In a method for manufacturing a honeycomb core by a domed bonding layer, a bonding sheet is, upon bonding of each cell, heated with hot air to form a uniform bonding layer on an end surface of each honeycomb cell, thereby providing a lightweight honeycomb core having stable strength. In the method for manufacturing the honeycomb core, a technique including the doming step of pumping, when bonding molding is performed for a core in which multiple ribs are connected to form an assembly of cells by means of a flat thermally-weldable bonding sheet laid on an upper surface of the core, upward hot air upwardly into the cells to form a dome-shaped bonding layer at the bonding sheet on an upper surface of each cell, the rupturing step of pumping downward hot air from above to the vicinity of the top of the dome-shaped bonding layer to rupture the bonding layer, and the thermal welding step of forming a uniform bonding layer on upper edge portions of the cells by means of meltability and surface tension.

Certain configurations of composite panels are described that comprise at least one aesthetic edge. In some embodiments, the composite panel with the aesthetic edge comprises a sandwich panel coupled to a shell layer. The sandwich panel may comprise skin layers and a core layer.

The present invention is directed to a new concept for an internal metallic tank of large-scale high-pressure gasholder in which pluralities of internal tanks have been accumulated like a honeycomb structure and for the manufacturing processes of the internal metallic tank.

A method and apparatus for fabricating a composite structure. The method comprises defining a shape for the composite structure with a first face sheet. The method places core sections on the shape defined by the first face sheet. The method places an adhesive in a group of joint cavities. The method places a second face sheet on the core sections placed on the first face sheet, wherein the first face sheet, the core sections, and the second face sheet, define a structural assembly in which the group of joint cavities are present. The method cures the structural assembly with the adhesive in the group of joint cavities to fabricate the composite structure in which the adhesive fills the group of joint cavities when the adhesive is cured.

Dry-scrubbing media compositions, methods of preparation and methods of use are provided. The compositions contain activated alumina and magnesium oxide. Optionally, activated carbon and other impregnates, such as hydroxides of group 1A metals, are included. The compositions exhibit improved efficiency and capacity for the removal of compounds, such as hydrogen sulfide, from an air-stream. The compositions are particularly useful for reducing or preventing the release of toxic gaseous compounds from the areas such as landfills, petroleum storage areas, refineries, drinking water systems, sewage treatment facilities, swimming pools, hospital morgues, animal rooms, and pulp and paper production sites.

A unitary core panel for a composite sandwich structure includes a plurality of cell walls defining a plurality of core cells, the plurality of cell walls extending across a thickness of the core, the plurality of core cells including one or more defined structural nonuniformities resulting in nonuniform properties of the core panel. A method of forming a core panel for a composite sandwich structure includes determining structural requirements of the core panel, designing the core panel to satisfy the structural requirements with one or more local nonuniformities in the core panel, and manufacturing the core panel as a unitary core panel with the one or more local nonuniformities.

The present disclosure relates to a process of manufacturing a multicellular structure comprising interconnected cells, wherein the process comprises: a) providing a polymerizable precursor of a polymeric material, wherein the polymerizable precursor comprises a reactive monomer mixture; b) providing a mold comprising precursor structures of the multicellular structure; c) optionally, heating at least one the reactive monomer mixture or the mold; d) incorporating the reactive monomer mixture into the precursor structures of the multicellular structure thereby substantially filling up the precursor structures of the mold, wherein the reactive monomer mixture has a viscosity of no greater than 10,000 mPa-s when incorporated into the precursor structures of the multicellular structure and when measured according to the viscosity test method defined in the experimental section; e) polymerizing the polymerizable precursor of the polymeric material into the precursor structures of the mold; and f) demolding the multicellular structure formed by polymerizing the polymerizable precursor of the polymeric material. According to another aspect, the present disclosure relates to a multicellular structure obtainable by the process as described above. In another aspect, the present disclosure relates to the use of a multicellular structure as described above for industrial applications.

A method and system for manufacturing a conical shaped acoustic structure. A sheet of acoustical material is cut to form individual pieces using a cutter system. Each individual piece in the individual pieces has a flat pattern for the conical shaped acoustic structure. An individual piece is positioned around a mandrel with a conical shape using an actuator system. Two edges of the individual piece are positioned for joining. The two edges of the individual piece positioned around the mandrel are joined to form the conical shaped acoustic structure.

The invention relates to a method for producing a reinforcement section in a preferably plate-shaped workpiece, wherein the workpiece has a core layer, a first cover layer and a second cover layer. In particular, such a workpiece may be a lightweight building board. Provision is made therein for a pasty, thermosetting mass to be introduced into an opening by way of the nozzle, while the nozzle and/or the workpiece moves at least temporarily during the release of the mass.

A composite panel assembly and method of forming the same includes a core, an inner skin coupled to a first side of the core, and an outer skin coupled to a second side of the core. A peripheral edge including portions of the core, the inner skin, and the outer skin, is compressed to close a path into the core.