Verfahren zur Installation einer Halterung

Details

Veröffentlichungs-Nr.

EP2813432

Aktenzeichen

EP13171838

Anmeldetag

13. Juni 2013

Veröffentlichung

20. Dezember 2017

Erteilung

20. Dezember 2017

Rechtsraum

EP

IPC

B64F5/00B29C67/00

Abstract

The present invention relates to a method of installing a fixture (1) , such as a bracket, in a fuselage structure (F) of an aircraft (A), the method comprising the steps of: providing or generating a three-dimensional digital model (M) of the fixture (1) ; arranging a head (6) of an additive manufacturing apparatus (7) in the fuselage structure; and forming the fixture (1) in situ in the fuselage structure (F) with the head (6) of the additive manufacturing apparatus (7) based upon the digital model (M) of the fixture (1) ; wherein the fixture (1) is installed in the fuselage structure (F) by bonding or fusing the fixture (1) to the fuselage structure as the fixture (1) is formed. Also, the invention provides a fixture (1) , such as a bracket, which is generated in situ in a fuselage structure (F) of an aircraft based upon a three-dimensional digital model (M), wherein the fixture (1) is bonded or fused to the fuselage structure (F) as the fixture (1) is formed.

Anmelder

Firma

Airbus Operations GmbH

Land

🇩🇪 Deutschland

Fachgebiete