AIRCRAFT LONGITUDINAL CONTROL SURFACE, LONGITUDINAL CONTROL AUGMENTATION SYSTEM FOR AIRCRAFT, AND AIRCRAFT

A longitudinal control augmentation surface of aircraft, particularly turboprop/propfan aircraft with engines mounted on the rear portion of the fuselage. This longitudinal control augmentation surface is positioned in the connecting structure of the engine with the fuselage. A longitudinal control...

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Bibliographische Detailangaben
Hauptverfasser:	PEREIRA, João Marcelo Souza, SCALABRIN, Leonardo Costa, DE CARVALHO, Bruno Javiel, DA SILVA, Thiago Felske
Format:	Patent
Sprache:	eng
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:	A longitudinal control augmentation surface of aircraft, particularly turboprop/propfan aircraft with engines mounted on the rear portion of the fuselage. This longitudinal control augmentation surface is positioned in the connecting structure of the engine with the fuselage. A longitudinal control augmentation system for aircraft with engines arranged in a rear portion of the fuselage close to a vertical tail, this system comprising means of controlling the longitudinal control augmentation surfaces of the aircraft to distribute a longitudinal offset of the aircraft between these surfaces by means of functions, and an aircraft comprising the longitudinal control augmentation surface and the longitudinal control augmentation system.