Flugzeugtriebwerksfrostschutzsperranordnung und Verfahren

Details

Veröffentlichungs-Nr.

EP2846023

Aktenzeichen

EP14172649

Anmeldetag

17. Juni 2014

Veröffentlichung

3. Januar 2018

Erteilung

3. Januar 2018

Rechtsraum

EP

IPC

F02C7/047B64D33/02

Abstract

There is provided an aircraft engine anti-icing (EAI) barrier assembly. The aircraft EAI barrier assembly has a slip joint subassembly having a forward end and an aft end. The forward end is configured for fixed attachment at a forward bulkhead of an engine of an aircraft, and an aft end with a sliding joint. The aircraft EAI barrier assembly has a barrier subassembly attached through an aft bulkhead and has two mount pads configured for joined sealed attachment around the aft end of the slip joint subassembly to form a barrier to an engine inlet of the engine.

Anmelder

Firma

The Boeing Company

Land

🇺🇸 USA

Fachgebiete