Highly loaded frame of an aircraft fuselage with a lattice structured web

A frame of a fuselage section of an aircraft that receives external loads, such as the rear section that receives the loads of the tail planes, comprising a first sector configured specifically to withstand these external loads and a second sector along the remaining perimeter of the fuselage, said...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	AREVALO RODRIGUEZ ELENA, CRUZ DOMINGUEZ FRANCISCO JOSE
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!