Aircraft with a trimmable horizontal stabilizer having the pivot elements in its forward side

The invention provides an aircraft with a trimmable horizontal stabilizer (13) that not requires a cut-out in resistant areas of the rear fuselage and that occupies less space that in conventional horizontal stabilizers. The rear fuselage (5) comprises at least a first section (9) having a resistant...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	Martínez Muñoz José Luis, Luque Buzo Miguel, Llamas Sandín Raúl
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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