adaptação para equilíbrio longitudinal de um estabilizador horizontal de uma aeronave

Fitting (30) for trimming the horizontal stabilizer (1a) of an aircraft, made of composite material, said fitting (30) comprising side walls (2a and 2b) of a torsion box as well as joining elements (3a, 3b) which join the fitting (30) to the frames of the tail fuselage (1) of the aircraft, said side...

Ausführliche Beschreibung

Bibliographische Detailangaben

1. Verfasser:	ELENA ARÉVALO RODRÍGUEZ
Format:	Patent
Sprache:	por
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
Online-Zugang:	Volltext bestellen
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