Title:
WING PANEL STRUCTURE FOR AIRCRAFT, WING STRUCTURE, AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2022/104775
Kind Code:
A1
Abstract:
Provided are a wing panel structure for an aircraft, a wing structure, and an aircraft. The wing panel structure comprises a plurality of wing panel units, and adjacent wing panel units are connected by means of an airfoil control unit (500, 600) and a wing panel periphery connecting member (3, 6, 10, 13). Each wing panel unit comprises a plurality of wing panel edge members (2, 4, 5, 7, 9, 11, 12, 14) and wing linkage connecting members (110, 210, 310) connected to each other. The wing linkage connecting member in each wing panel unit is correspondingly connected to a wing supporting rod (100, 200, 300) on an aircraft body. This wing panel structure has wide-range airfoil variable features in terms of chord length and curvature; the movement of the wing panel structure is driven by the movement of the wing supporting rod; the wing panel structure has a variable airfoil, is variable in pitch angle within a large range, and can be adjusted for complex flow fields or environments, thus the movement speed and movement efficiency are greatly improved, and high maneuverability can be achieved.
Inventors:
LI WEI (CN)
LUO BING (CN)
CUI WEICHENG (CN)
LUO BING (CN)
CUI WEICHENG (CN)
Application Number:
PCT/CN2020/130817
Publication Date:
May 27, 2022
Filing Date:
November 23, 2020
Export Citation:
Assignee:
UNIV WESTLAKE (CN)
International Classes:
B64C3/38; B64C3/48
Foreign References:
| CN109515683A | 2019-03-26 | |||
| CN106827991A | 2017-06-13 | |||
| CN111746783A | 2020-10-09 | |||
| CN111746785A | 2020-10-09 | |||
| US5971328A | 1999-10-26 |
Attorney, Agent or Firm:
KINGSOUND & PARTNERS (CN)
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