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Title:
FLEXIBLE CONNECTING STRUCTURE FOR ARRESTING WALL AND FUSELAGE, AND AIRPLANE
Document Type and Number:
WIPO Patent Application WO/2023/202055
Kind Code:
A1
Abstract:
A flexible connecting structure (100) for an arresting wall and a fuselage. The flexible connecting structure is configured to fix an arresting wall (200) to the interior of an aircraft (300), and comprises: a first connecting joint (10), the first connecting joint (10) being pivotally connected to a second connecting joint (201) arranged on the arresting wall; a flexible transition member (20), a first end (21) of the flexible transition member being fixed to a free end (11) of the first connecting joint; and an interframe short beam (30), which is fixed to an adjacent frame (301) and stringer (302) on an aircraft panel and fixed to a second end (22) of the flexible transition member. The structure can bear, by means of the flexible transition member, a course load transmitted via the arresting wall to the fuselage of the aircraft, thereby effectively avoiding excessive constraint of a rigid arresting wall on deformation of structures such as local skin of the fuselage under a working condition of pressurization, and eliminating the influence on the fatigue performance of the structure of the fuselage.

Inventors:
ZHAO XIAORAN (CN)
XIONG XUJUN (CN)
SHENG XUDONG (CN)
ZHAO JUNFENG (CN)
LIU ZUI (CN)
Application Number:
PCT/CN2022/132159
Publication Date:
October 26, 2023
Filing Date:
November 16, 2022
Export Citation:
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Assignee:
COMMERCIAL AIRCRAFT CORP CN (CN)
COMMERCIAL AIRCRAFT CORPORATION OF CHINA LTD SHANGHAI AIRCRAFT DESIGN AND RES INSTITUTE (CN)
International Classes:
B64C1/10
Foreign References:
CN114735193A2022-07-12
CN113734415A2021-12-03
US5915652A1999-06-29
CN109319087A2019-02-12
US4780034A1988-10-25
US20100178129A12010-07-15
US5085382A1992-02-04
US20180346121A12018-12-06
CN106672197A2017-05-17
Attorney, Agent or Firm:
SHANGHAI PATENT & TRADEMARK LAW OFFICE, LLC (CN)
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