estrutura da zona de introdução de carga na extremidade traseira de uma aeronave

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:	ELENA ARÉVALO RODRÍGUEZ, FRANCISCO JOSÉ CRUZ DOMÍNGUEZ, MANUEL ARIZA MARTÍN
Format:	Patent
Sprache:	por
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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