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Connecting method and bracket for aircraft interior trimming panel

A connection bracket and connection method technology, which are applied to the connection method and connection bracket field of aircraft interior panels, can solve problems such as noise at the connection point, and achieve the effects of good maintainability, reduction of installation errors, and reduction of vibration and noise.

Inactive Publication Date: 2019-04-09
XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

Moreover, the current installation of domestic interior panels generally has less consideration in terms of shock absorption. During the flight, the shaking of the joints will generate noise.

Method used

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  • Connecting method and bracket for aircraft interior trimming panel
  • Connecting method and bracket for aircraft interior trimming panel
  • Connecting method and bracket for aircraft interior trimming panel

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Experimental program
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Effect test

Embodiment Construction

[0012] Referring to the accompanying drawings, the connecting method of the aircraft interior trim panel of the present application is used to fix the interior trim panel 2 on the aircraft body 1, and has a connecting bracket 3, which contains a mounting rail 5 and a mounting slider 4, Described installation track 5 is a groove structure, and the upper end of installation slide block 4 is installation plate 9, and the lower end of installation slide block 4 is inlaid in the groove structure of installation track 5, and installation slide block 4 can be relative to installation track 5 Sliding, one or more installation sliders can be set in the installation track 5; the installation track 5 of the connecting bracket 3 is fixed on the aircraft body 1, and one end of the interior trim panel 2 is fixed with the aircraft body by a connector, and the interior trim panel 2 The other end is connected with the installation plate 9 of this connection bracket installation slide block.

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PUM

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Abstract

The invention discloses a connecting method and bracket for an aircraft interior trimming panel. The connecting method and bracket are used for fixing the interior trimming panel to an airframe, the connecting bracket comprises a mounting track and a mounting sliding block, the mounting track is of a groove-shaped structure, a mounting plate is arranged at the upper end of the mounting sliding block, the lower end of the mounting sliding block is inlaid into the groove-shaped structure of the mounting track, the mounting sliding block can slide relative to the mounting track, and one or more mounting sliding blocks can be arranged in the mounting track; and the mounting track of the connecting bracket is fixed to the airframe, one end of the interior trimming panel is fixed to the airframethrough a connecting piece, and the other end of the interior trimming panel is connected with the mounting plate of the mounting sliding block of the connecting bracket.

Description

technical field [0001] The application belongs to the technical field of aircraft design, and in particular relates to a connection method and a connection bracket of an aircraft interior trim panel. Background technique [0002] At present, most domestic aircraft interior decorations use interior decoration brackets and oblong holes, and cooperate with spring clamp self-locking nuts and screws to fix the interior panels, so as to realize the adjustment of the interior panels during installation. In this way, the adjustment of a larger size cannot be realized. When the size of the interior panel is changed, the connection position of the bracket on the structure needs to be replaced again. Moreover, the current installation of domestic interior panels generally has less consideration in terms of shock absorption. During the flight, the shaking of the connection will generate noise. At the same time, the interior trim panels are required to be beautiful during installation, ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64C1/10
CPCB64C1/10
Inventor 王雯王磊
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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