Aircraft with split type lifting ailerons and single ducted rotors

The invention provides an aircraft with split type lifting ailerons and single ducted rotors. The aircraft comprises an aircraft body (10), undercarriages (20), a left wing (30), a right wing (40) anda ducted power device (50), wherein the left wing (30) and the right wing (40) are arranged on the l...

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Bibliographic Details
Main Authors ZHOU JIANBO, CHEN PENGYU, GONG JINGSHU, DU CHANGBING, LI ZHUOCHEN
Format Patent
LanguageChinese
English
Published 12.05.2020
Subjects
AEROPLANES
AIRCRAFT
AVIATION
COSMONAUTICS
HELICOPTERS
PERFORMING OPERATIONS
TRANSPORTING
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Summary:The invention provides an aircraft with split type lifting ailerons and single ducted rotors. The aircraft comprises an aircraft body (10), undercarriages (20), a left wing (30), a right wing (40) anda 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 aircraft body (10), the left wing (30) and the right wing (40); the left wing (30) and the right wing (40) are symmetrically arranged relative to the aircraft body (10); and the duct power device (50) is connected with the undercarriage (20) arranged on the aircraft body (10). Compared withother vertical take-off and landing fixed-wing aircrafts, the aircraft adopts the split type lifting ailerons and the ducts, and has the advantages of simple structure, long voyage, large thrust, highaerodynamic efficiency, hi
Bibliography:Application Number: CN202010063956