A laminate structure and method of forming is provided. The laminate structure includes a first metal sheet having a first thickness, a second metal sheet having a second thickness, and an adhesive core having an adhesive thickness. The adhesive core is disposed between and bonded to the first and second metal sheets. The first and second metal sheets are made of an aluminum based material and the adhesive core is made of an adhesive material also described as a viscoelastic adhesive material. The laminate structure is configured such that a ratio of the sum of the first and second thickness to the adhesive thickness is greater than either to one (8:1). The laminate structure including the viscoelastic adhesive core is characterized by a composite loss factor at 1,000 Hertz which is continuously greater than 0.1 within a temperature range of 25 degrees Celsius to 50 degrees Celsius.

Aerogel-based components and systems for electric vehicle thermal management are provided. Exemplary embodiments include a heat control member. The heat control member can include reinforced aerogel compositions that are durable and easy to handle, have favorable performance for use as heat control members and thermal barriers for batteries, have favorable insulation properties, and have favorable reaction to fire, combustion and flame-resistance properties. Also provided are methods of preparing or manufacturing such reinforced aerogel compositions. In certain embodiments, the composition has a silica-based aerogel framework reinforced with a fiber and including one or more opacifying additives.

The present disclosure relates to articles and/or constructions with cohesive and to methods of making and using them. Many embodiments provide crush resistance in addition to customizability.

The present disclosure relates to articles and/or constructions with cohesive and to methods of making and using them. Many embodiments provide crush resistance in addition to customizability.

A foil transfer apparatus configured to transfer foil of a foil film to a sheet includes a cover movable between a closed position and an open position, a lock mechanism capable of locking the cover at the closed position, a heating member, a pressurizing member, a temperature sensor, and a controller configured to: calculate a first lock determination temperature and a second lock determination temperature that are values obtained by respectively adding a first correction value and a second correction value that are determined based on a condition for performing a foil transfer operation to a detection temperature detected by the temperature; control the lock mechanism to lock the cover when the first lock determination temperature is not lower than a first threshold; and control the lock mechanism to unlock the cover when the second lock determination temperature is lower than a second threshold.

A foil transfer apparatus configured to transfer foil of a foil film to a sheet includes a cover movable between a closed position and an open position, a lock mechanism capable of locking the cover at the closed position, a heating member, a pressurizing member, a temperature sensor, and a controller configured to: calculate a first lock determination temperature and a second lock determination temperature that are values obtained by respectively adding a first correction value and a second correction value that are determined based on a condition for performing a foil transfer operation to a detection temperature detected by the temperature; control the lock mechanism to lock the cover when the first lock determination temperature is not lower than a first threshold; and control the lock mechanism to unlock the cover when the second lock determination temperature is lower than a second threshold.

A composite molded cargo body panel including a core, an interior skin secured to a first side of the core having a thickness, and exterior skin secured to a second side of the core, and a plurality of recesses. The plurality of recesses are dispersed along a first direction at intervals in the interior skin, with the core thickness at each of the plurality of recesses being reduced compared to a maximum core thickness, and each of the plurality of recesses defines a support surface. A pocket is formed in each of the plurality of recesses, with the core thickness at the pocket being less than the core thickness at each of the plurality of recesses. A plurality of logistics inserts are attached to the respective support surfaces of the plurality of recesses so that, at each of the plurality of recesses, the logistics insert extends across the pocket.

A lightning strike protection layer for an aircraft is disclosed having a first portion and a second portion, the first portion includes a first fibre reinforced polymer composite layer and a first electrically conductive metal layer and the second portion includes a second fibre reinforced polymer composite layer and a second electrically conductive metal layer, and the first and second portions are joined at a butt joint, with the first and second fibre reinforced polymer composite layers abutting and the first and second electrically conductive metal layers abutting; and a butt-strap extending across the butt joint, the butt-strap comprising a third electrically conductive metal layer electrically connected to the first and second electrically conductive metal layers.

Implementations for composite display cover are described and provide improved protection and durability to device displays as compared with conventional display protection technologies. The described composite display cover, for instance, utilizes an ultra-thin glass layer with a polymer film applied directly to the glass layer and a hard coat applied to the polymer film. The polymer film, for instance, is applied to the glass layer without an adhesive. Further, the composite display cover can be attached to a display, such as via an adhesive layer that adheres the glass layer to a surface of the display.

The present invention is directed at electromagnetic shielding that is particularly suitable for applications in electric vehicles. The electromagnetic shielding is relatively lightweight and can be integrated into a carpet or textile type construction.