Composite anti-crash structure with lateral restraint for aircraft

The structure has hollow profiles (51) extending remotely and with respect to a shroud (19). The profiles are fixed to a flange (54) or a wall (18H) and are arranged to serve as a support to a upper part of a beam (18V), where the upper part is separated from the shroud following the rupture of the...

Ausführliche Beschreibung

Gespeichert in:

Bibliographische Detailangaben
1. Verfasser:	PAYEN, HERVE
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS PRODUCING PARTICULAR ARTICLES FROM PLASTICS OR FROM SUBSTANCESIN A PLASTIC STATE TRANSPORTING WORKING OF PLASTICS WORKING OF SUBSTANCES IN A PLASTIC STATE, IN GENERAL
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!

Beschreibung
Zusammenfassung:	The structure has hollow profiles (51) extending remotely and with respect to a shroud (19). The profiles are fixed to a flange (54) or a wall (18H) and are arranged to serve as a support to a upper part of a beam (18V), where the upper part is separated from the shroud following the rupture of the beam. A bend wall (92) delimiting a fuel tank is supported against the beam and transmits a lateral thrust to the beam.