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公开(公告)号:WO2019150128A1
公开(公告)日:2019-08-08
申请号:PCT/GB2019/050282
申请日:2019-02-01
Applicant: MOHSENI, Seyed Mohammad , SAMAD AEROSPACE LIMITED
Inventor: MOHSENI, Seyed Mohammad
CPC classification number: B64C29/0008 , B64C29/0016 , B64C29/0025 , B64C29/0033 , B64C39/10
Abstract: A VTOL aircraft is having four electric fans (3a, 3b, 4a, 4b) distributed around the centre of gravity of the aircraft. Of the four electric fans, two (3a, 3b) are set into openings through the body (1)and two (4a, 4b) are rotatable about an axis to provide either horizontal thrust or vertical thrust. Optionally a multi-mode hybrid turbine engine (5) may be provided at the rear of the aircraft.