公开(公告)号：USD810621S1

公开(公告)日：2018-02-20

申请号：US29561056

申请日：2016-04-12

申请人： KING SAUD UNIVERSITY

设计人： Shereef Aly Sadek

公开(公告)号：US09694906B1

公开(公告)日：2017-07-04

申请号：US15132107

申请日：2016-04-18

申请人： KING SAUD UNIVERSITY

发明人： Shereef Aly Sadek

IPC分类号： B64C29/00 ,  B64C39/08 ,  B64C39/02 ,  B64C25/10 ,  B64C5/06

CPC分类号： B64C29/00 ,  B64C5/06 ,  B64C25/10 ,  B64C29/0075 ,  B64C39/024 ,  B64C39/08 ,  B64C39/12 ,  B64C2201/021 ,  B64C2201/042 ,  B64C2201/048 ,  B64C2201/088 ,  B64C2201/104 ,  B64C2201/162 ,  B64C2201/187

摘要： The vertical takeoff and landing unmanned aerial vehicle includes a pair of selectively rotatable ducted fans and a selectively rotatable thrust vectoring nozzle providing vertical takeoff and landing for an unmanned aerial vehicle or a similar type of aircraft. A pair of fixed forward-swept wings are mounted on a rear portion of a fuselage, and a pair of canards are mounted on a top end of a forward portion of the fuselage. The pair of ducted fans are respectively mounted on free ends of the pair of canards, and are selectively rotatable about an axis parallel to a pitch axis of the fuselage. An engine is mounted in the rear portion of the fuselage, and a thrust vectoring nozzle is mounted on the rear portion of the fuselage for directing thrust exhaust from the engine. The thrust vectoring nozzle is selectively rotatable about an axis parallel to the pitch axis.