Title:
FIXED-WING AIRCRAFT HAVING VERTICAL TAKE-OFF AND LANDING ELECTRIC ROTORS AND DRIVEN BY FUEL POWER TO FLY FORWARDS
Document Type and Number:
WIPO Patent Application WO/2024/066918
Kind Code:
A1
Abstract:
A fixed-wing aircraft having vertical take-off and landing electric rotors and driven by a fuel power to fly forwards, comprising vertical take-off and landing electric rotor mechanisms (6) embedded in a fixed wing (2) or/and in an empennage horizontal stabilizer (13). Each vertical take-off and landing electric rotor mechanism comprises a duct body (61), a motor (62), a rotor (63, 64), a motor fixing frame (66) and a duct shielding cover mechanism (81). The duct body is fixedly embedded in the fixed wing or/and the empennage horizontal stabilizer, and vertically passes through an upper plane and a lower plane of the fixed wing or/and the empennage horizontal stabilizer. There is a motor or there are two motors having respective motor output shafts in the same axis, wherein one of the two motor output shafts faces upwards and the other faces downwards. The motor is fixedly disposed on the duct inner wall of the duct body by means of the motor fixing frame. The rotor is fixedly disposed on the motor output shaft, and the rotor and the motor are both retracted in an upper exit plane (22) and a lower exit plane (23) of the duct body.
Inventors:
WANG YONG (CN)
Application Number:
PCT/CN2023/116487
Publication Date:
April 04, 2024
Filing Date:
September 01, 2023
Export Citation:
Assignee:
JIANGSU YOUCHENG CNC TECH CO LTD (CN)
International Classes:
B64C27/26
Attorney, Agent or Firm:
CHANGZHOU XICHUANG PATENT AGENCY (GENERAL PARTNERSHIP) (CN)
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