Auskleidung für Drehsicherungslasche und Keramisches Bauteil

Details

Veröffentlichungs-Nr.

EP4276286

Aktenzeichen

EP23173360

Anmeldetag

15. Mai 2023

Veröffentlichung

18. Februar 2026

Erteilung

18. Februar 2026

Rechtsraum

EP

IPC

F01D25/24

Abstract

A gas turbine engine (20) includes a first component (62), a second component (64), an anti-rotation tab (80), and a liner (82). The first component (62) has a first wall (66) that includes a first slot (72), and the second component (64) has a second wall (68) that includes a second slot (74) that is in register with the first slot (72) to define a groove (76). The anti-rotation tab (80) extends into the groove (76) and limits rotation of the first component (62) and the second component (64). The liner (82) lines the groove to limit wear between the anti-rotation tab (80) and the first component (62) and between the anti-rotation tab (80) and the second component (64).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA

Fachgebiete