Airplane cabin curtain assembly

A curtain and component technology, which is applied in the field of aircraft cabin curtain components, can solve the threat of aircraft structure and aircraft safety operation, affect the travel comfort of passengers, and cannot satisfy passengers, so as to facilitate rest, reduce the difficulty of construction, and be easy to adjust Effect

Inactive Publication Date: 2012-11-14
成都富凯飞机工程服务有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0002] In the existing aircraft structure, some aircraft cabins are not equipped with a curtain structure, which affects the comfort of passengers traveling. However, if the curtain structure is added to the existing aircraft structure, the existing structural layout of the aircraft must be modified. It is difficult, and the number of curtains that can be increased is limited, which cannot meet the needs of passengers, and the modification of the aircraft structure will also pose a threat to the safe operation of the aircraft

Method used

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  • Airplane cabin curtain assembly
  • Airplane cabin curtain assembly
  • Airplane cabin curtain assembly

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Embodiment Construction

[0016] The present invention will be further described below in conjunction with accompanying drawing, protection scope of the present invention is not limited to the following:

[0017] Such as figure 1 , figure 2 Shown, the aircraft cabin partition curtain assembly, it comprises partition curtain assembly and left and right partition curtain assembly, described partition curtain assembly comprises guide rail A1, guide rail B2 and partition curtain support 3, guide rail A1 and guide rail B2 symmetrical arrangement, guide rail A1 is set on the large luggage box 4 on one side of the cabin, guide rail B2 is set on the large luggage box 4 on the other side of the cabin, and the middle partition curtain bracket 3 includes bracket body A5, sliding sleeve A6, fixed support rod 7, and sliding support rod 8 , sliding sleeve B9 and locking device 10, support rod guide rail 11 is provided in support body A5, fixed support rod 7 and sliding support rod 8 are all arranged in the support...

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Abstract

The invention discloses an airplane cabin curtain assembly, which comprises a middle curtain assembly and a left and right curtain assembly, wherein the middle curtain assembly comprises a guide rail A (1), a guide rail B (2) and a middle curtain support (3), and the guide rail A (1) and the guide rail B (2) are arranged on a big luggage carrier (4) of the cabin; the middle curtain support (3) comprises a support body A (5), a sliding sleeve A (6), a fixed support rod (7), a sliding support rod (8), a sliding sleeve B (9) and a locking device (10); the sliding sleeve A (6) is movably sheathed on the guide rail A (1), and the sliding sleeve B (9) is movably sheathed on the guide rail B (2); and the left and right curtain assembly comprises a pre-installed base (13) and a left and right curtain support (14). The airplane cabin curtain assembly has the beneficial effects that the airplane cabin curtain assembly is conveniently installed on an airplane on the basis that the original structure of the airplane is not damaged, so that the influence on the airplane safety is reduced, and the construction difficulty is reduced; and the installation structure is simple and convenient and is easily regulated, and the installation structure is firmly and stably fixed.

Description

technical field [0001] The invention relates to an aircraft cabin partition curtain assembly. Background technique [0002] In the existing aircraft structure, some aircraft cabins are not equipped with a curtain structure, which affects the comfort of passengers traveling. However, if the curtain structure is added to the existing aircraft structure, the existing structural layout of the aircraft must be modified. It is difficult, and the number of curtains that can be increased is limited, which cannot meet the needs of passengers, and the modification of the aircraft structure will also pose a threat to the safe operation of the aircraft. Contents of the invention [0003] The purpose of the present invention is to overcome the disadvantages of the prior art and provide an aircraft cabin curtain assembly that provides passengers with multi-directional curtains without changing the existing structure of the aircraft. [0004] The object of the present invention is achie...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D11/00
Inventor 孟玮
Owner 成都富凯飞机工程服务有限公司
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