Aufhängungssystem für ein Flugzeughilfstriebwerk

Details

Veröffentlichungs-Nr.

EP3040281

Aktenzeichen

EP14382585

Anmeldetag

30. Dezember 2014

Veröffentlichung

16. Oktober 2019

Erteilung

16. Oktober 2019

Rechtsraum

EP

IPC

F16F15/08B60K5/12B64D27/26F16B5/02B64D41/00

Abstract

A suspension system for an aircraft auxiliary power unit located in a fuselage structure, the system comprising: - struts (10), - auxiliary power unit attachment brackets (51, 52) for connecting the strut (10) to the auxiliary power unit (30), - vibration isolators (5) for joining the struts (10) and the auxiliary power unit attachment bracket (51, 52), - a cone-bolt (1) attached to the auxiliary power unit attachment brackets (51, 52) and having a longitudinal threaded hollow, - an inner bolt (2) partially located within the hollow of the cone-bolt (1) and threaded to it (1), - an outer bolt (3) having a longitudinal through-hole and partially located within the hollow of the cone-bolt (1) and comprising an external thread that engages the thread of the cone-bolt (1), the inner bolt (2) extending across the hollow of said outer bolt (3).

Anmelder

Firma

Airbus Operations S.L.

Land

🇪🇸 Spanien

Fachgebiete