B29C2045/0075

Compressible Non-Fibrous Adjuncts

Stapling assemblies for use with a surgical stapler are provided. In one exemplary embodiment, the stapling assembly includes a cartridge having a plurality of staples disposed therein and a non-fibrous adjunct formed of at least one fused bioabsorbable polymer and configured to be releasably retained on the cartridge. Adjunct systems for use with a surgical stapler are also provided. Surgical end effectors using the stapling assemblies are also provided. Methods for manufacturing stapling assemblies and using the same are also provided.

METHOD OF FILLING COOLING HOLES IN AN AIRFOIL COMPONENT

In an aspect, a method of filling a plurality of cooling holes in an airfoil component, the method comprises injecting a curable composition into a fill channel such that the curable composition flows through the fill channel to the plurality of cooling holes; forming a plurality of beads of the curable composition on a surface of the component over the plurality of cooling holes; directing a radiation to the respective beads in directions parallel to the respective central axes of the cooling holes associated with the respective beads to cure curable composition of the respective beads; and heating the component to cure the curable composition located in the fill channel.

METHOD FOR PRODUCING A SEAT FOR A SEATING OF ANY ONE ROAD VEHICLE AND PRODUCT THUS OBTAINED
20200180198 · 2020-06-11 ·

Method for producing a seat for a vehicle, the bottom and the foam obtained by molding in a double mold by the following subsequent steps: gluing: in which a robot moves the molded product in front of a glue nozzle; activation: in which the robot transfers the molded product into a heating station, activating the glue; loading: in which a user arranges the cover in a loading station; superimposition: in which the cover is transferred into a superimposition station; simultaneously, a second robot grasps the molded product and moves it into the superimposition station; pressing: in which a plurality of grippers press the edge of the cover against the edge of the bottom, causing irreversible gluing between the bottom and cover, forming the seat; moving-away: in which the second robot grasps the seat from the superimposition station and places it on a conveyor belt to move it away.

Method of filling cooling holes in an airfoil component

In an aspect, a method of filling a plurality of cooling holes in an airfoil component, the method comprises injecting a curable composition into a fill channel such that the curable composition flows through the fill channel to the plurality of cooling holes; forming a plurality of beads of the curable composition on a surface of the component over the plurality of cooling holes; directing a radiation to the respective beads in directions parallel to the respective central axes of the cooling holes associated with the respective beads to cure curable composition of the respective beads; and heating the component to cure the curable composition located in the fill channel.

Method of filling a microcavity with layers of polymeric material

A method of filling a microcavity with layers of a polymer material includes the following steps: (A) estimating a current vertical position of a bottom of the microcavity (current bottom position); (B) lowering the capillary tube into the microcavity towards the current bottom position; (C) dispensing a polymer composition from a tube outlet of the capillary tube under a dispensing applied pressure until the polymer composition substantially fills the microcavity; (D) curing a work piece including the microcavity and the polymer composition in the microcavity to obtain a current layer of the polymer material; and (E) repeatedly executing steps (A), (B), (C), and (D), until the layers of the polymer material have substantially filled the microcavity.

METHOD OF MANUFACTURING COVER WINDOW AND METHOD OF MANUFACTURING DISPLAY DEVICE
20240123661 · 2024-04-18 · ·

A method of manufacturing a display device, the method including ejecting a window raw material into a mold, precuring the ejected window raw material, molding a cover window by placing the precured window raw material onto a display panel and curing the precured window raw material, and separating the mold from the cover window.

Compressible stress and strain of non-fibrous adjuncts

Stapling assemblies for use with a surgical stapler are provided. In one exemplary embodiment, the stapling assembly includes a cartridge having a plurality of staples disposed therein and a non-fibrous adjunct formed of at least one fused bioabsorbable polymer and configured to be releasably retained on the cartridge. Adjunct systems for use with a surgical stapler are also provided. Surgical end effectors using the stapling assemblies are also provided. Methods for manufacturing stapling assemblies and using the same are also provided.

Process for the preparation of plastic composite molded bodies

Process for the preparation of plastic composite molded bodies in which hard-soft molded bodies made of low-melting thermoplastics and light curable polyorganosiloxane compositions are prepared as well as products produced by this process.

Vacuum injection molding for optoelectronic modules

Manufacturing optoelectronic modules includes supporting a printed circuit board substrate (27) on a first vacuum injection tool (24). The printed circuit board substrate (27) has at least one optoelectronic component mounted thereon and has a solder mask (40) on a surface (46) facing away from the first vacuum injection tool (24). The method includes causing the first vacuum injection tool (24) and a second vacuum injection tool (22) to be brought closer to one another such that a surface (46) of the second vacuum injection tool (22) is in contact with the solder mask (40). Subsequently, a first epoxy (100, 20) is provided, using a vacuum injection technique, in spaces (104) between the upper tool (22) and the solder mask (40).

METHOD OF FILLING COOLING HOLES IN AN AIRFOIL COMPONENT

In an aspect, a method of filling a plurality of cooling holes in an airfoil component, the method comprises injecting a curable composition into a fill channel such that the curable composition flows through the fill channel to the plurality of cooling holes; forming a plurality of beads of the curable composition on a surface of the component over the plurality of cooling holes; directing a radiation to the respective beads in directions parallel to the respective central axes of the cooling holes associated with the respective beads to cure curable composition of the respective beads; and heating the component to cure the curable composition located in the fill channel.