The vacuum sealer includes a base, a cover, a vacuuming device, at least a heating device, at least a heat-resistant element wrapping around the heating device, at least a heat insulation element between the base and the heating device, at least a power provision device, and at least a safety breaker device. The safety breaker device includes at least a safety switch, and at least a trigger element. The object to be sealed is placed on the heating device and, as the cover closes the base, the safety switch engages the trigger element to release safety breaker device and to allow the power provision device to power the heating device. The heat insulation element prevents heat from conducted to the base. With the dual protection from the safety breaker device and the heat insulation element, safety is enhanced and the power provision device may operate under high voltage.

In a method of manufacturing a thermoforming convex mold, the specification of a convex fixture is determined according to the curve shape of a thermoformed film sensor. The curve shape has a plane portion and a curve portion vertically downwardly extended from edges of the plane portion. The convex fixture has a base and a convex structure thereon. The height of each of the convex structure and the curve portion is in a range of 1 mm to 5 mm. The curvature radius of the curve corner between the top and the side wall of the convex structure is lower than 2 mm and higher than 0 mm. Next, the position of the side wall of the convex structure is uniformly shrunk inwardly by 0.4 mm to 0.6 mm, and the height of the convex structure is increased by 200% to 250%.

A caul body for forming a composite structure comprises a laminate having at least one carbon layer and at least one silicone layer. The at least one silicone layer defines an outer surface of the laminate. The laminate has a first region and a second region. A thickness of the at least one carbon layer in the first region is greater than a thickness of the at least one carbon layer in the second region. The first region has a hardness value greater than a hardness value of the second region.

A method of manufacturing a template, has: preparing a substrate containing quartz and having a surface, the surface including a protrusion and a depression; and processing the depression. The processing of the depression includes: a first step of forming a film on the surface, the film including a first region and a second region, the first region being provided on the protrusion, and the second region being provided on a bottom of the depression and being thinner than the first region; a second step of removing the second region with the first region partly remaining to expose the bottom of the depression; and a third step of processing the exposed part of the depression using a mask made of the remainder of the first region.

A method of joining first and second layers of polymeric composite material includes disposing a portion of a molded insert having a bottom end into a top surface of a first layer of material and then applying a layer of adhesive between the top surface of the first layer and a bottom surface of a second layer of material to create a bond-line thickness. Next, a top surface of the second layer is pierced with a headless end of a fastener and interlocked into the molded insert. A layer of protective coating is then applied to the top surface of the second layer of material to cover the interlocked fastener.

Packaging apparatus (1) comprises a packaging assembly (8) which has a supply unit (300) configured to supply electric energy to a conductive element of a heating head by causing an electric current flow through this conductive element; the conductive element defining a heating surface configured to heat seal one or more parts of said film. The electric conductive element comprising: a supporting substrate (206), at least a conductive structure engaged on the supporting substrate (206), at least one protective layer (208) covering the conductive structure as this latter is engaged between the supporting substrate (206) and the protective layer (208). The conductive element comprising at least one first and one second contacting tabs each integral with said conductive structure; each of said contacting tabs protruding transversally from a prevalent development surface of the conductive structure towards the supporting substrate (206) for defining a terminal contacting end. The heating head (700) comprising a first and second electric terminals respectively engaged with said first and second contacting tabs; each of said electric terminal is configured for stably constraining opposite faces of the respective contacting tab which define the thickness of said tab.

Packaging apparatus (1) comprises a packaging assembly (8) which has a supply unit (300) configured to supply electric energy to a conductive element of a heating head by causing an electric current flow through this conductive element; the conductive element defining a heating surface configured to heat seal one or more parts of said film. The electric conductive element comprising: a supporting substrate (206), at least a conductive structure engaged on the supporting substrate (206), at least one protective layer (208) covering the conductive structure as this latter is engaged between the supporting substrate (206) and the protective layer (208). The conductive element comprising at least one first and one second contacting tabs each integral with said conductive structure; each of said contacting tabs protruding transversally from a prevalent development surface of the conductive structure towards the supporting substrate (206) for defining a terminal contacting end. The heating head (700) comprising a first and second electric terminals respectively engaged with said first and second contacting tabs; each of said electric terminal is configured for stably constraining opposite faces of the respective contacting tab which define the thickness of said tab.

A method of manufacturing a self-supporting, monolithic fuselage body, including engaging peripheral mandrel sections around at least one central mandrel section, placing uncured composite material on the mold surface, curing the composite material on the mold surface, and sliding the central mandrel section(s) out of engagement with the peripheral mandrel sections and disengaging the peripheral mandrel sections from the cured composite material without collapsing the mandrel sections. The peripheral mandrel sections each include a shape-retaining core of a thermally insulating material and an outer layer on an outer surface of the shape-retaining core. The outer layer has a coefficient of thermal expansion within the range of variation of that of the coefficient of thermal expansion of the composite material. A mandrel for layup and cure of a predetermined composite material in the manufacture of a monolithic fuselage is also discussed.

Provided are polycarbonate fiber/carbon fiber composites and articles, the composites and articles having improved fire, smoke, and toxicity characteristics.

The present invention relates to a production method for a glassy carbon mold, and, more specifically, relates to a production method for a glassy carbon mold including the steps of: placing a mixture having a thermosetting resin, a curing agent, and a viscosity adjusting solvent between a thermosetting resin substrate and a master pattern formed by a micro-nano process; pressing either the master pattern or the thermosetting resin substrate and applying heat to form a cured thermosetting resin pattern part on the substrate; and removing the master pattern, and subjecting the substrate and the cured thermosetting resin pattern.