Statoranordnung mit Halteclip für Gasturbinenmotor

Details

Veröffentlichungs-Nr.

EP3406854

Aktenzeichen

EP18173421

Anmeldetag

21. Mai 2018

Veröffentlichung

23. September 2020

Erteilung

23. September 2020

Rechtsraum

EP

IPC

F01D9/04

Abstract

A stator assembly (60) of a gas turbine engine according to an example of the present disclosure includes, among other things, a first shroud (62) extending about an assembly axis (X) to bound a flow path (FP). The first shroud (62) defines a first shroud opening (68). An airfoil (66) has an airfoil body (66A) extending from a first end portion (66B). The first end portion (66B) is received in the first shroud opening (68) and defines a pair of airfoil openings (66D). A retention clip (72) has an intermediate portion (72A) connecting a first leg portion (72B) and a second leg portion (72C). The intermediate portion (72A) is compressible to position the first and second leg portions (72B, 72C) in the pair of airfoil openings (66D) such that the retention clip (72) limits movement of the airfoil (66) relative to the first shroud (62).

Anmelder

Firmen

Raytheon Technologies Corporation
United Technologies Corporation

Land

🇺🇸 USA

Fachgebiete