Title:
WING-DISMOUNTING ASSEMBLY AND AIRCRAFT
Document Type and Number:
WIPO Patent Application WO/2021/043335
Kind Code:
A3
Abstract:
Provided are a wing-dismounting assembly (1) and an aircraft having said wing-dismounting assembly (1). The wing-dismounting assembly (1) comprises a first connecting portion (10) and a second connecting portion (20); the first connecting portion (10) comprises a fixing seat (12), a press-fit component (13) and a buckling component (14); one of the fixing seat (12) and the second connecting portion (20) is fixed on a wing, and the other of the fixing seat (12) and the second connecting portion (20) is fixed on a fuselage; an installation groove (211) is formed in the second connecting portion (20), and a notch of the installation groove (211) is away from the first connecting portion (10); and the press-fit component (13) is rotationally connected to the fixing seat (12), the buckling component (14) is rotationally connected to the press-fit component (13), one end of the buckling component (14) is buckled in the installation groove (211), and the press-fit component (13) when press-fitted is used for driving the buckling component (14) to integrally move away from the notch of the installation groove (211), so as to buckle the buckling component (14) in the installation groove (211). The wing-dismounting assembly and the aircraft have the advantage of facilitating wing dismounting.
Inventors:
DU YUANYUAN (CN)
Application Number:
PCT/CN2020/123359
Publication Date:
April 22, 2021
Filing Date:
October 23, 2020
Export Citation:
Assignee:
AUTEL ROBOTICS CO LTD (CN)
International Classes:
B64C1/26; B64C3/00
Foreign References:
| CN211196589U | 2020-08-07 | |||
| CN207482173U | 2018-06-12 | |||
| CN206984303U | 2018-02-09 | |||
| CN109436292A | 2019-03-08 | |||
| CN206125394U | 2017-04-26 | |||
| CN206437190U | 2017-08-25 | |||
| US20030006340A1 | 2003-01-09 |
Attorney, Agent or Firm:
AFD CHINA INTELLECTUAL PROPERTY LAW OFFICE (CN)
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