Motorzubehörmontageanordnung

Details

Veröffentlichungs-Nr.

EP4741647

Anmeldetag

7. November 2025

Veröffentlichung

13. Mai 2026

Rechtsraum

EP

IPC

F02C7/32, F16F7/14

Abstract

A mounting arrangement includes a casing (17) of an aircraft engine (10) extending around an axis (11), an accessory (22), and a bracket (40) for mounting the accessory to the casing (17). The bracket (40) includes a first bracket segment (44') coupled to the casing (17) at a first mounting point, a second bracket segment (48') coupled to the accessory at a second mounting point, and a wire rope isolator (54') including a looped wire (56') coupling the first bracket segment (44') to the second bracket segment (48'). The first bracket segment (44') at the first mounting point and the second bracket segment (48') at the second mounting point extend in intersecting planes.

Anmelder

Firma

Pratt & Whitney Canada Corp.

Land

🇨🇦 Kanada

Fachgebiete