Rekonfigurierbares Herstellungssystem und Verfahren zur Herstellung von Verbundlaminaten

Details

Veröffentlichungs-Nr.

EP3628472

Aktenzeichen

EP19198297

Anmeldetag

19. September 2019

Veröffentlichung

2. November 2022

Erteilung

2. November 2022

Rechtsraum

EP

IPC

B29C70/22B29C70/30B29D99/00B29C70/54B29B11/16B29C31/08B29C53/04B29C70/34B29C70/38

Abstract

A manufacturing system includes a first mandrel (130), a second mandrel (150), and laminate securing mechanisms (190). The first mandrel (130) has a first mandrel surface (132) and a first mandrel surface edge (134). The second mandrel (150) has a second mandrel surface (152) and a second mandrel surface edge (154), and is positionable in a closed position in which the first mandrel surface edge and the second mandrel surface edge are in contact to form a continuous mandrel surface (162) collectively defined by the first mandrel surface and the second mandrel surface. The second mandrel translates to an open position defining a gap (166) between the first mandrel surface edge and the second mandrel surface edge for receiving a forming die (352,362). The laminate securing mechanisms (190) secure the composite laminate (400) on at least one of the first mandrel and the second mandrel during trimming and/or forming of the composite laminate.

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete