Patent classifications
B29D99/0021
Foamed structure, resin panel, method of manufacturing resin panel, method of manufacturing resin laminated body and foamed body
The first aspect of the present invention provides a foamed structure, comprising: a first foamed body extending in a first direction; a second foamed body extending in the first direction and facing the first foamed body with a gap interposed therebetween; and a reinforcement disposed in the gap between the first foamed body and the second foamed body, the reinforcement having an elongated shape, wherein the first foamed body has a portion overlapping with the second foamed body in the first direction view.
Molded Multi-Part Polymer Structural Plastic Building Assembly System For Land and Water
A building assembly system that comprises thermoformed high density polyethylene molded components filled with high density polyurethane foam. The molded components are configured in a cube or triangle form and secured against a steel frame to provide a habitable constructed unit. The composition of the high density polyethylene molded components filled with high density polyurethane foam meets standards for the American Society for Testing and Materials for a habitable structure used by humans. The habitable structure can be used on land or water.
Method of additive manufacturing an internal wave sparse structure with varying geometry for localized tunable structural properties throughout a part
Disclosed are three-dimensional parts, such as orthotics and prosthetics, having sinusoidal wave pattern infill structures first and second boundary walls. Also disclosed are printers or systems configured to manufacture such parts, as well as methods of manufacturing such parts. The sinusoidal wave pattern infill structures are formed between, and normal to, the first and second boundary walls and are configured to provide locally tunable structural properties in different regions of the part.
STRUCTURED PANEL WITH NON-PARALLEL CAVITY WALLS
A panel includes a corrugated base with base corrugations configured from first base segments and second base segments. A first of the base corrugations includes a first of the first base segments and a first of the second base segments that is non-parallel to the first of the first base segments. The first of the base corrugations forms a first channel that extends laterally between and longitudinally along the first of the first base segments and the first of the second base segments. A corrugated stringer includes a plurality of stringer corrugations arranged longitudinally along and within the first channel. The stringer corrugations are configured from first stringer segments and second stringer segments. A first of the stringer corrugations includes a first of the first stringer segments and a first of the second stringer segments that is non-parallel to the first of the first stringer segments.
COMPOSITE PANEL COMPRISING AN INTEGRATED ELECTRICAL CIRCUIT AND MANUFACTURING METHOD THEREOF
Here are described composite panels comprising at least one integrated or embedded electrical circuit, their methods of manufacturing and their use in the aeronautic and aircraft industries. Also described are aircraft components comprising the composite panel as defined herein.
Composite pressure vessel assembly and method of manufacturing
A composite pressure vessel assembly includes a first vessel having a first inner layer and a second vessel having a second inner layer. An outer layer of the assembly is in contact with and substantially envelopes the first and second inner layers. A junction of the assembly has outer boundaries defined by segments of the first inner layer, the second inner layer and the outer layer. A cross-layered component of the assembly is disposed in the junction, the first and second inner layers and the outer layer for adding strength to the junction and restricting delamination.
Composite core with reinforced plastic strips and method thereof
Some embodiments provide a core member for a composite panel that includes a hollow cell network structure, such as a honeycomb arrangement for example, and reinforced plastic strips positioned on a portion of the continuous honeycomb structure. The honeycomb structure and the solid plastic strips may be fastened together using heat and/or pressure applications. Additionally, the method for the production of the core member is provided.
Molded multi-part polymer structural plastic building assembly system for land and water
A building assembly system that comprises thermoformed high density polyethylene molded components filled with high density polyurethane foam. The molded components are configured in a cube or triangle form and secured against a steel frame to provide a habitable constructed unit. The composition of the high density polyethylene molded components filled with high density polyurethane foam in combination with its connection with a steel frame meets standards for the American Society for Testing and Materials for a habitable structure used by humans. The habitable structure can be used on land or water.
FLOOR BOARD, AND METHOD AND APPARATUS FOR MANUFACTURING SAME
A floor board, and a method and apparatus for manufacturing same. The floor board (100) comprises a polyurethane-foam board (110). The polyurethane-foam board (110) is made of a polyurethane foam material foamed from a polyurethane foam raw material. The polyurethane-foam board (110) is provided with a plurality of linear members (120) passing though the polyurethane-foam board in a predetermined direction. The plurality of linear members (120) are arranged at intervals. The polyurethane-foam board (110) is foaming-molded by continuous drawing.
Composite Panel Sandwich Structures with Integrated Joints
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.