One fusion machine can butt or socket fuse polyolefin pipes and fittings in straight alignment or at inwardly or outwardly mitered universal angles from 0° to 45° for butt fusion and from 0° to 10° for socket fusion. The machine is manually driven, hydraulically monitored and operated in all configurations from one side of the machine.

The invention relates to a method for making a textile part (A; A1, A2), comprising a step of forming a stitched seam (c1, c2, c3; C). The stitched seam step also aims to secure an electronic tag (1) to the textile part (A; A1, A2). The electronic tag (1) is formed from a strip comprising a wired electronic device comprising a chip (3a) associated with at least one antenna wire (3b), the chip (3a) and the antenna wire (3b) being arranged inside the stitched seam (c1, c2, c3; C). The invention also relates to the textile part provided with the tag.

A structural member including a lightweight core, one or more skins, and a crosslinking nanolayer interposed therebetween that results in significant mechanical strength in the structure. The core is a polymer of reduced density by way of included voids, such as an open or closed cell foam, honeycomb, or corrugated structure. The core polymer has a lower density and may have a higher softening or melting temperature than the polymer skin materials. The core may be discontinuous at the interface with the skin such that only a small percentage of the core surface is actually in contact with the skin compared to the overall area of the interface. The skin may be a thermoplastic layer that attaches to the core material. The skin may be a composite material including non-thermoplastic reinforcements. The crosslinking nanolayer is covalently bonded to the surface of the core material and provides molecular compatibility with the skin material.

A temporary substrate adhesive according to an embodiment includes a silane coupling agent and a photobase generator, but does not include a resin.

A temporary substrate adhesive according to an embodiment includes a silane coupling agent and a photobase generator, but does not include a resin.

A method for thermoforming a bicycle frame component includes the steps of: (A) preparing first and second casings both made of a thermoplastic material, the first casing having a first abutment surface, the second casing having a second abutment surface; (B) preparing a reinforcing unit; (C) abutting the first and second abutment surfaces against each other, and then placing the reinforcing unit at a junction of the first and second casings; and (D) thermally bonding the reinforcing unit to the first and second casings such that the first and second casings are joined to form the bicycle frame component. A bicycle frame component is also disclosed.

The invention is a hybrid composite material between a first joining partner having a metal surface and a second joining partner having a polymeric material surface. A process for producing a hybrid composite material associated therewith is also described. The hybrid composite material according to the invention is characterized in that the metal surface has microstructured depressions, having a diameter and a structure depth in the micrometer range, the microstructured depressions have metallic surface regions which are furnished entirely with nanostructures, the structure dimensions of which are in the nanometer range, the microstructured depressions are blind holes or throughhole openings fully passing through the first joining partner.

The invention is a hybrid composite material between a first joining partner having a metal surface and a second joining partner having a polymeric material surface. A process for producing a hybrid composite material associated therewith is also described. The hybrid composite material according to the invention is characterized in that the metal surface has microstructured depressions, having a diameter and a structure depth in the micrometer range, the microstructured depressions have metallic surface regions which are furnished entirely with nanostructures, the structure dimensions of which are in the nanometer range, the microstructured depressions are blind holes or throughhole openings fully passing through the first joining partner.

A hose assembly includes a corrugated metal tube having a plurality of corrugations and an outer cuff portion extending from an endmost one of the plurality of corrugations, radially outward of an inner diameter of the endmost corrugation, an end connection having an outer end defining a fluid connector and an inner end defining a nose portion received in the outer cuff portion of the corrugated metal tube, and a collar surrounding the outer cuff portion of the corrugated metal tube and the nose portion of the end connection. The collar, the outer cuff portion, and the nose portion are welded together.

A hose assembly includes a corrugated metal tube having a plurality of corrugations and an outer cuff portion extending from an endmost one of the plurality of corrugations, radially outward of an inner diameter of the endmost corrugation, an end connection having an outer end defining a fluid connector and an inner end defining a nose portion received in the outer cuff portion of the corrugated metal tube, and a collar surrounding the outer cuff portion of the corrugated metal tube and the nose portion of the end connection. The collar, the outer cuff portion, and the nose portion are welded together.