Tilting ducted fixed-wing aircraft

The invention provides a tilting ducted fixed-wing aircraft which comprises a fuselage, main wings, canards, ducted fan engines and undercarriages, the fuselage comprises a cockpit located on the front portion of the fuselage and a mission load cabin located on the rear portion of the fuselage, the...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	QIAN XIANYUN, XING RONG, SUN YAN
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION COSMONAUTICS HELICOPTERS PERFORMING OPERATIONS TRANSPORTING
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