Elasticized absorbent articles containing weakened elasticized portions and methods of manufacture are disclosed. A method comprises applying a first amount of adhesive to a first portion of at least one of the first web of material and the elastic strand, applying a second amount of adhesive to a second portion of at least one of the first web of material and the elastic strand, covering the elastic strand with either the first surface of the first web of material or a first surface of a second web of material to form an elasticized web. The elasticized web comprises a heavy bonding region and a light bonding region, wherein the heavy bonding region comprises a greater area density of adhesive than the light bond region. Finally, the method may further comprise partially weakening the waist panel elastic strand at least at one location within the second region.

Elasticized absorbent articles containing weakened elasticized portions and methods of manufacture are disclosed. A method comprises applying a first amount of adhesive to a first portion of at least one of the first web of material and the elastic strand, applying a second amount of adhesive to a second portion of at least one of the first web of material and the elastic strand, covering the elastic strand with either the first surface of the first web of material or a first surface of a second web of material to form an elasticized web. The elasticized web comprises a heavy bonding region and a light bonding region, wherein the heavy bonding region comprises a greater area density of adhesive than the light bond region. Finally, the method may further comprise partially weakening the waist panel elastic strand at least at one location within the second region.

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 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 crystalline shampoo, of a mixture comprising: one-quarter to three-quarter teaspoon of sodium lauryl sulfoacetate flake; one-eight to three-eights teaspoon of aloe vera leaf powder; one-eight to three-eights teaspoon of lactic acid; one-eight to three-eights teaspoon of olive oil; and 0.1 ml to 0.3 ml of essential oil. The mixture is encapsulated in a polyvinyl alcohol (PVA) sheet.

Disclosed is an edge wrapping method for a composite board, the top board of the composite board surrounds the bottom board of the composite board, a part or all of the side of the top board is disposed with a connecting portion extending beyond the bottom board and extending outwardly; the adjacent portion of the connecting portion and the bottom board are heated, and then the connecting portion is folded toward the inner side of the composite board and the connecting portion is welded to the side of the bottom board. The connecting portion and the bottom board are heated, and the root portion of the connecting portion near one end of the bottom board and the position of the bottom board close to the connecting portion are heated to a molten state, and then, the connecting portion is folded, and the connecting portion and the bottom board are welded together, the production efficiency of the present invention is high, the automatic production is realized, and the product qualification rate is effectively improved.

The invention relates to a method for manufacturing a tubular body (2) for a packaging in tube form (1), comprising the following steps: ) definition of the geometrical characteristics of the tubular body (2) to be produced; ) creation of an initial image (6) covering the surface of the tubular body (2) to be produced, said initial image (6) having a right lateral edge and a left lateral edge; ) creation of an intermediate image (8) from the initial image (6) by adding a lateral strip (13) to one of said edges of the initial image (6), said lateral strip (13) comprising a copy of the other of said edges of the initial image (6); ) printing of at least one intermediate image (8) on a sheet, the intermediate image (8) being disposed such that the lateral edges of the image are parallel to the direction of unwinding of the sheet; ) cutting of a small strip on each lateral side of the intermediate image (8) to form a final image (10); ) shaping of the sheet as tubular body (2) and edge-to-edge assembly to obtain a continuity of the design between the right edge and the left edge of the image.

A rotor blade segment of a wind turbine includes a seamless leading edge surface. A method of manufacturing a rotor blade segment of a wind turbine, the rotor blade segment having a seamless leading edge surface, includes forming an outer skin of the rotor blade segment. The outer skin defines a continuous outer surface. The continuous outer surface includes a pressure side surface extending between a pressure side aft edge and a pressure side forward edge, a suction side surface extending between a suction side forward edge and a suction side aft edge, and the seamless leading edge surface extends between the pressure side forward edge and the suction side forward edge. After folding the outer skin, the pressure side surface is positioned opposite the suction side surface and the pressure side aft edge is proximate the suction side aft edge.

The present disclosure provides method, computing device readable medium, and devices for dental appliances formed with folded material components. An example of a method of forming a dental appliance, includes forming a shell having a number of tooth apertures configured to receive and reposition a number of teeth of a patient along one jaw of a patient, the shell having a number of specialized components and wherein the number of specialized components are formed from folding multiple sections of the first sheet of material over each other.

The present disclosure provides method, computing device readable medium, and devices for dental appliances formed with folded material components. An example of a method of forming a dental appliance, includes forming a shell having a number of tooth apertures configured to receive and reposition a number of teeth of a patient along one jaw of a patient, the shell having a number of specialized components and wherein the number of specialized components are formed from folding multiple sections of the first sheet of material over each other.