B29C45/1418

METHOD FOR MANUFACTURING A COMPOSITE STRUCTURE
20220371287 · 2022-11-24 ·

A method for manufacturing a composite structure having first and second structural members includes the steps of: (A) placing a plate in a forming mold having a first molding member, and a second molding member with an injection hole; (B) moving the first molding member toward the second molding member to stamp and deform the plate; (C) injecting a molten substrate onto the plate via the injection hole to stamp and deform again the plate so as to form the first structural member; (D) removing an assembly of the first structural member and a solidified substrate from the first molding member; and (E) removing an excess part of the solidified substrate to form the second structural member.

Injection Molding System And Manufacturing System
20220371239 · 2022-11-24 ·

An injection molding unit includes a main unit and an optional unit, the main unit accommodating a first injection molding machine that molds an integrated product by injecting a first molding material into a cavity which is defined by a lower die and an upper die and in which an insert member is disposed. The optional unit includes at least one of a member molding unit that accommodates a second injection molding machine that molds the insert member by injecting a second molding material or a press molding machine that molds the insert member in press molding, and a robot unit that accommodates a robot that performs placement operation of placing the insert member in the cavity or transport operation of transporting the integrated product molded by the first injection molding machine. The main unit is so configured that the optional unit is attachable thereto and detachable therefrom.

Insert molding apparatus

An insert molding apparatus includes: a lower mold including a seating part on which an insert member including a through-hole is seated; an upper mold mounted on the lower mold to receive the insert member seated on the seating part; and a first fixing part including a first head provided in the lower mold and inserted into the through-hole of the insert member when the insert member is seated, and a first drive unit that moves the first head. The first drive unit is moved to adjust a length by which the first head is inserted into the through-hole.

METHOD FOR MANUFACTURING COMPOSITE MOLDED ARTICLE AND COMPOSITE MOLDED ARTICLE

A composite molded article is manufactured in such a manner that a molding mold that forms a molding space by mold closing and has a weir portion projecting into the molding space is opened, a flat plate-like first member that is softened under heating is arranged in a part of a portion where the molding space is formed, the stereoscopic first molded portion is formed with mold closing, simultaneously an injected molten resin is filled in a remaining portion of the molding space around the first member outside the weir portion in a state that the weir portion is made to abut against a thin portion provided at a peripheral edge of the first molded portion, and the second molding portion joined to the first molding portion is formed by hardening molten resin after the resin is caused to contact the first molded portion.

Inner part and resin molded article

Provided are an inner part and a resin molded article according to which it is possible to mitigate the concentration of stress at a distal end of a melt rib. An inner part, around which an outer portion is to be arranged through integral molding, includes a main body portion made of resin, and a melt rib provided protruding outward from the main body portion. The melt rib is formed such that a height of the melt rib is greater than a thickness of the melt rib, the thickness decreases from the main body portion to a distal end of the melt rib, and the melt rib includes a melting portion configured to partially melt during molding of the outer portion.

METHOD FOR MANUFACTURING A DOOR OF A THRUST REVERSAL SYSTEM, A THRUST REVERSAL SYSTEM DOOR THUS OBTAINED AND AIRCRAFT PROPULSION ASSEMBLY COMPRISING SEVERAL SAID DOORS
20230103118 · 2023-03-30 ·

A door for a thrust reversal system, an aircraft with such a door, and a method for manufacturing a door of a thrust reversal system. The door comprises a wall formed from long fibers embedded in a thermoplastic resin matrix and a network of ribs overmolded on one of the faces of the wall. A propulsion assembly of an aircraft comprises a thrust reversal system having a plurality of such doors.

Laminating thin strengthened glass to curved molded plastic surface for decorative and display cover application

A process comprises cold-forming a flat glass substrate into a non-planar shape using a die. The cold-formed glass substrate is bonded to a non-planar rigid support structure at a plurality of non-planar points using the die. Bonding methods include injection molding the non-planar rigid support structure, and direct bonding. An article is also provided, comprising a cold-formed glass substrate having opposing major surfaces and a curved shape, the opposing major surfaces comprising a surface stress that differ from one another. The cold-formed glass substrate is attached to a rigid support structure having the curved shape. The cold-formed glass substrate includes an open region not in direct contact with the non-planar rigid support structure, and the open region has a curved shape maintained by the non-planar rigid support structure.

CARRIER WITH LOCALIZED FIBROUS INSERT AND METHODS
20230093318 · 2023-03-23 ·

A structural reinforcement for an article including a carrier that includes: (i) a mass of polymeric material having an outer surface; and (ii) at least one consolidated fibrous insert (14) having an outer surface and including at least one elongated fiber arrangement having a plurality of ordered fibers arranged in a predetermined manner. The fibrous insert is envisioned to adjoin the mass of the polymeric material in a predetermined location for carrying a predetermined load that is subjected upon the predetermined location (thereby effectively providing localized reinforcement to that predetermined location). The fibrous insert and the mass of polymeric material are of compatible materials, structures or both, for allowing the fibrous insert to be at least partially joined to the mass of the polymeric material. Disposed upon at least a portion of the carrier may be a mass of activatable material.

Seat frame assembly and method of manufacturing same

Disclosed are a seat frame assembly and a method of manufacturing the same whereby adhesion of a reinforcing material attached to a seat frame is improved to secure rigidity of the seat frame and process speed is improved. According to one embodiment disclosed herein, seat frame assembly includes: a frame configured such that a portion of each of opposite sides is bent forward, and supporting an upper body of an occupant; and side members joined to the opposite sides of the frame, respectively, each of the side members including a groove formed in a surface being in close contact with the frame, wherein a portion of the frame that is surface-joined to each of the side members is provided with a protrusion inserted into the groove.

Insert molding method and insert molding component

An insert molding component includes a primary molding section with a concave portion formed on one surface thereof, an insert component disposed on a bottom side of the concave portion of the primary molding section, a heat-insulating component disposed in the concave portion of the primary molding section and disposed on a top of the insert component, and a secondary molding section disposed in contact with the one surface of the primary molding section.