Aircraft with split type lifting ailerons and single ducted rotors

The utility model provides an aircraft with split type lifting ailerons and single ducted rotors. The aircraft comprises an aircraft body (10), an undercarriage (20), a left wing (30), a right wing (40) and a ducted power device (50), wherein the left wing (30) and the right wing (40) are arranged o...

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Bibliographic Details
Main Authors ZHOU JIANBO, CHEN PENGYU, GONG JINGSHU, DU CHANGBING, LI ZHUOCHEN
Format Patent
LanguageChinese
English
Published 20.11.2020
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The utility model provides an aircraft with split type lifting ailerons and single ducted rotors. The aircraft comprises an aircraft body (10), an undercarriage (20), a left wing (30), a right wing (40) and a ducted power device (50), wherein the left wing (30) and the right wing (40) are arranged on the left side and the right side of the aircraft body (10) respectively, and the ducted power device (50) is installed behind the aircraft body. More than two undercarriages (20) are respectively arranged on the fuselage (10), the left wing (30) and the right wing (40); the left wing (30) and theright wing (40) are symmetrically arranged relative to the fuselage (10); and the duct power device (50) is connected with an undercarriage (20) arranged on the fuselage (10). Compared with other vertical take-off and landing fixed-wing aircrafts, the vertical take-off and landing fixed-wing aircraft has the advantages of being simple in structure, long in voyage, large in thrust, high in aerodynamic efficiency, high in s
Bibliography:Application Number: CN202020124264U