B29C65/542

Systems And Methods For Sealing A Bond Cavity Between Structural Components
20220194019 · 2022-06-23 ·

In an example, a method of sealing a bond cavity is described. The method comprises placing an adhesive around a perimeter of a first structure to be joined to a second structure. The method also comprises positioning the first structure relative to the second structure such that the adhesive is disposed between the first structure and the second structure. The method also comprises merging the first structure and the second structure until the first structure and the second structure are separated by a desired gap for bonding. The method also comprises heating the perimeter to at least partially cure the adhesive to form a leak-proof bond cavity perimeter between the first structure and the second structure.

Systems And Methods For Evacuated Injection Repair Of Bondline Voids
20220194031 · 2022-06-23 ·

In an example, a method is described. The method comprises forming a single hole into a bond gap repair area. The method also comprises evacuating, via an adhesive injection apparatus attached to the single hole, the bond gap repair area and an injection channel of the adhesive injection apparatus. The method also comprises forcing adhesive through the evacuated injection channel and into the evacuated bond gap repair area.

Systems And Methods For Adhesive-Injected Patch Repair
20220194032 · 2022-06-23 ·

In an example, a method is described. The method comprises placing a repair patch over a repair area of a structure, the repair patch comprising a repair-patch hole. The method also comprises sealing the repair patch and repair area with a vacuum bag having a seal ring around a periphery of the vacuum bag. The method also comprises evacuating, via an adhesive injection apparatus attached to the repair-patch hole and the seal ring of the vacuum bag, the repair area and an injection channel of the adhesive injection apparatus. The method also comprises forcing adhesive through the evacuated injection channel and into the evacuated repair area.

DIRECT INJECT JOINT ARCHITECTURE ENABLED BY QUICK CURE ADHESIVE
20220194020 · 2022-06-23 ·

Methods and apparatuses for assembling components are described. An apparatus in accordance with an aspect of the present disclosure comprises a first structure having a first tongue, a second tongue, and a third tongue, the second tongue being between the first tongue and the third tongue, a second structure having a first groove, a second groove, and a third groove, the second groove being between the first groove and the third groove, a first adhesive, coupled to the first tongue and the first groove and coupled to the third tongue and the third groove when the first structure is coupled to the second structure, and a second adhesive coupled to the second tongue and the second groove when the first structure is coupled to the second structure, wherein the first adhesive is injected into the first groove and the third groove and the second adhesive is injected into the second groove.

End effectors and methods for adhesively attaching a first part to a second part

An end effector, for adhesively attaching a first part to a second part, comprises a support and a first nozzle, coupled to the support and movable relative to the support, and a second nozzle, coupled to the support and movable relative to the support. The first nozzle comprises a first-nozzle body, comprising a first-nozzle-body outlet port and a first-nozzle separator plate, extending from the first-nozzle body. The second nozzle comprises a second-nozzle body, comprising a second-nozzle-body inlet port and a second-nozzle separator plate, extending from the second-nozzle body. The end effector further comprises a roller, coupled to the support, rotatable relative to the support about a roller axis, and located between the first nozzle and the second nozzle.

METHOD AND DEVICE FOR SPLICING MULTIFILAMENT TEXTILE FIBERS
20230264432 · 2023-08-24 ·

A method for splicing two bundles (1, 2) of multifilament textile fibers comprises: inserting an end portion of a first bundle (1) into a first end of a heat-shrinkable sheath (10) and an end portion of a second bundle (2) into a second end of the sheath, axially opposite the first end, until the ends of the end portions of the two bundles are facing each other; inserting a curable organic material inside the sheath (10) in a space separating the end portions of the bundles (1, 2); heating a portion of the heat-shrinkable sheath (10) surrounding a joining portion (9) to a predetermined temperature; curing the curable organic material; and removing the sheath (10).

System and method for welding thermoplastic components to create composite structure
11325320 · 2022-05-10 · ·

A system and method for welding thermoplastic components by positioning and moving a heated plate between the components to melt their respective faying surfaces, and as the plate moves, pressing the components together so that the melted faying surfaces bond together as they cool and re-solidify, thereby creating a composite structure. The plate has a heated portion which is positioned between and heated to melt a portion of the first and second faying surfaces. A manipulator mechanism moves the plate along an interface from between the portion to between a series of subsequent portions of the first and second faying surfaces, thereby welding the thermoplastic components along the entire interface to create the composite structure. The heated portion may contact the faying surfaces and melt them through conduction, or may be suspended between them and melt them through radiation and convection.

FLEXURE ARRANGEMENTS FOR OPTICAL COMPONENTS
20220137426 · 2022-05-05 ·

An optical system can include a receiver secured to a first optical component and a flexure arrangement secured to a second optical component. The flexure arrangement can include a plurality of flexures, each with a free end that can extend away from the second optical component and into a corresponding cavity of the receiver. Each of the cavities can be sized to receive adhesive that secures the corresponding flexure within the cavity when the adhesive has hardened, and to permit adjustment of the corresponding flexure within the cavity, before the adhesive has hardened, to adjust an alignment of the first and second optical components relative to multiple degrees of freedom.

Systems and methods for adhesive-injected patch repair

In an example, a method is described. The method comprises placing a repair patch over a repair area of a structure, the repair patch comprising a repair-patch hole. The method also comprises sealing the repair patch and repair area with a vacuum bag having a seal ring around a periphery of the vacuum bag. The method also comprises evacuating, via an adhesive injection apparatus attached to the repair-patch hole and the seal ring of the vacuum bag, the repair area and an injection channel of the adhesive injection apparatus. The method also comprises forcing adhesive through the evacuated injection channel and into the evacuated repair area.

Adhesive injection method and structure

An adhesive injection method is for injecting an adhesive that bonds an outer plate and a reinforcing member. The reinforcing member has through holes bored through the reinforcing member in a direction intersecting a bonding surface facing the outer plate. The method includes positioning the outer plate and the reinforcing member; disposing a sealing material covering a gap between the outer plate and the reinforcing member; and injecting the adhesive into the through holes in order from one end to the other end of the bonding surface. At the injecting, while the adhesive is injected into the through hole, when the adhesive is recognized through another through hole formed adjacent to the through hole into which the adhesive is being injected, a through hole into which the adhesive is to be injected is shifted from the through hole into which the adhesive is being injected to the other through hole.