Aircraft with double-fuselage tandem wing vertical take-off and landing layout

The patent of the invention discloses an aircraft with a double-fuselage tandem wing vertical take-off and landing layout, and particularly relates to the technical field of aviation aircrafts. The aircraft with a double-fuselage tandem wing vertical take-off and landing layout comprises two fuselag...

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Hauptverfasser: YANG XIAOCHUAN, WANG HAIJUN, JIANG JIULONG, MAO ZHONGJUN, HE KAIFENG, FU ZHI, XIAO HANSHAN, HE JUHENG
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creator YANG XIAOCHUAN
WANG HAIJUN
JIANG JIULONG
MAO ZHONGJUN
HE KAIFENG
FU ZHI
XIAO HANSHAN
HE JUHENG
description The patent of the invention discloses an aircraft with a double-fuselage tandem wing vertical take-off and landing layout, and particularly relates to the technical field of aviation aircrafts. The aircraft with a double-fuselage tandem wing vertical take-off and landing layout comprises two fuselages which are arranged at an interval, and an engine is arranged on each fuselage; a front tandem type wing and a rear tandem type wing which are distributed at an interval are arranged on the two fuselages; an electric tilting rotor wing arranged at one end of the front tandem type wing is also symmetrically arranged on each fuselage; a generator is connected between each electric tilting rotor wing and each engine, the generators are electrically connected with the engines, the rear tandem typewing is provided with a first lift fan located between the two fuselages and a sliding flow rudder located below the first lift fan, and each fuselage is provided with a vertical fin located at one end of the rear tandem typ
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language chi ; eng
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subjects AEROPLANES
AIRCRAFT
ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT
AVIATION
COSMONAUTICS
EQUIPMENT FOR FITTING IN OR TO AIRCRAFT
FLYING SUITS
HELICOPTERS
PARACHUTES
PERFORMING OPERATIONS
TRANSPORTING
title Aircraft with double-fuselage tandem wing vertical take-off and landing layout
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