STRUCTURE OF THE LOAD INTRODUCTION ZONE IN THE REAR END OF AN AIRCRAFT

The invention relates to the structure of the load-introduction area in the fuselage rear section of an aircraft, including elements (3, 4) for receiving loads from the horizontal and vertical tailplanes connected to structural elements (2, 8, 9), in which: (a) the structural elements are the skin (...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	CRUZ DOMINGUEZ, FRANCISCO JOSE, ARIZA MARTIN, MANUEL, AREVALO RODRIGUEZ, ELENA
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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