Lüfterschaufelverkleidungsanordnung für ein Flugzeugantriebssystem

Details

Veröffentlichungs-Nr.

EP4760056

Anmeldetag

12. Dezember 2025

Veröffentlichung

17. Juni 2026

Rechtsraum

EP

IPC

F01D11/00

Abstract

A fan blade fairing assembly (68) for a gas turbine engine (24) includes a fairing body (74), a replaceable component (132B), and a bonding assembly (128). The fairing body (74) includes an outer wall (82), a first sidewall (84), and a second sidewall (86). The outer wall (82) extends between and connects the first sidewall (84) and the second sidewall (86). The replaceable component (132B) is bonded onto the fairing body (74). The bonding assembly (128) includes an electrically debonding adhesive (130), a first conductive member (134), and a second conductive member (136). The electrically debonding adhesive (130) bonds the replaceable component (132B) onto the fairing body (74). The electrically debonding adhesive (130) is disposed between the first conductive member (134) and the second conductive member (136).

Anmelder

Firma

RTX Corporation

Land

🇺🇸 USA