Verfahren und Vorrichtung zur Prüfung eines Bauteils eines Gasturbinentriebwerks

Details

Veröffentlichungs-Nr.

EP4756188

Anmeldetag

5. November 2025

Veröffentlichung

10. Juni 2026

Rechtsraum

EP

Abstract

A method of inspecting a component of a gas turbine engine for an aircraft, in which a housing circumferentially surrounds the component so as to define an annular space between the housing and the component. The method comprises guiding a guide line into the annular space through an opening to the annular space and around the component in a circumferential direction, and withdrawing the guide line through the opening, such withdrawal moving a probe that is connected to the guide line in a circumferential direction around the component for performing an inspection of the compressor.

Anmelder

Firma

Rolls-Royce plc

Land

🇬🇧 Großbritannien