Gasturbinenmotor mit Inspektionsport und Verfahren zur Verwendung davon

Details

Veröffentlichungs-Nr.

EP4722495

Anmeldetag

30. September 2025

Veröffentlichung

8. April 2026

Rechtsraum

EP

Abstract

A gas turbine engine (22) is provided that includes a compressor section (26), a combustor section (28), a turbine section (30), and an inspection port (74). The turbine section (30) includes a rotor stage (66A,B) and a stator vane stage (64A.B). A core gas path (36) extends through the compressor section (26), the combustor section (28), and the turbine section (30). The inspection port (74) is disposed within the turbine section (30). The inspection port is configured to provide access through a portion of the core gas path (36) that extends within the turbine section (30) and to a component disposed radially inside of the portion of the core gas path (36) that extends within the turbine section (30).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA