Method and system for producing a panel member for an airframe

Patent metadata

Field	Value
Publication number	US-10059066-B2
Application number	US-201414463086-A
Country	US
Kind code	B2
Filing date	Aug 19, 2014
Priority date	Aug 28, 2013
Publication date	Aug 28, 2018
Grant date	Aug 28, 2018

Abstract

A method of producing a composite panel member, especially a composite panel member having a foam core sandwich structure for an airframe of an aircraft or spacecraft, including: providing at least one fiber reinforcement layer in a panel molding tool; moving or transferring the molding tool to an infusion station that is pre-heated to an infusion temperature and infusing the fiber reinforcement layer in the molding tool with a polymer resin; moving or transferring the molding tool to a curing station that is pre-heated to a curing temperature and curing the at least one resin-infused fiber reinforcement layer in the molding tool to form a composite panel member; and moving or transferring the molding tool to a cooling station that is provided at a cooling temperature and cooling the composite panel member in the molding tool.

First claim

The invention claimed is:

1. A system for producing a composite panel member with a sandwich structure, the system comprising:
a molding tool for receiving at least one fiber reinforcement layer and for molding a panel;
an infusion station for infusing the at least one fiber reinforcement layer in the molding tool with a polymer resin, wherein the infusion station is adapted to be heated to an infusion temperature;
a curing station for curing the at least one resin-infused fiber reinforcement layer in the molding tool to form a composite panel member, wherein the curing station is configured to be heated to a curing temperature;
a cooling station for cooling the composite panel member in the molding tool, wherein the cooling station is configured to be provided at or heated to a cooling temperature; and
a transfer mechanism for moving or transferring the molding tool from the infusion station to the curing station and from the curing station to the cooling station;
wherein the infusion station, the curing station, and the cooling station are arranged in series adjacent to one another and are provided as distinct regions of a single heating apparatus.

2. The system according to claim 1 , wherein the transfer mechanism includes a sliding or rolling transport device arranged to transport the molding tool between the infusion station, the curing station, and the cooling station.

3. The system according to claim 1 , wherein the molding tool has at least two mold parts which together define a mold cavity for accommodating the at least one fiber reinforcement layer and for molding the panel, wherein the mold parts are configured to hold or clamp the panel member against thermal expansion when the molding tool is closed; and wherein the system further comprises a digital controller for controlling or regulating a temperature in the infusion station and/or in the curing station and/or in the cooling station.

4. The system according to claim 2 , wherein the transfer mechanism includes a lay-up station for placement of the at least one fiber reinforcement layer in the molding tool.

Assignees

• Airbus Operations Gmbh

Inventors

• Zuardy Ichwan
• Grase Karim
• Jessrang Mathias
• Roehrig Martin

Classifications

• B29K2105/256

  Sheets, plates, blanks or films · CPC title

• B29C70/443 Primary

  and impregnating by vacuum or injection · CPC title

• C08J5/04

  Reinforcing macromolecular compounds with loose or coherent fibrous material · CPC title

• B29K2105/04

  cellular or porous · CPC title

• B29K2105/0872

  Prepregs · CPC title