Verfahren zur Inspektion von Kühlungsöffnungen in einer Turbinenmotorkomponente

Details

Veröffentlichungs-Nr.

EP4737691

Anmeldetag

15. August 2022

Veröffentlichung

6. Mai 2026

Rechtsraum

EP

IPC

F01D5/28, F01D5/18F01D9/06(SIEMENS AG et al.)

Abstract

A manufacturing method is provided. During this method, a preform component (60') for a turbine engine is provided that includes a substrate (74). A meter section (102) of a cooling aperture (64) is formed in the substrate (74'). An external coating (76',78') is applied over the substrate. At least a portion of the substrate (74') and the external coating (76',78') is scanned with an imaging system (156) to provide scan data indicative of an internal structure of the portion of the substrate (74') and the external coating (76',78'). A diffuser section of the cooling aperture is formed in the external coating (76',78') and the substrate (74') based on the scan data.

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA