The present invention relates to a method for the production of polyamide 6 with low extract content and a device for it. Here, a melt of non-extracted polyamide 6 is cleaned from monomer and oligomers in a degasification device in vacuum, wherein the vapor being withdrawn from the degasification device by the vacuum generation device is cleaned from monomer, oligomers and optionally water at first in a direct condenser which is operated with liquid ε-caprolactam and subsequently in a pre-separator which is cooled with a coolant, before it reaches the vacuum generation device. A particularly preferable variant of the method envisages the usage of the melt of polyamide 6 with low extract content so prepared in a direct process of spinning into textile fibers and/or filaments.

A method of sealing a first component to a second component comprising the steps of locating at least one fiber reinforced polyimide resin layer against a first sealing surface on a first component and against a second sealing surface on a second component. At least one fiber reinforced polyimide resin layer is compressed against the first sealing surface and the second sealing surface prior to curing at least one fiber reinforced polyimide resin layer. At least one fiber reinforced polyimide resin layer is heated to promote flow and conformation to the first sealing surface and the second sealing surface. At least one fiber reinforced polyimide resin layer is cured to provide a fluid tight seal between the first component and the second component.

A method for producing a shaped bar from fiber composite material uses a bonding tool which has a heating-up portion. The method includes the steps that a number of fiber tapes provided with a thermoplastic matrix are fed in parallel to the bonding tool, are brought together and heated and bonded in the heating-up portion to form a fiber cord. The fiber cord is subsequently placed by the bonding tool directly into a processing tool or a depositing device designed to place the fiber cord into the processing tool.

Systems, apparatuses, and methods for constructing an airship quickly and cost-effectively are described. In one embodiments, a jig for constructing a mainframe of an airship structure may have a first rail and a second rail that are configured to be parallel to each other, the first rail and the second rail each forming an arc, multiple first supporting structures coupled to the first rail, wherein the first supporting structures have non-uniform heights to support a curvature of the arc of the first rail, multiple second supporting structures coupled to the second rail, wherein the second supporting structures have non-uniform heights to support a curvature of the arc of the second rail, wherein the first rail and the second rail are configured to interface with detachable wheels coupled to an outer surface of the mainframe and enable the mainframe to be rotated along its axis on the jig

Textile hose for encasing elongated objects, characterised by having a radially elastic outer layer made from wear-resistant material and at least one inner layer made from thermally insulating material.

A method of producing a fiber reinforced composite material satisfies condition 1: a thermosetting resin base material (B) includes a thermosetting resin (a) and a nonwoven fabric-shaped base material (a thermosetting resin base material satisfying the condition 1 is referred to as a thermosetting resin base material (B-1)); and condition 2: the thermosetting resin base material (B) is a base material including the thermosetting resin (a), and a porous sheet-shaped base material (b) or a film-shaped base material (c), the thermosetting resin (a) has a viscosity of 1,000 Pa.Math.s or more at 40° C., and the thermosetting resin (a) has a minimum viscosity of 10 Pa.Math.s or less during heating from 30° C. at a temperature rise rate of 1.5° C./min (a thermosetting resin base material satisfying the condition 2 is referred to as a thermosetting resin base material (B-2)).

Systems, apparatuses, and methods for constructing an airship quickly and cost-effectively are described. In one embodiments, an airship structure may have a plurality of mainframes, each comprising interconnected pyramid structures. One of the pyramid structures may include an apex joint, four base joints, first connectors, and second connectors. The apex joint and base joints may each have slots configured for receiving connectors. The apex joint may have four apex-to-base slots and each base joint may have a base-to-apex slot and two base-to-base slots. Each of the first connectors may connect the apex joint to one of the four base joints using one of the apex-to-base slots of the apex joint and the base-to-apex slot of that base joint. Each of the second connectors may connect two of the four base joints using one of the base-to-base slots of each of the two base joints connected by that second connector.

A paint roller manufacturing system and method are described. In an embodiment, an inner strip of material and an outer strip of material are wound about a mandrel in offset relation. The inner strip of material and the outer strip of material each comprise material that results in a final paint roller which shrinks by less than 2.5 percent of the final paint roller axial length, or which has shrinkage that varies by less +/−0.1%, upon hardening and setting. An adhesive is applied to at least a portion of the outer strip as it is wound about the mandrel. A length of fabric is wound about at least the outer strip to form a paint roller tube, and compression is applied to the paint roller tube while advancing the paint roller tube in a direction parallel to the mandrel. A precision measuring or sensing device is used to control a cutting device causing the cutting device to cut the advancing paint roller tube into pre-selected lengths prior to the paint roller tube hardening and setting.

The present disclosure relates to composites. One composite may include a resin and oxidized polyacrylonitrile fibers. The oxidized polyacrylonitrile fibers may be provided as a nonwoven fabric. An additional composite may include a resin and material scraps respectively including carbon fibers. The material scraps may be positioned to at least partially overlap one another and define a substantially continuous layer. The material scraps may be provided as a fabric and/or a plurality of loose fibers.

An absorbent article and method of making the absorbent article are disclosed. The absorbent article having a topsheet, a backsheet, and an absorbent core structure having one or more layers wherein at least one layer is a heterogeneous mass layer, wherein the topsheet and the heterogeneous mass are integrated such that they reside in the same X-Y plane.