B29C70/76

SYSTEMS AND METHODS FOR AN OBJECT WITH A BONDED ADHESIVE STRIP
20180009584 · 2018-01-11 ·

A method for joining adhesive tape to an object includes providing a piece of adhesive material, the piece of adhesive material having an adhesive surface covered with a removable cover on a first side and a non-tacky surface on a second side. The method further includes placing the piece of adhesive material in a mold and extruding an extrudable material over the adhesive tape, the extrudable material contacting the non-tacky surface of the adhesive material in the mold. The method further includes molding an object in the mold from the extrudable material and bonding the non-tacky surface to the object, the bonding resulting from the heat of the extrudable material.

SYSTEMS AND METHODS FOR AN OBJECT WITH A BONDED ADHESIVE STRIP
20180009584 · 2018-01-11 ·

A method for joining adhesive tape to an object includes providing a piece of adhesive material, the piece of adhesive material having an adhesive surface covered with a removable cover on a first side and a non-tacky surface on a second side. The method further includes placing the piece of adhesive material in a mold and extruding an extrudable material over the adhesive tape, the extrudable material contacting the non-tacky surface of the adhesive material in the mold. The method further includes molding an object in the mold from the extrudable material and bonding the non-tacky surface to the object, the bonding resulting from the heat of the extrudable material.

Concrete rodder and methods of use and manufacture of same
11713548 · 2023-08-01 ·

Apparatus and method for screeding/rodding concrete (and method of manufacture of the same), comprising: a rigid base member configured to comprise a tight tolerance of levelness along its length, and a mounting structure for securely attaching a working layer; attachment of a preferably fiberglass working layer comprising a durable material deposited on the rigid base member and capable of being finished to a smooth surface suitable for advantageous direct contact with poured wet concrete.

EDGE DESIGN OF A FLAT STIFFENING STRUCTURE FOR A COMPONENT
20230012965 · 2023-01-19 ·

A component having a flat reinforcing element of a first stiffness and a flat material of a second stiffness. The first stiffness is higher than the second stiffness. The flat reinforcing element has a first end on a first narrow side. The flat material, on a second narrow side thereof, has a second end that bifurcates into two strips. The two strips of the second end enclose the first end on both sides in a zone of enclosure.

Pumpable crib bag

A pumpable crib bag may include a body defining a longitudinal axis, at least one reinforcing wire helically extending about the longitudinal axis and along a length of the body, and at least one pocket configured to hold the at least one reinforcing wire therein. The at least one reinforcing wire may include a first material and a second material.

DEVICE FOR SHAPING A FIBROUS PREFORM FOR PRODUCING A BLADED PART OF A TURBOMACHINE

A device for shaping at least one fibrous preform for producing a bladed part of a turbomachine, this device including a mould formed by several parts that are interlocked with each other, this mould defining at least one internal cavity configured to receive the preform and to enclose the preform integrally, this cavity being intended to have two platform areas and a blade area extending between the two platform areas, wherein the mould includes at least a lower shell, an upper shell, a side shell, and end shells, and in that each of the side and end shells includes three elements, respectively lower, intermediate and upper.

DEVICE FOR SHAPING A FIBROUS PREFORM FOR PRODUCING A BLADED PART OF A TURBOMACHINE

A device for shaping at least one fibrous preform for producing a bladed part of a turbomachine, this device including a mould formed by several parts that are interlocked with each other, this mould defining at least one internal cavity configured to receive the preform and to enclose the preform integrally, this cavity being intended to have two platform areas and a blade area extending between the two platform areas, wherein the mould includes at least a lower shell, an upper shell, a side shell, and end shells, and in that each of the side and end shells includes three elements, respectively lower, intermediate and upper.

Methods and systems for identifying processing locations in composite layups
11472138 · 2022-10-18 · ·

Described are methods and systems for identifying processing locations in composite layups. An optical magnetic marker is magnetically supported by a layup tool at a target position, such that a portion of the marker protrudes above the tool processing surface. When a composite layup is placed onto that surface, the protruding portion extends into the layup at a processing location. When the layup is cured, the marker is permanently embedded into the layup. Separating the cured layup from the tool removes the marker from the tool and allows an additional marker to advance into the target position for processing another layup. The embedded marker or, more specifically, marker's reflective surface is used during optical inspection of the layup surface to precisely determine the processing location. In some examples, the marker is consumed while the layup is processed at that location,

Methods and systems for identifying processing locations in composite layups
11472138 · 2022-10-18 · ·

Described are methods and systems for identifying processing locations in composite layups. An optical magnetic marker is magnetically supported by a layup tool at a target position, such that a portion of the marker protrudes above the tool processing surface. When a composite layup is placed onto that surface, the protruding portion extends into the layup at a processing location. When the layup is cured, the marker is permanently embedded into the layup. Separating the cured layup from the tool removes the marker from the tool and allows an additional marker to advance into the target position for processing another layup. The embedded marker or, more specifically, marker's reflective surface is used during optical inspection of the layup surface to precisely determine the processing location. In some examples, the marker is consumed while the layup is processed at that location,

FIBER COMPOSITE STRUCTURE AND METHOD FOR MANUFACTURING A FIBER COMPOSITE STRUCTURE
20230122380 · 2023-04-20 ·

A fiber composite structure includes a base structure being formed of a first fiber composite material that includes first fiber bundles embedded in a first matrix material, wherein the base structure includes an opening defined by first fiber bundles which include first sections and a second section that continuously or uninterruptedly interconnects the first sections, wherein the second section forms a bay that defines a part of the circumference of the opening. The fiber composite structure further includes a functional structure positioned in the opening of the base structure and joined with the first fiber composite material of the base structure.