A method for manufacturing a rivet connection of a fiber composite component. The method includes positioning a first component which contains a fiber composite material in an overlap joint with a second component, laser-drilling a shared through-hole at least through the fiber composite material of the first component, inserting a rivet into the through-hole and fixing the rivet to the first and to the second component.

In one embodiment, a method of forming a rigid package includes positioning a label with a plastic outer surface within a mould, positioning a PET sheet over the mould, contacting a first surface portion of the plastic outer surface with a second surface portion of the PET sheet, wherein at least one of the first surface portion and the second surface portion has a surface energy modified by a surface energy treatment, thermoforming the positioned PET sheet in the mould, and direct bonding the first surface portion and the second surface portion.

A method for producing a film having a fine irregular pattern intermittently includes feeding a film to be processed intermittently from upstream side to the vicinity of the surface of a die having a fine irregular pattern, transferring the pattern to the surface of the film by pressing the film against the surface of a die, stripping the processed film on which a pattern is formed from the surface of a die, and then feeding a new film to be processed to the die, wherein the processed film is stripped from the surface of a die by gripping and moving the processed film to the upstream side, and then the processed film is fed by a length of intermittent feed to the surface of a die while preventing the processed film from creasing.

A surgical implant (10) comprises an areal, flexible, porous basic structure (12) having a first face and a second face. At least one resorbable dyed film piece (20) is attached to the basic structure (12) and comprises a plurality of solid protrusions emerging from the dyed film piece (20) in a direction away from the basic structure (12). The at least one dyed film piece (20) is arranged in a shape structure which is asymmetric (“E”) in the area of the basic structure (12). Optionally, the implant (10) further comprises an adhesion barrier sheet (16).

A thermoforming machine and device are described. The thermoforming device relates to a mold assembly comprising a first and second mold, and to a mold that can be used in a thermoforming process. A method for thermoforming a product is also described. It is noted that the thermoforming device comprises a second pre-stretcher, in addition to a first pre-stretcher and a calibration element, and that the second pre-stretcher is at least partially and moveably arranged inside a second mold body. Movements of the first pre-stretcher, the second pre-stretcher, and the calibration element are configured to be individually controlled.

Providing blanks from a fibre web includes removing the blanks from removal regions and depositing the blanks in at least one deposit element. The blanks are then removed from the deposit elements in accordance with a sequence predefined by a layer-by-layer construction of a workpiece. The blanks that are individually removed from the removal regions are stacked on top of one another in the deposit elements in a sequence that corresponds to a layering sequence of the blanks in the workpiece. The blanks are then successively removed individually from the deposit elements in a sequence that is reversed with respect to the layering sequence of the blanks in the workpiece and are stacked on top of one another in a storage element before being successively removed from the storage element in the sequence predefined for constructing the workpiece layer-by-layer and inserted into a mould for producing the workpiece.

In various aspects, the present disclosure pertains to thermoformed webs that comprise polymer films having one or more thermoformed cavities contained therein, the polymer films comprising a polymer blend of amorphous polyethylene terephthalate (APET) and a copolyester that comprises (a) dicarboxylic acid residues (e.g., dicarboxylic acid residues that comprise terephthalic acid residues and, optionally, one or more additional dicarboxylic acid residues) and (b) diol residues (e.g., diol residues comprising ethylene glycol residues and, optionally, one or more additional diol monomer residues). Other aspects of the disclosure pertain to methods of forming such thermoformed webs, packaged products comprising such thermoformed webs, and methods of recycling such thermoformed webs.

A reinforcement sheet has a composite layer including fibres and a polymer A and a coating layer including polymer B, each polymer having at least 65 mol % of a repeat unit of formula:

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wherein for each polymer A and B, t1, and w1 independently represent 0 or 1 and v1 represents 0, 1 or 2. A method of forming the reinforcement sheet is also disclosed, in addition to a method for forming an article comprising a laminate of the reinforcement sheets and the article comprising such a laminate. The repeat unit may be ether-ether-ketone.

The invention relates to a container made from thermoplastic polymer with at least one inner reinforcing rib in a container wall, wherein the reinforcing rib is formed by at least one linear groove track in a container outer wall, the groove track extends over a length on the container outer wall, the groove track is formed by a multiplicity of depressions in the container outer wall, said depressions being arranged at a distance from one another, and wherein material bridges are provided between each of the depressions, said material bridges each having a smaller depth than the depressions. The invention furthermore relates to a method for producing such a container by extrusion blow molding or thermoforming.

A method of correcting, in a composite component, an inappropriate countersink with an inappropriate maximum diameter and/or depth, the inappropriate countersink being provided in the composite component at a fixation opening having a first opening diameter, the method comprising at least the steps of: Preparing a repair patch; Arranging the repair patch on the composite component in an area surrounding the inappropriate countersink; Pressing the repair patch at least partly into the inappropriate countersink by means of an associated pressure tool; and Fixing the repair patch in the inappropriate countersink.