Hybrider Scharnier- und Verschlussriegel

Details

Veröffentlichungs-Nr.

EP2690018

Aktenzeichen

EP13177876

Anmeldetag

24. Juli 2013

Veröffentlichung

11. März 2020

Erteilung

11. März 2020

Rechtsraum

EP

IPC

B64D27/12B64D27/18B64D29/02B64D33/04

Abstract

A hybrid beam (500) for support of a nacelle panel of a jet engine comprises a first longitudinal composite panel (402) and a second longitudinal composite panel (404), wherein the first longitudinal composite panel (402) is integrally affixed to the second longitudinal composite panel (404) along a longitudinal edge (406). The composite panels form a composite beam structure (400) that is substantially open with a cross-section that is generally "L-shaped". A plurality of hinge stations (540) are affixed to a first side of the first longitudinal composite panel (402) and at least one track guide (520) is disposed on a second side of the first longitudinal composite panel (402). The track guides (520) receive a head portion of a slider (550) that is fixed to the translating jet engine nacelle panel. Each hinge station (540) further comprises a bushing for defining a center of rotation for the jet engine nacelle panel relative to the beam (500).

Anmelder

Firmen

Rohr Inc.
Layland, Michael J.
James, Norman J.
Forsey, David
Soria, Christian

Land

🇺🇸 USA

Fachgebiete