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Title:
AIRCRAFT REALIZING VERTICAL TAKE-OFF AND LANDING, AND CONTROL METHOD FOR AIRCRAFT REALIZING VERTICAL TAKE-OFF AND LANDING
Document Type and Number:
WIPO Patent Application WO/2023/197568
Kind Code:
A1
Abstract:
An aircraft realizing vertical take-off and landing, and a control method for the aircraft realizing vertical take-off and landing. The aircraft realizing vertical take-off and landing comprises: a fuselage (10), a tail thrust rotor wing (60), a fixed tail wing (30), two first power assemblies (40), and two second power assemblies (50). Two sides of the fuselage are provided with wings; the two first power assemblies are symmetrically mounted on the wings on the two sides of the fuselage; each first power assembly comprises a tilt rotor wing (42) and a first fixed rotor wing (43), wherein the tilt rotor wing is mounted on the wing through a rotor wing tilting mechanism; the two second power assemblies are symmetrically mounted on the wings on the two sides of the fuselage and are respectively positioned on outer sides of the first power assemblies; the tail thrust rotor wing is mounted at a tail of the fuselage; and the fixed tail wing is connected to the first power assemblies on the two sides of the fuselage. The aircraft realizing vertical take-off and landing and the control method can improve the layout mode of an EVTOL manned aircraft in the prior art, and improve the loading capacity and endurance capacity of the aircraft realizing vertical take-off and landing.

Inventors:
XUE SONGBAI (CN)
XIE SHAIMING (CN)
WANG CHANGYUN (CN)
SHA YONGXIANG (CN)
LUO JUNCHANG (CN)
Application Number:
PCT/CN2022/128571
Publication Date:
October 19, 2023
Filing Date:
October 31, 2022
Export Citation:
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Assignee:
CHENDU AEROVAN TECH CO LTD (CN)
GEELY HOLDING GROUP CO LTD (CN)
International Classes:
B64C27/52
Foreign References:
CN112937849A2021-06-11
CN214190098U2021-09-14
CN108382579A2018-08-10
CN106143898A2016-11-23
CN114771826A2022-07-22
CN216994844U2022-07-19
US20210362849A12021-11-25
Attorney, Agent or Firm:
J.Z.M.C. PATENT AND TRADEMARK LAW OFFICE (GENERAL PARTNERSHIP) (CN)
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