Structure for the fuselage rear end

Load introduction zone in the rear end of an aircraft comprising receiving elements (3, 4) of the loads of the horizontal and vertical tail stabilizers connected to structural elements (2, 8, 9) wherein: a) said structural elements are the cladding (8), two contiguous load-bearing frames (2) with a...

Ausführliche Beschreibung

Bibliographische Detailangaben

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