Aircraft with split type lifting ailerons and double ducted rotors

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

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Bibliographic Details
Main Authors ZHOU JIANBO, XIONG CHUN, WEN TAO, TANG QIDONG, DU CHANGBING
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 double ducted rotors. The aircraft comprises an aircraft body (10), undercarriages (20), a left wing (30) and a right wing (40),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; the undercarriages (20) are respectively arranged on the aircraft body (10), the left wing (30) and the right wing (40); and a left duct power device (50) and a right duct power device (55) are respectively arranged at the extending ends of the left wing (30)and the right wing (40). Compared with other vertical take-off and landing fixed-wing aircrafts, the structure is simple; the split lifting ailerons and the ducts are adopted, the rotors are arrangedin the ducts, and compared with isolated rotors, the ducts improve the streaming characteristics of the propeller tip areas of the rotors, reduce the loss of the propeller tips, and the aircraft withthe split type lifting aile
Bibliography:Application Number: CN202010063957