A method of joining a first component to a second component. A membrane is provided between the first component and a fluid. Pressure of the fluid is used to apply a compression force to a first part of the first component via the membrane. The pressure of the fluid is also used to apply an insertion force to the second component which pushes projections of the second component into a second part of the first component. The method can be integrated into a conventional manufacturing method, such as a vacuum-bagging process, which employs fluid pressure and a non-permeable membrane to compress the first component. The pressure of the fluid is used not only to apply the compression force, but also to apply the insertion force to the second component.

There are provided a method and device for thermocompression bonding of possibly preventing any warping of a resin member to be caused by thermocompression bonding, and of possibly reducing the time to be taken for processing. The method for thermocompression bonding, includes: preheating a resin member using an infrared radiation section; and subjecting the resin member to thermocompression bonding using a heating section and a pressurization section.

An assembly includes a medical package defining a housing configured to receive a medical supply. The medical package comprises a first sealable region and a second sealable region. The first and second sealable regions are configured to be sealed together to secure the medical supply within the housing. The medical package includes a thermal pattern configured to exhibit a first visible indicium indicative of an unsealed region between the first and second sealable regions. The thermal pattern is configured to irreversibly transform to a second visible indicium indicative of a sealed region between the first and second sealable regions in response to exposure to a temperature greater than or equal to a first temperature threshold, and to a third visible indicium indicative of a sterilized stage of the medical package in response to exposure to a temperature greater than or equal to a second temperature threshold.

A device for welding the bottom flange of a stiffener on the side of a skin. The stiffener and the skin are made of a composite comprising a thermoplastic polymer matrix. The device comprises a punch, an anvil and a press to make a clamping between the punch and the anvil. The punch comprises a part forming a pressure table with a cross-section width less than or equal to the width of the stiffener bottom flange and a heating element with width less than the width of the pressure table. The anvil comprises a cooling component and has a cross-section width smaller than the width of the skin. A method for implementing the device.

To provide a manufacturing method of a composite film for laminated glass, the method enabling the high-yield manufacture of the composite film that causes less appearance failure in the obtained laminated glass, while ensuring smooth workability. A manufacturing method of a composite film composed of a resin intermediate film and a plastic film for laminated glass, including: feeding the resin intermediate film with 0.04 to 0.4 N/cm tension and the plastic film, between a two rolls whose surface temperatures are 25 to 50 C., and pressing these to obtain a laminate; and feeding the laminate between a third roll whose surface temperature is 60 C. or higher and lower than Tg of a resin in the plastic film and a fourth roll whose surface temperature is lower than this by 15 to 30 C., so as to bring the plastic film into contact with the third roll, and pressing the laminate.

Methods and devices for bonding a plurality of substrates in a nip provided between an anvil and a bonding device may involve preheating a portion of a first substrate for a preheating duration to impart a preheated temperature, and then conveying the plurality of substrates to the nip to form a bond. The portion of the first substrate may reach the nip at a final temperature that is within 0 C. to 40 C. of the preheated temperature. A time-in-nip to create the bond may be less than 20 milliseconds. The preheating duration may be at least 200% longer than the time-in-nip. Laminate materials formed via such methods and devices may include unbonded areas in the nonwoven material that may have at least 5 fibers per square inch that are fused at fiber-to-fiber intersections caused by preheating the nonwoven material.

A connection element includes a composite component with a cured epoxy resin, a first layer including a first thermoplastic polymer and an intermediate layer arranged between the composite component and the first layer, the first layer containing both the cured epoxy resin of the composite component and the first thermoplastic polymer of the first layer. The first thermoplastic polymer has a melting point above a curing temperature of the epoxy resin and is soluble at a temperature of at least 150 C. in the epoxy resin used for producing the composite component.

A method for bonding composite structures which includes providing a first and second composite substrate and coupling a co-cure prepreg tape having chemically protected polymerizable functional groups onto a surface of both the first and second composite substrates. The first and second composite substrates are then cured to the co-cure prepreg tape at a first temperature to form a co-cure prepreg tape portion where the first and second composite substrates are fully cured and the co-cure prepreg tape is partially cured. The co-cure prepreg tape portion of the first composite substrate is then coupled to the co-cure prepreg tape portion of the second composite substrate and a deprotection initiator is applied to facilitate deprotection of the chemically protected polymerizable functional groups and cure the co-cure prepreg tape portion of the first and second composite substrates to form a single covalently bonded composite structure.

A method for manufacturing a thermally protected polymer composite structure using a thermal barrier layer, the thermal barrier layer being porous and including a tool-side surface and a non-tool-side surface opposed from the tool-side surface, the method including co-bonding an adhesive onto the non-tool-side surface of the thermal barrier layer to yield a coated thermal barrier layer comprising a coated surface, and co-bonding a polymer matrix composite material onto the coated surface of the coated thermal barrier layer.