmolded after the polymer resin has been injected and polymerized, the tooling includes, arranged at least in the internal cavity, firstly a sectorized ring made up of at least three mutually touching inserts including one forming a keystone, the ring having an outside surface that matches the internal cavity with back-draft and an inside surface that presents natural draft, and secondly a conical drum secured to the inside surface of the sectorized ring to support it and that is withdrawn, once separated from the sectorized ring, relying on the natural draft created by the inside surface of the sectorized ring.

Method for demoulding a composite material with an organic matrix

A mold () comprising a plurality of blocks () that, in an assembled position, define a mold cavity, the mold being characterized in that it includes at least one pusher (), said pusher () being configured to be housed in a first block () of said plurality, in a side facing the mold cavity, and, when the pusher () is housed in said first block (), to present a first surface (S) flush with the mold cavity, and in that the mold () also includes actuator means () enabling the pusher () to be moved relative to the first block (), and sealing means () configured to isolate the actuator means () from the mold cavity. An associated molding method.

Mould, particularly injection mould, and injection moulding method using such a mould

The invention provides an injection mold core () for making a composite material part having a closed box, the core being in the shape of a wedge that is to be inserted inside a closed box () of at least one fiber preform into which a matrix-precursor fluid is to be injected, the core presenting both an opening right section () through which the core is to be unmolded from the box of the preform after the matrix has set, and also a maximum right section () of greater size than the opening right section, the core comprising at least three distinct elements () that are assembled together, each core element presenting a maximum right section of size that is smaller than the opening section.

Growing community of inventors

Moissy-Cramayel, France

Raoul Jaussaud