F16B19/04

Aluminum alloy, aluminum alloy spring, and fastening member made of aluminum alloy
11505851 · 2022-11-22 · ·

An aluminum alloy according to the present invention includes 1.2% by mass to 4.0% by mass of copper, 4.0% by mass to 14.0% by mass of zinc, 0.5% by mass to 4.0% by mass of magnesium, 0.01% or less of silicon, and 0.01% or less of iron, with the balance containing aluminum and inevitable impurities, and has an average equivalent circle crystal grain size of 500 nm or less.

HANDLE FOR A KITCHEN CONTAINER AND RELATIVE SYSTEM FOR FASTENING TO SUCH A KITCHEN CONTAINER
20170360260 · 2017-12-21 ·

The invention describes a system for fastening a handle to a kitchen container that comprises a plate-like fastening element, configured for being irremovably constrained both to a wall of the kitchen container, and to the handle. The plate-like fastening element is configured to be housed and restrained in a corresponding blind hole obtained at an end of the handle. The plate-like fastening element comprises at least one inclined hooking wing, integral with the plate and projecting below one of its surfaces. Each inclined hooking wing is configured for inserting, through elastic deformation while switching from the disassembled configuration to the assembled configuration of the fastening system, into at least one corresponding concave portion obtained on an inner surface of the blind hole towards which each inclined hooking wing projects in the assembled configuration of the fastening system.

HANDLE FOR A KITCHEN CONTAINER AND RELATIVE SYSTEM FOR FASTENING TO SUCH A KITCHEN CONTAINER
20170360260 · 2017-12-21 ·

The invention describes a system for fastening a handle to a kitchen container that comprises a plate-like fastening element, configured for being irremovably constrained both to a wall of the kitchen container, and to the handle. The plate-like fastening element is configured to be housed and restrained in a corresponding blind hole obtained at an end of the handle. The plate-like fastening element comprises at least one inclined hooking wing, integral with the plate and projecting below one of its surfaces. Each inclined hooking wing is configured for inserting, through elastic deformation while switching from the disassembled configuration to the assembled configuration of the fastening system, into at least one corresponding concave portion obtained on an inner surface of the blind hole towards which each inclined hooking wing projects in the assembled configuration of the fastening system.

NEGATIVE POISSON`S RATIO MATERIALS FOR FASTENERS
20230189940 · 2023-06-22 ·

The disclosure describes a zipper including two rows of zipper teeth, in which at least some of the zipper teeth include a negative Poisson's ratio (NPR) foam material having a Poisson's ratio of between 0 and −1, and a slider movably attached to one of the rows of the zipper teeth and configured to connect the two rows of zipper teeth when the slider is moved in a first direction and to disconnect the two rows of zipper teeth when the slider is moved in an opposite direction.

NEGATIVE POISSON`S RATIO MATERIALS FOR FASTENERS
20230189940 · 2023-06-22 ·

The disclosure describes a zipper including two rows of zipper teeth, in which at least some of the zipper teeth include a negative Poisson's ratio (NPR) foam material having a Poisson's ratio of between 0 and −1, and a slider movably attached to one of the rows of the zipper teeth and configured to connect the two rows of zipper teeth when the slider is moved in a first direction and to disconnect the two rows of zipper teeth when the slider is moved in an opposite direction.

DIFFERENT MATERIAL JOINING STRUCTURE AND DIFFERENT MATERIAL JOINING METHOD
20170349220 · 2017-12-07 ·

A different material joining structure has: a first panel made of a first metal material; a second panel made of a second metal material that has a higher conductivity than that of the first panel, is different from the first metal material, and at least a part of which faces the first panel; and a rivet for joining the first panel and the second panel, wherein the rivet is made of the first material, and includes a head portion that is embedded in the second panel in a non-penetrating manner and a bottom portion that abuts on the first panel, and wherein a nugget portion as a joint portion is disposed between the first panel and the bottom portion, the nugget portion being formed by resistance welding the rivet to the first portion with the rivet disposed between the first panel and the second panel.

DIFFERENT MATERIAL JOINING STRUCTURE AND DIFFERENT MATERIAL JOINING METHOD
20170349220 · 2017-12-07 ·

A different material joining structure has: a first panel made of a first metal material; a second panel made of a second metal material that has a higher conductivity than that of the first panel, is different from the first metal material, and at least a part of which faces the first panel; and a rivet for joining the first panel and the second panel, wherein the rivet is made of the first material, and includes a head portion that is embedded in the second panel in a non-penetrating manner and a bottom portion that abuts on the first panel, and wherein a nugget portion as a joint portion is disposed between the first panel and the bottom portion, the nugget portion being formed by resistance welding the rivet to the first portion with the rivet disposed between the first panel and the second panel.

Apparatus and methods for reducing corrosion of joining composite workpieces

The present disclosure relates a rivet body, including a rivet head and a rivet shank, composed of a different material than a mandrel used for insertion into a workpiece(s), the mandrel including a mandrel shaft and a mandrel cap. The rivet body receives the mandrel shaft, including the mandrel cap, through the rivet shank. The mandrel shaft is received by the installation tool, which rotates the rivet body, and the mandrel cap locally deforms workpieces(s) through friction riveting to install the rivet body. During the friction riveting, the fast-rotating rivet body is pushed into the workpiece(s) causing local deformation/melting where the mandrel cap contacts the workpiece(s). The mandrel cap creates a cavity which progresses through an upper surface and a lower surface of the workpiece(s).

Apparatus and methods for reducing corrosion of joining composite workpieces

The present disclosure relates a rivet body, including a rivet head and a rivet shank, composed of a different material than a mandrel used for insertion into a workpiece(s), the mandrel including a mandrel shaft and a mandrel cap. The rivet body receives the mandrel shaft, including the mandrel cap, through the rivet shank. The mandrel shaft is received by the installation tool, which rotates the rivet body, and the mandrel cap locally deforms workpieces(s) through friction riveting to install the rivet body. During the friction riveting, the fast-rotating rivet body is pushed into the workpiece(s) causing local deformation/melting where the mandrel cap contacts the workpiece(s). The mandrel cap creates a cavity which progresses through an upper surface and a lower surface of the workpiece(s).

Thin gel gasket and a method of making and using the same

A thin, cured gel gasket is disclosed, including methods of making the thin gel gasket and the use of the thin gel gasket in an aircraft joint. In one embodiment, the thin gel gasket has no skeleton or other structure and is comprised of only a cured polyurethane gel and has a thickness of less than about 12 mill. It is manufactured using a release film that is adapted in a number of ways to make release from the gel prior to use easier. In one method of making and using the thin gel gasket. it is applied to a joint which is subject to compression, in one embodiment, a lap joint of an aircraft fuselage.