B29K2305/00

System and method for bending a hollow core sheet using rods
11267217 · 2022-03-08 ·

A hollow core sheet having a plurality of channels and at least one bendable reinforcement rod adapted in width and thickness to a given channel dimensions for insertion inside a channel wherein the method of insertion consists in the steps of having the at least one bendable reinforcement rod having either or both of the width or the thickness having an outer dimension (OD) set between 0.50 0.75 of the given dimension of the channel with a variation of 5%.

Low cost joined cascade
11156185 · 2021-10-26 · ·

A cascade array includes a first strongback having a first thermoset or thermoplastic composite material. The cascade array further includes a second strongback having a second thermoset or thermoplastic composite material. The cascade array further includes a first vane that is coupled to the first strongback and the second strongback and includes a third thermoset or thermoplastic composite material.

Low cost joined cascade
11156185 · 2021-10-26 · ·

A cascade array includes a first strongback having a first thermoset or thermoplastic composite material. The cascade array further includes a second strongback having a second thermoset or thermoplastic composite material. The cascade array further includes a first vane that is coupled to the first strongback and the second strongback and includes a third thermoset or thermoplastic composite material.

Pipe-forming apparatus for spiral pipe and pipe-forming method thereof

A pipe-forming apparatus with which a spiral pipe can be formed using a simple configuration without an inner periphery restriction body. A driving part (10) of a pipe-forming apparatus (3) presses a following strip portion (92) toward a pipe end portion (91e) of a preceding spiral pipe portion (91) obliquely with respect to a machine-height direction HD. A pipe end guide is constrained in a machine-width direction WD with respect to the pipe end portion, and slidably engaged in a propelling longitudinal direction LD. A pressing force for the following strip portion provides a fitting force between the following strip portion and the pipe end portion, and a propelling force for forward propulsion. A pipe is formed in a state where a part other than a partial part at which the pipe-forming apparatus is provided in a circumferential direction of the pipe end portion is released from the pipe-forming apparatus.

Methods of producing thermoplastic composites using fabric-based thermoplastic prepregs
11141949 · 2021-10-12 · ·

A thermoplastic product includes a fabric-based reinforcing sheet and a polymerized thermoplastic material. The fabric-based reinforcing sheet is wound about a mandrel to form a plurality of layers having a cross-sectional shape that corresponds to the mandrel. The fabric-based reinforcing sheet includes a plurality of fiber bundles, which may have a bidirectional orientation or configuration. A polymerized thermoplastic material is disposed within each layer of the fabric-based reinforcing sheet. The polymerized thermoplastic material bonds each layer of the fabric-based reinforcing sheet to an adjacent layer.

Methods of producing thermoplastic composites using fabric-based thermoplastic prepregs
11141949 · 2021-10-12 · ·

A thermoplastic product includes a fabric-based reinforcing sheet and a polymerized thermoplastic material. The fabric-based reinforcing sheet is wound about a mandrel to form a plurality of layers having a cross-sectional shape that corresponds to the mandrel. The fabric-based reinforcing sheet includes a plurality of fiber bundles, which may have a bidirectional orientation or configuration. A polymerized thermoplastic material is disposed within each layer of the fabric-based reinforcing sheet. The polymerized thermoplastic material bonds each layer of the fabric-based reinforcing sheet to an adjacent layer.

Injection molded composite blank and guide

This specification discloses an article of manufacture. The article of manufacture has at least one structural blank and at least one guide. The structural blank has a plurality of oriented fiber plies in a thermoplastic matrix. The guide has a plurality of random dispersed fibers in a thermoplastic matrix. The guide is affixed to the structural blank by injection molding and over molding the guide onto the structural blank. The article of manufacture can take a number of forms for use in industries such as aircraft, automobiles, motorcycles, bicycles, trains or watercraft.

Injection molded composite blank and guide

This specification discloses an article of manufacture. The article of manufacture has at least one structural blank and at least one guide. The structural blank has a plurality of oriented fiber plies in a thermoplastic matrix. The guide has a plurality of random dispersed fibers in a thermoplastic matrix. The guide is affixed to the structural blank by injection molding and over molding the guide onto the structural blank. The article of manufacture can take a number of forms for use in industries such as aircraft, automobiles, motorcycles, bicycles, trains or watercraft.

Systems and methods for joining blade components of rotor blades

Systems and methods for joining blade components of a rotor blade are provided. A method includes positioning a first blade component and a second blade component such that a joint location of the first blade component and a joint location of the second blade component are proximate each other. The method further includes applying a force to an outer surface of the second blade component and an opposing force to an inner surface of the second blade component. The force and opposing force maintain an aerodynamic contour of the second blade component. The method further includes connecting the joint location of the first blade component and the joint location of the second blade component together.

Systems and methods for joining blade components of rotor blades

Systems and methods for joining blade components of a rotor blade are provided. A method includes positioning a first blade component and a second blade component such that a joint location of the first blade component and a joint location of the second blade component are proximate each other. The method further includes applying a force to an outer surface of the second blade component and an opposing force to an inner surface of the second blade component. The force and opposing force maintain an aerodynamic contour of the second blade component. The method further includes connecting the joint location of the first blade component and the joint location of the second blade component together.