Verfahren und Systeme zur Herstellung von Verbundteilen

Details

Veröffentlichungs-Nr.

EP4530051

Aktenzeichen

EP24186293

Anmeldetag

3. Juli 2024

Veröffentlichung

2. April 2025

Rechtsraum

EP

IPC

B29C43/36B30B5/02B29C35/02B29C43/10B29C70/34B29C70/44B29C70/54

Abstract

A method for forming composite parts includes loading an uncured composite material into a middle cavity of a chamber between an upper membrane and a lower membrane, wherein a lower cavity is defined below the lower membrane, and wherein an upper cavity is defined above the upper membrane, wherein a forming tool is disposed within the upper cavity. A vacuum is applied to the upper cavity, the middle cavity, and the lower cavity to remove at least a portion of gas entrapped within the uncured composite material. The vacuum is released from the upper cavity and the lower cavity, and the chamber is heated to a forming temperature of the uncured composite material. Pressure is controlled in the upper cavity and the lower cavity to form the heated composite material, wherein a greater pressure is applied to the lower cavity than to the upper cavity such that a pressure differential between the lower cavity and the upper cavity causes the heated composite material to form around the forming tool. The chamber is heated to a curing temperature to cure the heated composite material.

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete