Aerospatiale Societe Nationale Industrielle

Societe Nationale Industrielle Et Aerospatiale

Societe Nationale Industrielle Aerospatiale

Mbda France

Astrium Sas

Societe Anonyme Dite: Aerospatiale Societe Nationale Industrielle

Eads Launch Vehicles

Vostech B.v.

Eads Space Transpotation Sa

Aerospatiale Societe Nationale Ind.

Chomarat Textiles Industries

Cahuzac, Georges

Georges J Cahuzac

Francois J Monget

Lucien Fantino

Jean-Louis Darrieux

Jean Banos

Francedillaois Jean Monget

Jean-Claude Cantagrel

Marc Bouchez

François Falempin

Etienne Lemaire

Jack Gauthier

Laurent Sabary

Jean-Marc Jacques Dupillier

Bernard Andre Jollivet

Jean-Claude Baudry

Bruno Dubearn

Patrick Georges DeCraecker

Thierry Salmon

Eric Chocheyras

Thomas Roure

A triaxial textile armature is provided for making composite materials. The armature includes a central layer of axial yarns cross-linked by bias yarns extending in a first and a second direction the bias yarns extending in the first direction passing through the central layer of axial yarns in even intervals between axial yarns of the central, and the bias yarns extending in the second direction passing through the central layer of axial yarns in odd intervals.

Triaxial textile armature, process for producing triaxial textile armatures and composite material part

A reinforcement insert includes superposed laps of fiber which are coupled to each other by a coupling fiber which passes through the laps in order to form fiber sections wherein at least certain sections thereof are rectilinear. The fiber sections and laps are immersed in a cured resin. The total density of the fibers that make up the insert ranges from 50% to 60% of the volume of the insert and the fiber sections take up 3%-10% of the volume of the insert. A method for creating a sandwich structure includes at least one such insert.

Composite material insert and method for the production thereof, and method for creating a sandwich structure comprising said insert

A method of producing a double-walled thermo-structural composite monolith may include assembling, by stitching, a sandwich having a core and outer fibrous armors. The stitched sandwich structure is impregnated with a viscous resin. After the resin hardens, the core is removed from the sandwich structure.

Method for making a double-walled thermostructural composite monolithic component and resulting component

A weaving device for the production of thick textile armatures constituted by superposed layers of threads secured together by a binding thread traversing the layers, includes a frame provided laterally and at its periphery with regularly distributed hooking pins, elements for depositing with the aid of the pins, thread and elements for flattening the layers. The pins have a first section with a slight inclination outwardly of the frame and a second straight section prolonging the first and having an a substantially greater inclination outwardly of the frame. The elements for depositing thread include a plurality of guides each supplying a thread, and are moved simultaneously and spaced at an interval equal to n times the interval between pins. The elements for weaving the layers include elements adapted to press the assembly of the layers about their periphery.

Weaving device for the production of thick textile armatures and armatures thus obtained

The present invention relates to a connecting rod made of composite material, especially for internal-combustion engines, the composite material being formed by a reinforcement embedded in a cured material, and the connecting rod (A) comprising, along the longitudinal extension (X&mdash;X) of the connecting rod, a central shank (B) extended respectively, at its two ends, by a connecting-rod big end (C) and a connecting-rod small end (D). According to the invention, the connecting rod (A) is produced entirely as a single component made of composite material and the reinforcement of the composite material comprises superposed plies of crossed straight filling yarns, the filling yarns, which extend parallel to the longitudinal extension (X&mdash;X) of the connecting rod (A), constituting at least twice the volume percentage of the filling yarns which extend in each of the directions other than the longitudinal extension (X&mdash;X) of the connecting rod (A), and binding yarns pass through the superposed plies.

Connecting rod made of composite material

The present invention relates to the production of a reinforcement for a composite component, comprising a fibrous substrate (22, 23) reinforced by a stitching thread forming stitches (27.1, 27.2; 30.1, 30.2; 33.1, 33.2 and 36.1, 36.2) passing through said substrate. According to the invention, said stitches are oblique and pass through said substrate slantwise, making an angle of inclination of at most 30.degree.. It is advantageous for said fibrous substrate to consist of plies of crossed threads (22, 23) defining mesh cells (24) through which said stitches pass.

Fibrous reinforcement for a composite component, and process and device

The manufacture of a fibrous structure (1) for a composite material part. At least one portion (3) of the fibrous structure (1) is obtained by at least partial machining of a fibrous blank stiffened by freezing a liquid impregnating the blank.

Method of manufacturing a fibrous structure for a composite fiber-matrix

A method of making a connecting rod made of composite material, especially for internal-combustion engines, the composite material being formed by a reinforcement embedded in a cured material, and the connecting rod (A) comprising, along the longitudinal extension (X-X) of the connecting rod, a central shank (B) extended respectively, at its two ends, by a connecting-rod big end (C) and a connecting-rod small end (D). The connecting rod (A) is produced entirely as a single component made of composite material and the reinforcement of the composite material comprises superposed plies of crossed straight filling yarns, the filling yarns, which extend parallel to the longitudinal extension (X-X) of the connecting rod (A), constituting at least twice the volume percentage of the filling yarns which extend in each of the directions other than the longitudinal extension (X-X) of the connecting rod (A), and binding yarns which pass through the superposed plies.

Method of manufacturing a connecting rod made from composite material

Weaving device for producing a woven structure which is intended for the production of a composite component, including especially a component (5) for generating different speeds of movement for at least some of the warp yarns (FC). Component (5) includes a substantially plane profiled cam (5) capable of rotating about a longitudinal axis (X--X) and arranged so that the longitudinal axis (X--X) is approximately orthogonal to the direction (D) defined by the warp yarns (FC). The profile of the cam is defined by a variable transverse length (h) perpendicular to the longitudinal axis (X--X).

Weaving device for the production of a structure for a composite

The present invention relates to a method and to a system for producing a reinforcement for a composite component, formed by said reinforcement embedded in a cured matrix, said reinforcement comprising superposed plies of thread. According to the invention, the system comprises means (5) for the memory storage and processing of data, in which means the mathematical model of the reinforcement (A) to be produced may be created and stored in memory and which are capable of controlling means (3) for steering the tool (1) for laying down and/or stitching thread (F).

Method and system for producing a reinforcement for a composite component

The invention relates to a method for producing a reinforcement in the form of a sheet for a composite component, the reinforcement including superposed plies of thread. In accordance with the method, straight portions of thread are arranged, for each ply, at least substantially in a parallel fashion with respect to each other and all the superposed plies are consolidated by using a thread passing through the plies. According to the invention, the superposed plies are laid down on a support, the superposed plies are compacted by mechanical pressure, and in order to preserve the state of compaction of the plies which is thus obtained, the thread for consolidating the plies is stitched, without knotting, through the plies down to at least the level of the surface of the support, the plies having, after compaction, a density of the portions of the thread constituting them which is sufficient to retain the consolidating thread by friction.

Method for producing a reinforcement in the form of a sheet for a

The present invention relates to a method and a machine for producing a reinforcement in the form of a block for a composite component formed by said reinforcement embedded in a cured matrix. According to the invention, said block (B) is made up by continuously forming a succession of superposed sheets, and the machine, comprising a stand provided with a subframe and with uprights for mounting at least one frame which can move along said uprights, capable of receiving a thread laying-down tool which can move in a plane transverse to said uprights, is noteworthy in that it comprises an additional frame (6) which can move along said uprights (4) and is provided with pegs (9) for hooking on said straight portions of thread (F).

Method for producing a reinforcement in the form of a block for a

Machine is provided for the simultaneous laying down/winding of a plurality of rovings, including a gantry supporting a laying down/winding head carrier mechanism plate movable along the X,Y,Z directions, at least one laying down/winding head rotatably mounted on the mechanism plate around at least one vertical axis and comprising a laying down/winding roller, a mechanism for presenting on the roller rovings along at least two tangent laps, selective mechanisms for driving and cutting each roving, and spools delivering the rovings. The spools are mounted on a fixed creel and the rovings are guided between the creel and the head by sets of return pulleys disposed in such a way as to limit the surface scanned by the rovings and reduce the jerks of the roving reeling speed. The machine is especially adapted for production of composite structures.

Machine for the simultaneous laying down and winding of a plurality of

A machine for producing a reinforcement for a composite component. The machine includes a stand with a subframe having uprights with slideways for mounting a transverse bar on which is mounted a movable carriage. The carriage has a first movable arm extending in another direction and includes a second movable arm. The carriage is movable in a first direction, X, the first arm is movable in a second direction, Y, orthogonal to the first, and the second arm is movable transversely with respect to the plane defined by the bar and first arm in a third, Z, direction. Motors are provided to producing such movements. The second arm includes a thread-stitching tool which also constitutes a tool for laying down the thread and is mounted on a rotary support at the lower end of which is arranged the needle.

Machine for producing a reinforcement for a composite component

The present invention relates to a method for producing a reinforcement for a composite component, said reinforcement including superposed plies of thread, according to which method:

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Le Bouscat, France

Georges J Cahuzac