A method and a connecting element for joining two components, at least one of which is made of a fiber-reinforced composite, are proposed.

The present intake manifold consists of segments including an upper member, a lower member, and a middle member that is interposed between these members to demarcate and form intake passages so that the intake passages are arranged in a straight line, and has first welded portions at which the upper member and the middle member are welded together, and second welded portions at which the middle member and the lower member are welded together. The first welded portions are extended outward from the intake passage formed by the upper member and the middle member, and the second welded portions are extended outward from the intake passage formed by the middle member and the lower member. The middle member is provided with ribs holding the first welded portions and the second welded portions in one piece.

The invention relates to a method of producing a low-pressure compressor stator for an axial turbine engine. The stator comprises an external shroud with stubs and an annular row of stator blades extending radially towards the inside from the stubs. The method comprises the following stages: supply or production of a starting bar; bending of the bar so that it makes a circle, in order to form an unwrought external shroud; turning to form an axial annular wall delimited by annular fixing flanges; orbital friction-welding of a row of blades onto the stubs of the external shroud. The stubs are realized during a milling stage of the bar or of the external shroud, the milling being carried out before or after the bending stage. The shroud and the blades can be produced in titanium or in a thermoplastic polymer.

The present intake manifold consists of segments including an upper member, a lower member, and a middle member that is interposed between these members to demarcate and form intake passages so that the intake passages are arranged in a straight line, and has first welded portions at which the upper member and the middle member are welded together, and second welded portions at which the middle member and the lower member are welded together. The first welded portions are extended outward from the intake passage formed by the upper member and the middle member, and the second welded portions are extended outward from the intake passage formed by the middle member and the lower member. The middle member is provided with ribs holding the first welded portions and the second welded portions in one piece.

A method for joining thermoplastic composite includes: providing a first part having a first joining surface disposed in a first plane and a second joining surface disposed in a second plane that is non-parallel to the first plane; providing a second part having a third joining surface disposed in the first plane and a fourth joining surface disposed in the second plane; disposing the parts so that the first and third joining surfaces are in contact with one another, and the second and fourth joining surfaces are in contact with one another; forcing the second and fourth joining surfaces against one another; and welding the first and third joining surfaces together using a vibration welding process, wherein the welding process and the forcing of the second and fourth joining surfaces against one another causes the second and fourth joining surfaces to be welded.

The invention relates to a method of producing a low-pressure compressor stator for an axial turbine engine. The stator comprises an external shroud with stubs and an annular row of stator blades extending radially towards the inside from the stubs. The method comprises the following stages: supply or production of a starting bar; bending of the bar so that it makes a circle, in order to form an unwrought external shroud; turning to form an axial annular wall delimited by annular fixing flanges; orbital friction-welding of a row of blades onto the stubs of the external shroud. The stubs are realized during a milling stage of the bar or of the external shroud, the milling being carried out before or after the bending stage. The shroud and the blades can be produced in titanium or in a thermoplastic polymer.

A method and a connecting element for joining two components, at least one of which is made of a fiber-reinforced composite, are proposed.