Abstract: A method and processing station for producing a veneer having two parallel opposed faces and including at least one lignocellulosic layer made of lignocellulosic fibers having a grain extending along the opposed faces of the veneer. The processing station carries out the method by applying a compressive force to the veneer along at least one direction extending along the opposed faces of the veneer so as to mechanically compress the lignocellulosic fibers.

Abstract: A method and processing station for producing a veneer having two parallel opposed faces and including at least one lignocellulosic layer made of lignocellulosic fibers having a grain extending along the opposed faces of the veneer. The processing station carries out the method by applying a compressive force to the veneer along at least one direction extending along the opposed faces of the veneer so as to mechanically compress the lignocellulosic fibers.

Abstract: A method and processing station for producing a veneer having two parallel opposed faces and including at least one lignocellulosic layer made of lignocellulosic fibers having a grain extending along the opposed faces of the veneer. The processing station carries out the method by applying a compressive force to the veneer along at least one direction extending along the opposed faces of the veneer so as to mechanically compress the lignocellulosic fibers.

Abstract: A method for coating a surface of a supporting element with a layer of ligneous material in order to form a motor vehicle trim element. The method includes the following consecutive steps: precutting the coating layer so as to form at least one precut area in the layer of ligneous material; positioning the layer of ligneous material relative to the supporting element by means of the precut area; and attaching the layer of ligneous material to the surface of the supporting element.

Abstract: A lining element includes at least one decorative layer formed from at least one complex that includes both a ligneous material layer having a backside and a front side and a reinforcement layer extending over the backside of the ligneous material layer. The decorative layer further includes at least one additional layer made in a material different from the ligneous material. The front side of the additional layer substantially extends in the continuity of the front side of the complex. The additional layer and the complex are attached to each other through at least one seam.

Abstract: The invention relates to a method in which the coating (6) is thermoformed and the coating (6) is cut in at least one cutting region (18). According to one aspect of the invention, the reinforcement layer (12) is impregnated with a thermosetting resin at least in one cutting region (18), and the coating (6) is cut in the cutting region after the thermoforming of the coating and the setting of the thermosetting resin.

Abstract: The invention relates to a method consisting in: inserting the coating (6) into a shaping and injection-molding mold (14); closing the mold (14) such that the coating (6) is shaped against a shaping surface (22) of the mold (14) as the mold (14) is closed; and, subsequently, overmolding the substrate (4) by injecting a plastic material into the mold (14). According to one aspect of the invention, the shaping surface (22) is induction-heated in order to thermoform the coating (6) as the mold (14) is closed, by generating induced currents that propagate along the shaping surface (22), and the induction heating is stopped in order to set the plastic material.

Abstract: The trim element (1) comprises at least one decorative element (6) made in a first material and comprising an external face forming a portion of the visible face of the trim element (1) and an internal face, said decorative element (6) being laid out on a film in plastic material (4), different from the first material, said film (6) comprising at least one underside area (16), extending over the internal face of the decorative element (6), said film being at least partly laid out on a substrate (2). The film (4) further comprises at least one peripheral area (18) extending around at least one portion of the decorative element (6) and forming another portion of the visible face of the trim element (1).

Abstract: A method and processing station for producing a veneer having two parallel opposed faces and including at least one lignocellulosic layer made of lignocellulosic fibers having a grain extending along the opposed faces of the veneer. The processing station carries out the method by applying a compressive force to the veneer along at least one direction extending along the opposed faces of the veneer so as to mechanically compress the lignocellulosic fibers.

Abstract: A device for a motorized aircraft includes at least one avionic component positioned in the aircraft, at least one engine interface positioned in the aircraft and at least one engine controller positioned in or near an engine of the aircraft. The at least one engine interface is designed to exchange data between the at least one avionic component and the at least one engine controller. The at least one engine interface is generic and able to communicate with engine controllers of various types that may be mounted on the aircraft. The at least one engine controller is specific to a particular engine.

Abstract: The trim element (1) comprises at least one decorative element (6) made in a first material and comprising an external face forming a portion of the visible face of the trim element (1) and an internal face, said decorative element (6) being laid out on a film in plastic material (4), different from the first material, said film (6) comprising at least one underside area (16), extending over the internal face of the decorative element (6), said film being at least partly laid out on a substrate (2). The film (4) further comprises at least one peripheral area (18) extending around at least one portion of the decorative element (6) and forming another portion of the visible face of the trim element (1).

Abstract: A method for coating a surface of a supporting element with a layer of ligneous material in order to form a motor vehicle trim element. The method includes the following consecutive steps: precutting the coating layer so as to form at least one precut area in the layer of ligneous material; positioning the layer of ligneous material relative to the supporting element by means of the precut area; and attaching the layer of ligneous material to the surface of the supporting element.

Abstract: A vehicle trim element that includes a complex formed from at least one layer of ligneous material and a reinforcing layer that extends over an inner face of the layer of ligneous material. The trim element further includes a substrate made from a first plastic material and at least one insert made from a second plastic material. The insert is located between the reinforcing layer of the complex and the substrate so as to space the substrate away from the reinforcing layer. The substrate is overmolded by injection on the insert.

Abstract: A lining element includes at least one decorative layer formed from at least one complex that includes both a ligneous material layer having a backside and a front side and a reinforcement layer extending over the backside of the ligneous material layer. The decorative layer further includes at least one additional layer made in a material different from the ligneous material. The front side of the additional layer substantially extends in the continuity of the front side of the complex. The additional layer and the complex are attached to each other through at least one seam.

Abstract: The invention relates to a method consisting in: inserting the coating (6) into a shaping and injection-molding mold (14); closing the mold (14) such that the coating (6) is shaped against a shaping surface (22) of the mold (14) as the mold (14) is closed; and, subsequently, overmolding the substrate (4) by injecting a plastic material into the mold (14). According to one aspect of the invention, the shaping surface (22) is induction-heated in order to thermoform the coating (6) as the mold (14) is closed, by generating induced currents that propagate along the shaping surface (22), and the induction heating is stopped in order to set the plastic material.

Abstract: The invention relates to a method in which the coating (6) is thermoformed and the coating (6) is cut in at least one cutting region (18). According to one aspect of the invention, the reinforcement layer (12) is impregnated with a thermosetting resin at least in one cutting region (18), and the coating (6) is cut in the cutting region after the thermoforming of the coating and the setting of the thermosetting resin.

Abstract: The invention relates to a compression mould for coating a rigid member that includes a male portion and a female portion each including a reception surface, respectively, of the member and of a coating layer. The surface has the shape of the member, one of the portions being movable so as to bear against the member and the coating layer in order to bind the coating layer to the member. A silicone-based coating is attached to one of the portions, wherein the coating is intended to bear against the member in order to apply a substantially uniform pressure on said member.

Abstract: The invention relates to a device for motorized aircraft comprising at least one avionic component (300) positioned in the said aircraft, at least one engine interface (310) positioned in the said aircraft and at least one engine controller (315) positioned in or near an engine (320) of the said aircraft. According to the device of the invention, the said at least one engine interface (310) is designed to exchange data between the said at least one avionic component (300) and the said at least one engine controller (315). The said at least one engine interface (310) is generic and able to communicate with engine controllers (315) of various types that may be mounted on said aircraft. The said at least one engine controller is specific to a particular engine.

Abstract: A method for coating a component with a thin layer of ligneous material, includes selecting a sheet of coating constituted at least partially by a thin layer of ligneous material intended to be visible in the finished component, coating the surface of the sheet with a thin layer of a transparent composition containing a synthetic resin, and fixing the coated sheet to the surface of the component. In the fixing step, the layer of composition deposited on the surface of the sheet has a resilience which is at least 5% greater, and preferably at least 10% greater, than that of the thin layer of ligneous material in all directions, and the composition layer is transparent so that the layer of ligneous material is visible through the layer of composition. A step of engraving the surface of transparent composition opposite the layer of ligneous material is advantageous after coating.