Method and system of vacuum assisted resin transfer moldings for repair of composite materials and structure

US9944026B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9944026-B2
Application numberUS-201214115886-A
CountryUS
Kind codeB2
Filing dateMay 4, 2012
Priority dateMay 6, 2011
Publication dateApr 17, 2018
Grant dateApr 17, 2018

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

The present disclosure provides a method of repairing a damaged portion of a panel formed of composite material. The method includes preparing the damaged portion for repair and applying a pressure responsive adhesive layer to substantially cover the damaged portion. The method also includes disposing a vacuum-assisted resin transfer molding repair patch assembly to substantially cover the damaged portion and substantially covering the repair patch assembly with a vacuum bag assembly. Resin is introduced into and impregnates the repair patch assembly. The repair patch assembly is cured after being impregnated.

First claim

Opening claim text (preview).

What is claimed is: 1. A method of repairing a damaged portion of a panel formed of composite material, comprising: preparing the damaged portion for repair; disposing a vacuum-assisted resin transfer molding repair patch assembly to substantially cover the damaged portion, wherein the repair patch assembly is a preassembled repair patch assembly including an injection plate, a scrim material, and an injection tube defining the inlet side of the repair patch assembly; wherein the scrim material includes a plurality of openings to provide space for a liquid resin to occupy; covering the repair patch assembly with a first vacuum bag assembly; disposing a heat blanket over the first vacuum bag assembly; covering the heat blanket and the first vacuum bag assembly with a second vacuum bag assembly; introducing liquid resin through the injection plate of the repair patch assembly; impregnating the repair patch assembly including the scrim material with the introduced liquid resin by independently drawing a vacuum inside the first vacuum bag assembly and the second vacuum bag assembly to substantially impregnate the repair patch assembly including the scrim material with the liquid resin; heating the repair patch assembly with the heat blanket to ensure full impregnation of the repair patch assembly including the scrim material; curing the repair patch assembly to provide an adhesive joint between the panel and the repair patch assembly; and removing the first vacuum bag assembly, the second vacuum bag assembly, and the heat blanket while not removing the repair patch assembly from the panel. 2. The method of claim 1 , wherein the preparing step comprises removing the damaged portion from the panel. 3. The method of claim 1 , wherein the preparing step comprises replacing the damaged portion with a honeycomb core material. 4. The method of claim 1 , further comprising cleaning the damaged portion and nearby area with a cleansing tool. 5. The method of claim 1 , further comprising: preheating the repair patch assembly to a desired temperature; and removing air or volatile material from the repair patch assembly. 6. The method of claim 1 , further comprising: mixing the liquid resin in a cartridge; and coupling the cartridge to an inlet side of the repair patch assembly. 7. The method of claim 1 , further comprising discontinuing the impregnating step when the liquid resin begins to pass through an outlet side of the repair patch assembly. 8. The method of claim 1 , further comprising controlling the introducing step by opening or closing an inlet valve or outlet valve. 9. The method of claim 1 , wherein the curing step comprising increasing the temperature of the repair patch assembly to a temperature greater than 100° C. 10. The method of claim 1 , wherein scrim material having a predetermined thickness configured to provide an adhesive layer thickness between the repair patch assembly and the damaged portion. 11. The method of claim 1 , wherein the scrim material is one of a gauze or a textile material.

Assignees

Inventors

Classifications

  • B29C73/02Primary

    using liquid or paste-like material (B29C73/16 takes precedence) · CPC title

  • using patches sealing on the surface of the article (B29C73/14 takes precedence) · CPC title

  • Heating or curing, e.g. crosslinking or vulcanizing {during moulding, e.g. in a mould}(cold vulcanisation B29C35/18 {; vulcanising tyres, presses therefor B29D30/0601}) · CPC title

  • for polishing, roughening, buffing or sanding the area to be repaired · CPC title

  • Apparatus therefor, e.g. for applying (B29C73/30 takes precedence) · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US9944026B2 cover?
The present disclosure provides a method of repairing a damaged portion of a panel formed of composite material. The method includes preparing the damaged portion for repair and applying a pressure responsive adhesive layer to substantially cover the damaged portion. The method also includes disposing a vacuum-assisted resin transfer molding repair patch assembly to substantially cover the dama…
Who is the assignee on this patent?
Pipes R Byron, Coker Ian Cameron, Adams Douglas Edward, and 3 more
What technology area does this patent fall under?
Primary CPC classification B29C73/02. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 17 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).