System und Verfahren zur Herstellung einer Flugzeugmotorkomponente

Details

Veröffentlichungs-Nr.

EP4822466

Anmeldetag

13. April 2026

Veröffentlichung

14. Oktober 2026

Rechtsraum

EP

IPC

G05B19/401

Abstract

A method (300) for manufacturing a component of an aircraft engine (10) includes positioning two sub-components of the component in a fixture of a CNC machine, and performing, with a 3D scanner, a first scan of the two sub-components on the fixture. A predetermined tool pathway for combining the two sub-components is updated based on the first scan to establish a modified tool pathway for combining the two sub-components. A welding procedure is performed to combine the two sub-components based on the modified tool pathway to form the component. Using the 3D scanner, and with the component retained in place in the fixture, a second scan of the component is performed to identify the presence of one or more surface defects on the component. In response to identifying the presence of the surface defect(s), a corrective procedure is performed to correct the one or more surface defects on the component.

Anmelder

Firma

Pratt & Whitney Canada Corp.

Land

🇨🇦 Kanada

Fachgebiete