Abstract: The invention pertains to a composite part with a fibrous reinforcement and a thermoplastic polymer matrix, comprising: substrate part with a matrix of a first thermoplastic polymer having a first melting temperature; stiffener made of a composite material with a matrix of a second thermoplastic polymer having a second melting temperature; comprising the steps of: obtaining an unconsolidated preform of the substrate part; obtaining a preform of the stiffener; integrating a layer of the first thermoplastic polymer into the preform of the stiffener at a location configured to be in contact with the substrate part; and subjecting the substrate part and the preform of stiffener to a thermomechanical cycle so as to consolidate the substrate part and weld the stiffener to the substrate part.

Abstract: A leading edge slat of a wing element of an aircraft. The aircraft defining a mark including a main fuselage axis x and a spanwise axis y. The wing procuring a lift along an axis z. The wing element having a skin forming the leading edge slat, a spar linked to the skin and a stiffening structure linked on the leading edge side to the spar and to the skin. The stiffening structure being formed from a formed sheet metal having a plurality of bosses distributed according to the length of the leading edge. The bosses extending between the spar and the inner face of the skin.

Abstract: A method for manufacturing a composite part with continuous fiber reinforcement and a polymer matrix from a composite preform. On one of the faces of the composite preform, a demarcated layer of thermoplastic polymer is deposited using an additive manufacturing method.

Abstract: A method for the hot stamping of a composite part with continuous fiber reinforcement in a thermoplastic matrix. A blank including a laminated structure of plies consisting in unidirectional tapes of fibers pre-impregnated with thermoplastic polymer is obtained. The blank is heated in the open to a temperature greater than or equal to the melting temperature of the polymer making up the matrix. The blank is then stamped.

Abstract: An apparatus and method for stamping a thermoplastic matrix composite blank, in view of heating and stamping the blank. The apparatus includes a machined blank and a frame. A plurality of cleats are fixed on the frame, extend towards the interior of the frame. The cleats delimit an internal opening surface of the frame, free from any obstacle. A locator is linked with a cleat and configured to cooperate with a hole machined in the blank. A heat sink is located near the locator and configured to maintain locally the blank temperature under the melting temperature of the polymer constituting the matrix, during the heating and transfer of the blank.

Abstract: A method for making a first ply for laying up a fibrous preform on a tool. An attachment zone is made on the laying up surface of the tool. The zone is integral with the laying up surface of the tool. A polymer is deposited by additive manufacturing on the surface of the tool. The polymer deposit passes on the attachment zone. The first ply is laid up by activating the tackiness of the polymer deposited using additive manufacturing, so as to make the deposited fibers adhere to the material deposited by additive manufacturing.

Abstract: A method for assembling a box structure includes elementary parts assembled along an understructure of stiffeners and skins. The understructure and skins are made of composite material with a polymer matrix. The method includes sizing the box structure for the loads to which it is subjected and for a glued assembly. A map of the loads on the structure is obtained and a first load limit is defined depending on the probability of the structure being damaged. The understructure and the skins are assembled by gluing them. An additional layer is applied that covers the assembled elementary parts to areas of the assembled box structure where the first load limit is reached.

Abstract: A device for fireproofing a section of a structural part made of composite material. The device includes a skin having an outer surface configured to face the flame and an inner surface. The skin is made of composite material that includes fibrous reinforcement in a polymer matrix. The skin includes a fastener to fasten the part to the structure. The device includes a layer of needled mineral felt placed between the inner surface of the skin and a surface of the structural part.

Abstract: A method for forming a thermoplastic composite material with continuous fiber reinforcement by stamping. A flat blank comprising a pre-consolidated stack of plies by automatic fiber placement of fibers referred to as the thermoplastic pre-impregnated fibers is obtained. The flat blank is reheated to a temperature greater than or equal to the melting temperature of the thermoplastic polymer making up the matrix of the thermoplastic pre-impregnated fibers. The reheated flat blank is hot stamped and the part formed between the stamping punch and die is consolidated.

Abstract: A device for welding the bottom flange of a stiffener on the side of a skin. The stiffener and the skin are made of a composite comprising a thermoplastic polymer matrix. The device comprises a punch, an anvil and a press to make a clamping between the punch and the anvil. The punch comprises a part forming a pressure table with a cross-section width less than or equal to the width of the stiffener bottom flange and a heating element with width less than the width of the pressure table. The anvil comprises a cooling component and has a cross-section width smaller than the width of the skin. A method for implementing the device.

Abstract: A laminated composite structural panel with fiber reinforcement comprising a skin with a thickness e1 and a localized reinforcement or patch. The skin is made up of a stack of fibrous plies in a matrix made of a thermoplastic polymer. The localized reinforcement or patch is joined to the surface of the skin and rises to a thickness of e2 in a direction that is locally normal to the skin, which is made up of a stack of fibrous plies in a matrix made of thermoplastic polymer. The surface of the plies that make up the patch is decreasing from the ply of the patch in contact with the skin so that the edges of the patch have a slope p greater than 0.5. The patch and the skin is joined by a weld.

Abstract: A method for assembling a skin and a flange of a stiffener. The periphery of the contact between the skin and the flange of the stiffener is sealed by applying a bead of adhesive on the flange of the stiffener in contact with the skin. A first and second orifices are made in the skin. The orifices open at the interface between the skin and the flange of the stiffener. The adhesive is injected through the first orifice at the interface between the skin and the flange of the stiffener while keeping the skin in contact with the stiffener until the interface between the skin and the stiffener is completely filled with the adhesive.

Abstract: A device for compacting and consolidating a stack of fibrous plies pre-impregnated with a thermoplastic polymer, configured to be placed in an oven. The device comprises containment blocks, a flexible compacting plate and a vacuum pump. The containment blocks are supported by a board and demarcate the perimeter of the stack. The containment blocks comprise open grooves that open into the perimeter of the stack. The flexible compacting plate has an area equal to that of the stack but is capable of being inserted inside the perimeter demarcated by the containment blocks. The vacuum pump applies a vacuum to the wrapped volume of the stack comprising a plurality of holes in the board that open outside the perimeter of the stack. A method for implementing the device for manufacturing a thick composite panel having a thermoplastic matrix.

Abstract: A method for making a structural element comprising a panel in composite material with fiber reinforcement in an organic matrix obtained by laying up and curing. The panel comprises a side likely to be exposed to contact with hydrocarbons. The required layer structure is obtained by laying up the plies of fibers pre-impregnated with resin having a curing temperature T1. A ply made of a thin film of polymer that can withstand hydrocarbons and the curing temperature T1, referred to as the protective film, is applied on the side exposed to hydrocarbons. The entire layered structure is cured under pressure at the temperature T1.

Abstract: An apparatus and method for stamping a thermoplastic matrix composite blank, in view of heating and stamping the blank. The apparatus includes a machined blank and a frame. A plurality of cleats are fixed on the frame, extend towards the interior of the frame. The cleats delimit an internal opening surface of the frame, free from any obstacle. A locator is linked with a cleat and configured to cooperate with a hole machined in the blank. A heat sink is located near the locator and configured to maintain locally the blank temperature under the melting temperature of the polymer constituting the matrix, during the heating and transfer of the blank.

Abstract: A landing gear box is made of composite material panels comprising a skin made of composite material and having two opposite general sides, and first stiffeners extending over one of the sides of the skin. It is characterised in that it comprises additional stiffeners that are arranged on the side of the skin opposite that bearing the first stiffeners, and which extend in a direction distinct from that of the first stiffeners. The skin and the stiffeners arranged on each side are preferably made integral by co-moulding.

Abstract: A stiffened panel and method for producing such a panel comprising a laminated skin extending in two directions, made of a resin and a continuous fibers reinforcement. A first stiffener in the form of a beam is made of a resin with continuous fibers reinforcement and extends on a first side of the laminated skin in a first direction. A second stiffener in the form of a beam is made of a resin with continuous fibers reinforcement and extends on a second side of the laminated skin in a second direction. The resins which make up the skin and the stiffeners are thermoplastic in nature and the stiffeners are closely joined to the skin by welding.

Abstract: A thermally insulating protection element for piping, including a hollow body with an open concavity and having a wall. The wall includes at least one rigid positioning and/or support platform designed to accommodate the fastening of technical equipment to be associated with the protection element. The element is designed to not only insulate piping, but also to constitute a direct device for supporting and fastening technical equipment such as a sensing line.

Abstract: A method for laying up a tape of fibers comprising a thermoplastic polymer and the consolidation upon deposition of a workpiece thus laid up. The method comprises the steps of pre-consolidating a tape of fibers pre-impregnated with a thermoplastic polymer by pultruding strands pre-impregnated with the thermoplastic polymer through a die. The pre-consolidated tape is stored in the form of a semi-finished product. The semi-finished product is tape laid on a ply of the same nature that is first deposited on a tooling by pressing the semi-finished product on the ply. The interface between the semi-finished product and the ply first deposited is heated to a temperature T, capable of welding the semi-finished product on the ply.

Abstract: A method for making a structural element comprising a panel in composite material with fiber reinforcement in an organic matrix obtained by laying up and curing. The panel comprises a side likely to be exposed to contact with hydrocarbons. The required layer structure is obtained by laying up the plies of fibers pre-impregnated with resin having a curing temperature T1. A ply made of a thin film of polymer that can withstand hydrocarbons and the curing temperature T1, referred to as the protective film, is applied on the side exposed to hydrocarbons. The entire layered structure is cured under pressure at the temperature T1.