A cable includes a core with a plurality of first wires made of carbon steel and a plurality of strands surrounding the core. Each strand includes a plurality of second wires made of stainless steel. The cable has a maximum cross-sectional dimension less than 2 millimeters.

A window lifter assembly for adjusting a window pane comprising a rail defining a track, a slider coupled to and configured to translate along the track to move the window pane, a pulley rotatably coupled the rail, and a cable wound around the pulley and operatively connected to the slider so that movement of the cable rotates the pulley and moves the window pane, wherein the pulley is provided with an anti-friction coating that is configured to form a bearing surface between the pulley and an untreated portion of the rail.

A magnetic latch (10) for an appliance is disclosed for use with a strike plate (12). The latch includes a body (16) having two oppositely disposed side walls (18) and a bottom surface or wall (20). The body defines a magnet recess (26). An elongated handle (40) is pivotally coupled to the body. A spring loaded plunger pin (34) biases the handle. A magnet assembly (44) is positioned within the body. The magnet assembly includes a magnet (46) having a peripheral edge (48), and a pair of metal plates (54). The magnet has a peripheral cushioning sleeve (58) extending about the peripheral edges of the magnet. The peripheral sleeve is generally rectangular in shape having two oppositely disposed end walls (60) which include a cushioning projection (68). A pivot pin (74) extends through the magnet assembly to allow rocking motion.

A hinged component includes first and second portions of material coupled together by a composite live hinge. The live hinge includes a layer of tensile fabric and a layer of elastomer interposed between the tensile fabric and the material of one or both of the coupled first and second portions. The composite live hinge is capable of joining structural composite materials without the need for scoring, and thereby weakening, the structural composite material along the desired hinge line. The live hinge can be embedded in the materials it joins in a method that is compatible with traditional structural composite layup processes and in a manner which prevents resin from the structural composite materials from infiltrating the tensile fabric and compromising its flexibility.

A pivot sliding door guiding device includes a longitudinal profile with a guiding track and slider, supported on support rollers in a linearly movable manner in the guiding track, and which is connected to a door leaf and transfers a bearing load onto the slider. In the guiding track, convex bearing members extending in the longitudinal direction are disposed, on which support rollers of the slider with, in each case, peripherally extending concave guiding grooves roll and are retained in the transverse direction. The door leaf is connected to the slider whereby a center of gravity acts off-center on the slider in running and transverse directions. The slider has support rollers which serve for the load transfer of the load acting from the door leaf on the slider. The rollers roll on upper and lower convex bearing members, and transfer load of the door leaf via the convex bearing members.

A construction element includes a first wall, and a second wall. The walls are arranged at a distance from one another, forming a space wherein at least one non-concrete composite bar is arranged. Concrete is arranged in the space between the first wall, the second wall, and the composite bars.

A method for producing a carrier element for a window lifting device in which adjustment of a glass is performed by means of a traction means, the carrier element being displaceable along a guide rail of the window lifting device and being connected to the traction means, is provided. The completed carrier element has at least two interconnected bodies which are produced from dissimilar materials having dissimilar melting points, and the carrier element having the at least two bodies is produced by a multicomponent injection-molding method. In the production of the carrier element by the multicomponent injection-molding method a body from a material melting at a lower temperature is molded before a body from a material melting at a higher temperature, and the body from the material melting at a higher temperature is molded to the body from the material melting at a lower temperature.

A flexible hinge assembly for aircraft interior components and the like, including: a first structural component, wherein the first structural component includes a core material and one or more skin layers coupled to the core material; a second structural component, wherein the second structural component includes a core material and one or more skin layers coupled to the core material; wherein the one or more skin layers of the first structural component and the one or more skin layers of the second structural component are one or more of coupled together and integrally formed; and a flexure disposed between the first structural component and the second structural component, wherein the flexure is formed by the coupled together and/or integrally formed skin layers.

A supporting member includes: a rotatable spindle supported in a first housing; a cylindrical first guide fixed in a second housing, and guiding a relative movement of the spindle in an axial direction; a second guide fixed in the first housing, having an inner diameter larger than a first guide's outer diameter, and relatively movable in the direction to the first guide; and a nut being a stepped shaft-like member including an insertion portion inserted into the first guide, a protruding portion protruded from the first guide, and a narrow portion provided therebetween. The first guide includes a caulking portion to the nut at an opening end. The caulking portion includes a portion extending to intersect in the direction along a step between the insertion portion and the narrow portion, and another portion parallel to the direction along an outer circumferential surface of the narrow portion.

A hinged component fabrication method in which, in a layup stage of fabrication, the component includes a live hinge joining uncured material portions together at a hinge region and comprising a layer of tensile fabric at least partially infiltrated by an uncured elastomer layer at least partially interposed between the tensile fabric and the uncured material portions such that the uncured elastomer blocks the uncured material portions from infiltrating the hinge region. The method may include locating overlapped tensile fabric and elastomer layers in a tool and introducing polymer-based material into the tool such that polymer-based material portions overlap respective opposite ends of the fabric and elastomer layers. The polymer-based material portions are formed to a desired shape using the forming tool so that the fabric and elastomer layers form a live hinge between the polymer-based material portions.