Methods of manufacturing a layered glass element and various components of a layered class element, such as a pre-form assembly and a woven panel, are disclosed herein. These methods include the step of supplying a woven panel having a plurality of elongated strands woven into an open weave to define a first porous surface opposite of a second porous surface. A layer of interlayer material is applied to the first and second porous surfaces to encapsulate at least a portion of the woven panel within the interlayer material. These elements may be placed between a first and second layer of glass materials. A degree of pressure and heat is then applied for a first period of cure time to bond the interlayer material and the woven panel into either a pre-form assembly or a layered glass element.

An example of a lamination kit includes a first flexible film substrate, a primer fluid, a fixer fluid, an aqueous inkjet ink, a lamination adhesive, and a second flexible film substrate. The primer fluid includes a first binder. The fixer fluid includes a cationic salt and an organic acid. The aqueous inkjet ink includes a second binder, a pigment, a surfactant, a co-solvent, and a balance of water.

Provided is a joint manufacturing method including: a step A of preparing a laminate in which two objects to be joined are temporarily adhered with a heat-joining sheet including a pre-sintering layer interposed between the two objects to be joined; a step B of increasing a temperature of the laminate from a temperature equal to or lower than a first temperature defined below to a second temperature; and a step C of holding the temperature of the laminate in a predetermined range after the step B, in which the laminate is pressurized during at least a part of the step B and at least a part of the step C. The first temperature is a temperature at which an organic component contained in the pre-sintering layer is decreased by 10% by weight when the pre-sintering layer is subjected to thermogravimetric measurement.

Fabrication of a multi-layer X-ray source is disclosed using bulk structures to fabricate a multi-layer target structure. In one implementation, layers of X-ray generating material, such as tungsten, are interleaved with thermally conductive layers, such as diamond layers. To prevent delamination of the layers, various mechanical, chemical, and/or structural approaches may also be employed.

The present disclosure is directed to a position-controlled lamination tool or press that includes an array or plurality of pressure sensors and an array or plurality of heating/cooling elements or components, which may be coupled together, for preventing or reducing laminating film or material bleed out and improving thickness variation performance. The pressure sensors may provide a controller, which is coupled to the lamination tool, with real-time feedback on any thickness variations across a substrate panel and the controller may adjust the temperature output of the heating and cooling elements to locally modify the viscosity of the laminating material in one or more regions of the substrate panel to either decrease or increase the flowability of the laminating material.

A fabric containing carbon fibers impregnated with a silicone, polyurethane or acrylic emulsion which is then dried together with the fabric is disclosed. A protective layer containing a film, a woven or non-woven fabric is applied onto one side of the fabric.

Provided is a joint manufacturing method including: a step A of preparing a laminate in which two objects to be joined are temporarily adhered with a heat-joining sheet including a pre-sintering layer interposed between the two objects to be joined; a step B of increasing a temperature of the laminate from a temperature equal to or lower than a first temperature defined below to a second temperature; and a step C of holding the temperature of the laminate in a predetermined range after the step B, in which the laminate is pressurized during at least a part of the step B and at least a part of the step C. The first temperature is a temperature at which an organic component contained in the pre-sintering layer is decreased by 10% by weight when the pre-sintering layer is subjected to thermogravimetric measurement.

A fuel cell manufacturing method and a fuel cell manufacturing device are provided in which it is possible to heat, in a localized manner, sections for which heating is desired. In this fuel cell manufacturing method, a laminate is obtained by stacking a membrane electrode assembly and a separator that has an adhesive disposed therebetween. Coils are provided adjacent a site of the laminate to be heated. Preferably, coils are disposed on opposite sides of the site in the stacking direction of the membrane electrode assembly and the separator such that current flows in the same direction as directions intersecting the stacking direction. The site to be heated is subjected to induction heating by passing current through the coils.

Infrared transmitting glasses bonded into an optical element without interlayer voids by stacking at least two different infrared transmitting glasses inside a vessel where each glass has a different refractive index, a different dispersion, or both, and where the glasses all have similar viscosities, thermal expansion coefficients, and glass transition temperatures; placing a weight on top of the stack; applying a vacuum to the vessel; applying an isostatic pressure of at least 1500 psi; and after releasing the isostatic pressure, annealing at a temperature within 10 C. of the glass transition temperature at a pressure between 0 and 1000 psi. Applying the vacuum, applying the isostatic pressure, and annealing are done sequentially and with no intermediate transitions to ambient temperature or pressure.

A laminate (110) of polypropylene films (100), a luggage shell (120) constructed of the laminate (110), a method (200) of making the laminate (110), and a method (280) of making the luggage shell (120) are provided. The films (100) include a core (102) and at least one outer layer (104). The laminate (110) includes a plurality of films (100). The laminate (110) may be formed by laminating a plurality of films 100 under predetermined pressure, temperature, and time conditions. The shell (120) may be formed by deep drawing a sheet of laminate (110) while applying heat and tension to the laminate (110).