Butt joint test device and test method for wing root lower wall plate of aircraft wing with dihedral angle

A test device and wallboard technology, applied in the direction of measuring device, using stable tension/pressure test material strength, instruments, etc., can solve the problems of insufficient consideration of influence, inaccurate verification of actual force transmission path, etc., to reduce loading Capability requirements, simple structure, and the effect of avoiding damage

Pending Publication Date: 2021-11-26
BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC +1
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AI Technical Summary

Problems solved by technology

For the type selection and test verification of the butt joint structure of the lower wall plate in the wing root connection area, the common method is to simulate and replace the actual butt joint configuration with a straight butt joint structure, but the influence of the dihedral angle at the wing root of the civil aircraft structure is not considered. Sufficient, the verification of the actual force transmission path is not accurate enough

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  • Butt joint test device and test method for wing root lower wall plate of aircraft wing with dihedral angle
  • Butt joint test device and test method for wing root lower wall plate of aircraft wing with dihedral angle
  • Butt joint test device and test method for wing root lower wall plate of aircraft wing with dihedral angle

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Embodiment Construction

[0061]Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, the same numerals in different drawings refer to the same or similar elements unless otherwise indicated. The implementations described in the following exemplary examples do not represent all implementations consistent with the present invention. Rather, they are merely examples of apparatuses and methods consistent with aspects of the invention as recited in the appended claims.

[0062] The terms "first", "second" and the like in the description and claims of the present invention are used to distinguish similar objects, and are not necessarily used to describe a specific order or sequence. It is to be understood that the data so used are interchangeable under appropriate circumstances such that the embodiments of the invention described herein, for example, can be practi...

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Abstract

The invention discloses a butt joint test device and test method for a wing root lower wall plate of an aircraft wing with a dihedral angle, and relates to the technical field of aircraft lower wall plate butt joint test, and the device comprises: a test piece which comprises an outer wing side wall plate and a central wing side wall plate which are transversely arranged, wherein the outer wing side wall plate and the central wing side wall plate are fixedly connected through a connector; a fixing unit which is connected with the central wing side wall plate and is used for fixing the test piece; a support unit which is connected with the connector and is used for providing support for the test piece; and a lever unit which is connected with the outer wing side wall plate and is used for transmitting and amplifying an external load. According to the invention, the actual force transmission path of the lower wall plate of the wing root connection area can be simulated more accurately, and the analysis method of the wing root connection area can be verified more fully.

Description

technical field [0001] The invention relates to the technical field of butt joint test of the lower wall plate of an aircraft, in particular to a test device and a test method for the butt joint test of the lower wall plate of the wing root of an aircraft wing with dihedral. Background technique [0002] For the structure of modern civil aircraft, the connection relationship of the wing root connection area where the central wing box and the outer wing box are docked is complicated, and the shear force and bending moment load are high. The butt joint structure of the lower wall plate affects the overall scheme of the wing root connection area. Under the action of flight load, it is subjected to tensile load, and tests need to be carried out to verify its structural bearing capacity, assembly characteristics and related analysis methods. For the type selection and test verification of the butt joint structure of the lower wall plate in the wing root connection area, the commo...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): G01N3/08
CPCG01N3/08G01N2203/0003G01N2203/0017G01N2203/0075G01N2203/0676G01N2203/0682
Inventor 马志阳贺体人汤平汤剑飞陈普会徐吉峰
Owner BEIJING AERONAUTIC SCI & TECH RES INST OF COMAC
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