An inflation device includes a balloon and a shaft coupled to one another via an overmold that includes a shut-off ridge. The shaft is in pressure communication with the balloon. Therefore, when fluid pressure is increased in the shaft the balloon may inflate. The use of shut-offs to form the overmold including shaping the shut-off ridge should result in an overmold with no flash and few or no bubbles within its structure.

A housing for an electronic device is disclosed. The housing comprises a first component and a second component separated from the first component by a gap. The housing also includes a first molded element disposed at least partially within the gap and defining at least a portion of an interlock feature, and a second molded element disposed at least partially within the gap and mechanically engaging the interlock feature. The first component, the second component, and the second molded element form a portion of an exterior surface of the housing. A method of forming the housing is also disclosed.

A method for producing a light module for a lighting device of a motor vehicle, wherein the module comprises a support component and a light-outcoupling component. According to the invention, a connection element for establishing a retaining connection between the support component and the light-outcoupling component is molded at least onto the support component by means of an injection molding process.

An injection molded composite component includes a groove extending from a first surface of the composite component and a tubing material placed within the groove and formed integrally with the composite component such that the tubing material forms an integrated conduit on the first surface of the composite component.

A mold assembly for forming a component exhibiting a sealed interior, including providing first and second mold halves, forming first and second half shells of material within cavities defined within each of the mold halves, and upon mating the mold halves together in a first closed mold configuration. The mold halves are reopened, with at least one of the shells being subsequently reoriented such that the first and second half shells are arrayed in opposing fashion with perimeter extending edges of each half shell arranged in contact with one another. Additional steps include reclosing the mold halves and subsequently forming a second perimeter extending material in contact with the contacting perimeter extending edges in order to bond the half shells together, upon which the mold halves are reopened and a completed component removed.

A joining structure includes a first member, a second member of a material different from that of the first member, and a separation mechanism provided between the first member and the second member and that separates the first member and the second member from each other, wherein a resin is filled into the space between the edge of at least one member among the first member and the second member, and the other member.

The invention relates to a method of manufacturing a composite building element that includes a casing material, a bulk material, and a locking element, the method including the steps of: (a) continuously feeding a first sheet of casing material into a filling station; (b) securing the bulk material to the first sheet of casing material; (c) continuously feeding the bulk material and the first sheet of casing material out of the filling station; the method characterised by the step of: (d) securing the locking element to the first sheet of casing material prior to securing the bulk material to the first sheet of casing material.

An isokinetic oscillation exercise device of an elongated flexible blade having a first and second end and a grip portion coupled to a middle portion of the elongated flexible blade. End caps coupled to said first and second ends adapted to storage. Further, a method is disclosed of manufacturing an isokinetic oscillation exercise device that provides a flexible elongated flexible blade, a grip portion injection molding, a pliable ring injection moldings, and end caps injection molding; slides the pliable rings on the elongated flexible blade separated by a length of the grip portion, overmolds a first-shot of the grip portion over the pliable rings, overmolds a second-shot of the grip portion to the first-shot of the grip portion to the elongated flexible blade, seals the first-shot to the second-shot of the grip portion against the pliable rings; and attaches the end caps to the elongated flexible blade.

The invention relates to a method for producing a grid made of composite material for straightening an air flow for an aircraft turbine engine. The described method is based on the use of longitudinal members (301) which have recesses (303) to allow the penetration of connecting elements (304) into said recesses during the manufacture of the grid.

A shaped part can comprise an opaque decorative layer, at least two symbols on the front side, a translucent base, the decorative layer having one or more first light channels, one or more first functional having a first light element, a first functional layer on the rear side of the base, the first functional elements on the front side of the first functional layer, the decorative layer having one or more second light channels, one or more second functional elements having a second light element, a second functional layer on the rear side of the decorative layer, the second functional elements in or on the second functional layer, and being provided at least partially in the second light channels, the second functional elements covering the second light channels of the decorative layer such that the second light channels become or are shielded from light of the first light elements.