Rhombic composite wing aircraft

The utility model relates to a rhombic composite wing aircraft which comprises a fuselage, and the fuselage is sequentially provided with a front wing, a thrust duct, a rear wing and an empennage from the front part to the rear part; the two thrust ducts are symmetrically arranged on the two sides o...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: BING FUQIANG, XU XING
Format: Patent
Sprache:chi ; eng
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Beschreibung
Zusammenfassung:The utility model relates to a rhombic composite wing aircraft which comprises a fuselage, and the fuselage is sequentially provided with a front wing, a thrust duct, a rear wing and an empennage from the front part to the rear part; the two thrust ducts are symmetrically arranged on the two sides of the fuselage; wingtips at the left end and the right end of the front wing are connected with wingtips at the left end and the right end of the rear wing through connecting wings, and a plurality of lift fans capable of providing lift force in the vertical direction are arranged on the front wing and the rear wing respectively; the front wing, the rear wing and the two connecting wings jointly form a rhombic composite wing; the duct tilting device is connected with a thrust duct, and the thrust duct can do tilting motion relative to the fuselage so as to be switched between a vertical take-off and landing mode and a level flight cruising mode. According to the scheme, the vertical take-off and landing performance