Montageanordnung

Details

Veröffentlichungs-Nr.

EP2784290

Aktenzeichen

EP14157135

Anmeldetag

28. Februar 2014

Veröffentlichung

17. Mai 2017

Erteilung

17. Mai 2017

Rechtsraum

EP

IPC

F02C7/32B60R16/02F01D21/04F01D25/28H05K7/14F01D21/14

Abstract

A rigid electrical raft (200) is provided to a gas turbine engine via a fusible mount arrangement (400). The rigid electrical raft may be a part of an electrical system of the gas turbine engine, for example a part of the electrical harness. The fusible mount (400) is arranged to break when a predetermined load is applied. The rigid electrical raft may be attached to a fan case of the engine, and the predetermined load may that which results from a fan blade being released from the hub. This ensures that the rigid electrical raft is protected from the load.

Anmelder

Firma

Rolls-Royce plc

Land

🇬🇧 Großbritannien

Fachgebiete