The present invention discloses an aircraft using a distributed electric ducted fan flap lift-rising system. The aircraft symmetrically arranges two distributed electric ducted fan flap lift-rising systems on both sides of the front middle part of the fuselage; the distributed electric ducted fan wing flap lift system has relatively large wingspan and aspect ratio; the number of electric ducted fans arranged on the leading edge is relatively large; the rear middle part of the fuselage is provided with a lift fan; rear wings are symmetrically disposed both sides of the rear middle part of the fuselage; the center of gravity of the aircraft is located in the middle of the fuselage; and the aircraft has a tandem wing layout. The aircraft of the present invention has the advantages of small friction, and no pollution and low noise of the electric ducted fan.
Aircraft using distributed electric ducted fan flap lift-rising system
2015-10-14
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Distributed type electric ducted fan flap lifting system and hovercar thereof
European Patent Office | 2015
|AIRCRAFT WING HAVING INTEGRATED DISTRIBUTED DUCTED FAN, AND ELECTRIC AIRCRAFT
European Patent Office | 2024
|Lift flap bearing apparatus, lift flap assembly, airfoil and aircraft
European Patent Office | 2016
|