Enhanced composite live hinge

Patent metadata

Field	Value
Publication number	US-11066859-B2
Application number	US-201916398414-A
Country	US
Kind code	B2
Filing date	Apr 30, 2019
Priority date	Aug 6, 2013
Publication date	Jul 20, 2021
Grant date	Jul 20, 2021

Abstract

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.

First claim

What is claimed is:

1. A method of making a hinged component, comprising the steps of:
sandwiching a layer of tensile fabric between a first layer of elastomer and a second layer of elastomer, thereby forming a layered structure;
locating the layered structure in a component forming tool;
introducing polymer-based material into the forming tool such that a first portion of polymer-based material overlaps one end of the layered structure and a second portion of polymer-based material overlaps an opposite end of the layered structure; and
forming the portions of polymer-based material to a desired shape using the forming tool so that the layered structure forms a live hinge between the first and second portions of polymer-based material;
wherein the first and second layers of elastomer are arranged in the forming tool so that the polymer-based material is prevented from infiltrating the tensile fabric.

2. The method of claim 1 , wherein at least some of the polymer-based material is in the form of curable sheets of pre-preg material, and the method further comprises the step of curing the pre-preg material while it is in the desired shape.

3. The method of claim 2 , wherein the tensile fabric or the elastomer or both are curable materials that are co-cured with the pre-preg material.

4. The method of claim 2 , wherein the elastomer cross-links with the pre-preg material during the step of curing.

5. The method of claim 1 , wherein the live hinge is formed without scoring any portion of the hinged component along a desired hinge region.

6. The method of claim 1 , wherein introducing the polymer-based material into the forming tool includes injecting a thermoplastic resin into a mold cavity of the tool.

7. The method of claim 1 , wherein:
at least part of the first and second layers of elastomer are interposed between the tensile fabric and the material of at least one of the first and/or second portions such that the elastomer blocks material of the first and second portions of material from infiltrating a hinge region of the tensile fabric.

8. The method of claim 1 wherein at least one of the first and second portions of polymer-based material is a structural composite comprising reinforcing fibers in a polymer matrix after the portions of polymer-based material are formed to the desired shape using the forming tool.

9. The method of claim 1 wherein at least one of the first and second portions of polymer-based material comprises a thermoplastic resin.

10. The method of claim 1 wherein the elastomer is co-curable with the tensile fabric and the first and second portions of polymer-based material.

Assignees

• Lockheed Corp

Inventors

• Malia Michael J
• Kaplun Brian
• Consalvi Dominick

Classifications

• B29C65/5021

  being multi-layered · CPC title

• B64C9/02

  Mounting or supporting thereof · CPC title

• B29C66/1122

  Single lap to lap joints, i.e. overlap joints (B29C66/45, B29C66/472, B29C66/52272 take precedence) · CPC title

• B29C66/7292

  coated (B29C66/72941 takes precedence) · CPC title

• B29C66/721

  Fibre-reinforced materials (B29C66/729 takes precedence) · CPC title