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Decorative plate support assembly

A decorative panel and component technology, applied in aircraft parts, fuselage frame, transportation and packaging, etc., can solve the problems of complex path setting, unsuitable for assembling and disassembling decorative panels, etc., and achieves easy installation, simple mechanism design, fast installation and The effect of disassembly

Active Publication Date: 2021-06-18
COMAC +1
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0012]However, the routing of this device is too complicated to be suitable for installing and removing trim panels in aircraft cabins

Method used

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  • Decorative plate support assembly
  • Decorative plate support assembly
  • Decorative plate support assembly

Examples

Experimental program
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Embodiment Construction

[0075] Reference will now be made in detail to embodiments of the invention, examples of which are illustrated in the accompanying drawings and described hereinafter.

[0076] While the invention will be described in conjunction with exemplary embodiments, it will be understood that the description is not intended to limit the invention to those illustrated embodiments. On the contrary, the invention is intended to cover not only the exemplary embodiments, but also various alternatives, modifications, equivalents and other embodiments, which may be included within the spirit and scope of the invention.

[0077] For ease of explanation and precise definition of the technical solutions of the present invention, the terms "upper", "lower", "inner" and "outer" are used to describe the features of the exemplary embodiments with reference to their positions in the drawings. to describe.

[0078] figure 2 -4 shows a preferred embodiment of the trim panel bracket assembly 100 accor...

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PUM

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Abstract

The invention relates to a decorative plate support assembly which comprises a decorative plate connecting part used for being connected with a decorative plate, and the decorative plate connecting part comprises a maintaining part; a fixed support is used for being fixedly connected with a fixing structure; a limiting block is connected with the fixed support and can move relative to the fixed support, and the limiting block comprises an operating part used for operating the limiting block; the limiting support is connected with the fixed support and matched with the limiting block so that the limiting support can move between a mounting position and a dismounting position along with movement of the limiting block, in the mounting position, the decorative plate connecting part is held by the limiting support through the holding part, and in the dismounting position, the decorative plate connecting part can be dismounted from the limiting support, and the movement of the limiting block relative to the fixed support is realized by enabling the control part to generate displacement in a single direction. According to the invention, the decorative plate can be conveniently detached from one side, deviating from the support assembly, of the decorative plate.

Description

technical field [0001] The invention relates to the field of aircraft design, in particular to the structural design of aircraft interior decoration, and more particularly to a bracket assembly for decorative panels such as hoisting decorative panels. Background technique [0002] For the needs of beauty and safety, decorative panels are generally installed in the aircraft cabin. [0003] When the decorative panel is installed, it is generally necessary to hide the bracket of the decorative panel on the inner side of the decorative panel due to the consideration of factors such as the beauty of the interior of the engine room. However, the decorative panels need to be disassembled during maintenance, so some installation methods that can be easily disassembled are needed in the art to install the decorative panels. [0004] The prior art mainly uses quick-release locks for installation, and most lock installation methods need to pay attention to the installation and disasse...

Claims

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Application Information

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IPC IPC(8): B64C1/06E04F13/21E04F13/22
CPCB64C1/066E04F13/0803
Inventor 周琴刘曦明王泽汉何永军周飞鹂党亚斌
Owner COMAC
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