Provided is a method for producing automotive glass with a member having a U-shaped cross section in a highly efficient and space-saving manner. The present invention relates to a method for producing automotive glass with a member by curing an adhesive for bonding an adherend 21 having a U-shaped cross section to an edge portion 20a of automotive glass 20, using a superheated steam generator 1. The superheated steam generator 1 includes a boiler part 2 for generating steam, a superheating unit 3 for superheating steam generated in the boiler part 2, and a superheated steam chamber 10 having a groove portion 111 for covering the edge portion 20a of the automotive glass 20 and including superheated steam ejection portions 12 for ejecting superheated steam supplied from the superheating unit 3. The step of curing the adhesive comprises covering the edge portion 20a of the automotive glass 20 together with the adherend 21, with the groove portion 111 of the superheated steam chamber 10, and spraying superheated steam to the adherend 21 from both sides of automotive glass 20 from the superheated steam ejection portions 12.

A foam assembly system is provided. The system is configured to heat a surface of foam. After the heating of the foam, an adhesive is applied, typically a high solids adhesive. The foam is then bonded to another foam surface. It has been found that the pre-heating of the foam before adhesive application greatly enhances the bond strength between the foam and the second foam surface to which it is adhered.

Aspects of the present disclosure are directed to a three-dimensional joint and/or formation thereof, such as by 3D-printing the joint. The joint is provided with an interface region having a curable material in a curable state. The joint is positioned with the interface region in contact with a joinable member, and the interface region is cured to form a bond between the joint and the joinable member. Such an approach may, for example, involve forming a mechanical and/or chemical bond with the joint. Further, by utilizing such a joint (e.g., in a 3D-printed form), complex structural components can be formed from a curable material that can be partially cured with structures formed therein, and cured further to create the bond.

The disclosure relates to a component device, in particular for a primary supporting component of an aircraft, which comprises a first component element, a second component element, a bonding providing a connection between the first component element and the second component element, a marker substance device configured to dispense a volatile marker gas to the environment when in contact with the surrounding air and being hermetically sealed from the surrounding air by the first component element, the second component element, and/or the bonding if the bonding is not damaged, and a detector device configured to detect the marker gas dispensed by the marker substance device.

Methods for reworking structures and reworked cellular core panels, reworked structures comprising the reworked cellular core panels, and guides and cutting apparatuses for reworking cellular acoustic panels and reworking cellular acoustic and non-acoustic panels are disclosed.

A composite fibrous susceptor for use in induction welding is described, along with methods of its construction and use. The composite fibrous susceptor can include a magnetically susceptible continuous fiber in conjunction with a thermoplastic polymer. The composite fibrous susceptor can be deposited according to an additive manufacturing process on a surface to be bonded according to an induction welding process.

A foam assembly system is provided. The system is configured to heat a surface of foam. After the heating of the foam, an adhesive is applied, typically a high solids adhesive. The foam is then bonded to another foam surface. It has been found that the pre-heating of the foam before adhesive application greatly enhances the bond strength between the foam and the second foam surface to which it is adhered.

The present disclosure is directed to methods for joining rotor blade components using thermoplastic welding. The method includes arranging a first thermoplastic component and a second thermoplastic component together at an interface, determining a size of a tolerance gap between the first and second components at the interface, placing a thermoplastic insert between the first and second components at the interface, the insert being larger than the tolerance gap, heating the insert and the first and second components such that the insert begins to flow so as to fill the tolerance gap between the first and second components, applying pressure to the interface such that the insert and the first and second blade components remain substantially in direct contact with each other at the interface, and welding the insert and the first and second components together at the interface, wherein the heat and the applied pressure between the insert and the first and second components at the interface maintain the insert and the first and second substantially in direct contact at the interface during welding.

The invention relates to a device for laminating a laminating foil element onto a component having a profiled lamination plane using a lamination tool, by means of which tool the laminating foil element is laminated onto the component, the lamination tool comprising a first tool half and a second tool half, and the device comprising a deflection arrangement for deflecting portions of the laminating foil element out of the profiled lamination plane.

A layered object manufacturing (LOM) system and method that provide controlled application of an adhesive onto multiple layers of a paper substrate to effect generation of a three dimensional object. The LOM system includes an adhesive reservoir, an adhesive dispenser, a paper feed mechanism, and a substrate grabber. The dispenser dispenses the adhesive from the reservoir onto the paper substrate at a build location. The paper feed mechanism feeds individual sheets of paper. The substrate grabber transports the sheets from the paper feed mechanism to a build object location to form layers of the paper substrate. The method successively binds individual paper sheets to one another using a water based adhesive applied to specific locations on each individual paper sheet. The method also includes separating scrap material from the three dimensional model and discarding the scrap material.