Title:
AIRCRAFT, AIRCRAFT CONTROL METHOD AND DEVICE, AND COMPUTER-READABLE STORAGE MEDIUM
Document Type and Number:
WIPO Patent Application WO/2023/225819
Kind Code:
A1
Abstract:
Embodiments of the present application provide an aircraft. The aircraft is characterized by comprising: a fuselage; main wings, which are fixedly connected to the fuselage, the main wings being used to provide lift to the aircraft; canards, which are arranged at the positions of the fuselage close to a nose, and are used to provide lift to the aircraft; and a multi-rotor assembly, which comprises first rotor assemblies and second rotor assemblies, wherein the first rotor assemblies are mechanically coupled to the main wings, the second rotor assemblies are rotatably connected to the canards, and the second rotor assemblies are configured to be capable of adjusting the tilting angles of the second rotor assemblies relative to the canards and providing lift and/or forward tension to the aircraft.
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Inventors:
ZHOU WEIXIANG (CN)
Application Number:
PCT/CN2022/094545
Publication Date:
November 30, 2023
Filing Date:
May 23, 2022
Export Citation:
Assignee:
SZ SHANZHI TECH CO LTD (CN)
International Classes:
B64C27/26; B64C27/28
Foreign References:
| CN113525678A | 2021-10-22 | |||
| CN111169631A | 2020-05-19 | |||
| CN212243812U | 2020-12-29 | |||
| CN106184737A | 2016-12-07 | |||
| CN208325621U | 2019-01-04 | |||
| CN113788142A | 2021-12-14 | |||
| CN214824040U | 2021-11-23 | |||
| US20110303795A1 | 2011-12-15 | |||
| US20220089279A1 | 2022-03-24 | |||
| CN107499505A | 2017-12-22 |
Attorney, Agent or Firm:
BEIJING BESTIPR INTELLECTUAL PROPERTY LAW CORPORATION (CN)
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