The present invention relates to a booster seat comprising a seat shell with a lower face for supporting the seat shell and an upper face, on which a seat base and lateral seat cushion regions and backrest regions that delimit the seat base laterally and rearwards are provided. The lower face of the seat shell has a stacking contour which is designed to provide a stacking capability on the upper face of the seat shell. The invention also relates to a booster seat comprising a strap system that has four eyelets, wherein one retaining strap is allocated to a pair of eyelets. Two eyelets are arranged in the front outer region of each lateral seat cushion region, while two eyelets are arranged in the rear outer region of each lateral seat cushion region or in the lateral outer region of the back region. The invention further relates to a method for producing a booster seat of this type.

A foamed cotton mop head has a mounting member (1) having a joint portion (11) mounted on a mounting plate (12) extending downward and a foamed cotton head (2) mounted on the mounting member (1); wherein, the mounting plate (12) is inserted downward into the top of the foamed cotton head (2) and attached to the foamed cotton head (2), forming a framework for the foamed cotton head (2). The whole foam cotton head (2) is partially supported by the mounting plate (12), so that the foamed cotton head (2) is kept at certain strength, not floppy, and difficult to shake and deform during mopping. The mopping operation becomes easier, and the hand feeling is better. During the water squeezing, it is ensured that the surface of the foamed cotton head are subjected to the squeezing force evenly and difficult to deform. In addition, it is easier for the foamed cotton head to pass through the elastic bayonet of the water squeezing frame.

A system for insulating a structural element in a motor vehicle including a structural element having a first constituent part and a second constituent part which are joined together at a first joining point and a second joining point and form a cavity. The system furthermore includes a device having a carrier and a first expandable adhesive, wherein the carrier is arranged on the first constituent part of the structural element by way of a fastening element. The system furthermore includes a second expandable adhesive which is arranged on the second constituent part of the structural element. In this case, the first expandable adhesive and the second expandable adhesive are configured, and arranged, in such a way that, after the adhesives have been expanded, the device and the second expandable adhesive substantially completely fill a cross section of the structural element.

A method of forming a building panel includes embossing dimples into a sheet, where the dimples extend outward from a plane, and expanding a foam core onto the plane and into portions of the dimples. The method may include forming dimples that are convex relative to the plane and the foam core or the sheet having a thin foil having a plastic protective coating. The method may include attaching a cellulosic layer to the foam core opposite the plane. Additionally, flow channels may be formed in the sheet between the dimples, such that expanding the foam core onto the plane substantially fills both the dimples and the flow channels. The method may include embossing concave dimples onto the plane and the foam core, such that expanding the foam core onto the plane substantially fills the concave dimples. The foam core and sheet may bond without adhesives.

There is disclosed a method of applying activatable material to a member of an article of manufacture such as an automotive vehicle. According to the method, the activatable material is provided to an applicator followed by applying the activatable material to the member wherein the activatable material is attached by way of a mechanical interlock via one or more through-holes.

Methods of manufacturing of aerospace structures are disclosed. More specifically, methods of manufacturing relatively lightweight yet strong aerospace structures. In one embodiment, the method includes the addition of a volume of a rigid and flexible polyurethane mixture into a mold to create a composite structure. In one aspect, the method includes the integration of special structures within a larger structure to remove traditionally structurally weak or vulnerable areas.

An electrically decoupled jet engine. The electrically decoupled jet engine includes a combustion chamber which creates a toroidal flow of air and a rotational electric motor which drives a fuel supply into the combustion chamber. The toroidal flow of air is mixed with the fuel and combusted in the combustion chamber to create thrust.

The present disclosure relates to a clothing treatment device capable of omitting a frame for structurally connecting an inner case and a cabinet by filling a foaming agent between the inner case and the cabinet forming an appearance. The clothing treatment device comprises a cabinet having an opening at the front thereof: a door which is rotatably provided in front of the opening to open and close the opening; an inner case which is provided in the cabinet to form an accommodation space in which clothes are accommodated, and a hot air supply unit which is provided at the lower portion of the inner case to supply at least one of hot air and moisture to the accommodation space, wherein the inner case is formed of a styrene resin that maintains adhesion to the foaming agent injected into the inner portion of the cabinet.

Fabricate a panel (5) by building a sacrificial relief (10) by an additive process of multilayer deposition, applying a facade layer (20,30) over the sacrificial relief so as to conform to the contour of the sacrificial relief, depositing a foamable composition (40, 50, 60) over the facade layer.

A system for insulating a structural element in a motor vehicle including a structural element having a first constituent part and a second constituent part which are joined together at a first joining point and a second joining point and form a cavity. The system furthermore includes a device having a carrier and a first expandable adhesive, wherein the carrier is arranged on the first constituent part of the structural element by way of a fastening element. The system furthermore includes a second expandable adhesive which is arranged on the second constituent part of the structural element. In this case, the first expandable adhesive and the second expandable adhesive are configured, and arranged, in such a way that, after the adhesives have been expanded, the device and the second expandable adhesive substantially completely fill a cross section of the structural element.