A REINFORCED LEADING EDGE SECTION FOR AN AIRCRAFT

The invention refers to a reinforced leading edge section (1) for an aircraft, comprising:- an outer skin (2) formed with an aerodynamic leading edge profile,- an inner reinforcement (3) arranged internally with respect to the outer skin (2) along the span of the leading edge section (1), wherein sa...

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Bibliographische Detailangaben
Hauptverfasser:	VIVARACHO RODRIGUEZ, Rubén, RAMIREZ BLANCO, Gonzalo
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AEROPLANES AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS HELICOPTERS PARACHUTES PERFORMING OPERATIONS TRANSPORTING
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Beschreibung
Zusammenfassung:	The invention refers to a reinforced leading edge section (1) for an aircraft, comprising:- an outer skin (2) formed with an aerodynamic leading edge profile,- an inner reinforcement (3) arranged internally with respect to the outer skin (2) along the span of the leading edge section (1), wherein said inner reinforcement (3) comprises a base (3') with a C-shaped configuration joined to the outermost part of the outer skin (2), and a web (3") having a free end (3"a) and an opposite end (3"b) joined to the base (3'), the web (3") extended in a direction transverse to the direction of the span of the leading edge section (1).