Montageverfahren von Zusammengesetzten Kernverbundstrukturrandfugen

Details

Veröffentlichungs-Nr.

EP3360801

Aktenzeichen

EP17203716

Anmeldetag

27. November 2017

Veröffentlichung

29. März 2023

Erteilung

29. März 2023

Rechtsraum

EP

IPC

B64G1/00B64G1/40B29C65/50F16B5/02F16B5/01F16B11/00B29C65/00// B29L31/30

Abstract

A composite wall assembly edge joint, includes a first composite buildup pad secured to a first composite face sheet with the first composite buildup pad having a first tapered section with a first inclined surface which extends in a first direction and having a second section which extends from the first tapered section with a second surface which extends in a second direction, different from the first direction, toward a first end of the first composite face sheet. The assembly further includes a composite flute core member, having a tapered first portion secured to the first tapered section; a second portion secured to the first composite face sheet; and a third portion which extends in the second direction, away from the tapered first portion, toward the first end of the first composite face sheet secured to the second section.

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete