Patent classifications
B29C65/542
Connection of elements in motor vehicles
A system of connected elements for a motor vehicle includes: a first element which has at least one depression on a surface; a second element which is arranged on the first element in such a manner that a surface of the second element and the depression of the first element form a cavity; a filling opening which forms an access to the cavity; and an adhesive which at least partially fills the cavity and thereby adhesively bonds the first element to the second element.
SYSTEMS AND METHODS FOR JOINING NODES AND OTHER STRUCTURES
An additively manufactured node is disclosed. A node is an additively manufactured (AM) structure that includes a feature, e.g., a socket, a channel, etc., for accepting another structure, e.g., a tube, a panel, etc. The node can include a node surface of a receptacle extending into the node. The receptacle can receive a structure, and a seal interface on the node surface can seat a seal member between the node surface and the structure to create an adhesive region between the node and the structure, the adhesive region being bounded by the node surface, the structure, and the seal member. The node can also include two channels connecting an exterior surface of the node to the adhesive region. In this way, adhesive can be injected into the adhesive region between the node and the structure, and the adhesive can be contained by the seal member.
ROBOTIC TERMINAL EFFECTOR FOR AUTOMATIC PLACEMENT OF INSERTS IN A COMPOSITE PANEL OF THE SANDWHICH TYPE WITH A CELLULAR CORE
A robotic terminal effector for automatic placement of an insert in a cavity formed in a composite panel of the sandwich type with a cellular core. The insert including an upper flange having a resin inlet orifice and a resin outlet orifice. The effector being intended to be mounted on a carrier, and having a contact body with a contact surface. The contact surface having a means for injecting resin into an empty space delimited by the insert and the cavity when the insert is positioned in the cavity, and a means for grasping hold of the insert by suction. The resin-injection and grasping means being configured in such a way as to leave the contact surface free to be pressed firmly against an upper face of the composite panel so as to generate a continuous sealed region around the cavity while the insert is being placed in the cavity.
System and method for repairing a composite structure
A method of repairing a composite structure includes providing an assembled composite structure comprising a substantially rigid outer component, wherein the composite structure comprises a void space at least partially bounded by the outer component. The method further includes forming an injection hole through the outer component to provide a path between the void space and space external to the composite structure. The method further includes injecting foam into the void space through the injection hole while the foam is in a substantially unexpanded state and expanding the foam within the void space.
Manufacturing method of assembly
In a manufacturing method of an assembly, the assembly including a metal part and a pipe, the pipe including a material containing a resin, an adhesive is first adhered to an outer circumferential surface of the pipe and a metal part covering at least a portion of an outer circumferential surface of the pipe. Here, an area to which the adhesive is adhered on the outer circumferential surface of the pipe is defined as an adhesion area. Next, by a heat source provided inside the pipe, a target area is heated without interposing the metal part. The target area is located radially interior to the adhesion area and located on an inner circumferential surface of the pipe.
AGILE ROBOTIC HEADLAMP ASSEMBLY WITH SONIC FASTENING AND INJECTED LENS ADHESIVE
A system for assembling a plurality of components into an assembly is provided. The system includes an installation table, a first transfer robot, a second transfer robot, and an adhesive dispensing robot. The first transfer robot is configured to assemble some of the plurality of components into a first sub-assembly and transfer the first sub-assembly to the installation table. The second transfer robot is configured to assemble remaining ones of the plurality of components into a second sub-assembly, transfer the second sub-assembly to the installation table, and attach the second sub-assembly to the first sub-assembly. The adhesive dispensing robot is configured to apply an adhesive between the first sub-assembly and the second sub-assembly, after the second sub-assembly is attached to the first sub-assembly, to bond the second sub-assembly to the first sub-assembly.
METHOD FOR REPAIRING DELAMINATION AND MOISTURE BY HEAT, PRESSURE AND ADHESIVE
A method for repairing window laminates in which two plies have become separated to create a void, and wherein moisture may have entered through an edge of the window laminate and into the void. The method includes the steps of: placing the window laminate in a vacuum bag and inserting the vacuum bag containing the window laminate into an oven or autoclave for a minimum of ten minutes at a minimum temperature of 120 degrees Fahrenheit to remove the moisture between the plies; removing the vacuum bag and window laminate from the oven, and removing the window from the vacuum bag; forcing a needle on a syringe through the edge of the window laminate in the area of the void; and injecting an adhesive in the syringe into the void to fill the void with the adhesive.
Plastic woven fabric sewing machine
A plastic woven fabric sewing machine includes a stitching device on a tabletop of a worktable in which two overlapped fabrics are placed on the tabletop to be stitched, a tip of a needle portion of a stitching needle cylinder penetrates through the two fabrics to enter a thread knot shaping recess, a plastic material in a chamber is injected into the thread knot shaping recess from a needle hole, after the injected plastic material is cooled, it forms a thread knot to buckle the two fabrics, the tip of the needle portion is retracted from the two fabrics to generate a short stitching thread section, the tip of the needle portion is displaced on the two fabrics to complete one stitch of the two fabrics, the two fabrics are stitched together through continuous multiple stitches, and the stitches each have the thread knot.
System and Methods for Bonding A Structural Component Within a Channel of a Rail
The present disclosure provides a system for an aircraft. The system includes a rail having a bottom surface, and a first and a second sidewall extending from the bottom surface. The first sidewall, the second sidewall, and the bottom surface define a channel. The rail also includes blind holes, located in the bottom surface. The system also includes spacers, each comprising a stem and a top portion, extending substantially perpendicular to the stem. The stem of each of the spacers is configured to be positioned in a respective one of the blind holes such that a longitudinal axis of the top portion of each of the spacers is parallel to a longitudinal axis of the channel. The system also includes a structural component, a portion of which is configured to be positioned into the channel such that the structural component rests on the top portion of each of the spacers.
SYSTEM AND METHOD FOR WELDING THERMOPLASTIC COMPONENTS TO CREATE COMPOSITE STRUCTURE
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.