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Oxygen cylinder compartment

A technology for oxygen cylinders and compartments, which is applied in the field of oxygen cylinder compartments, and can solve the problems of shaking oxygen cylinders, bulky protective devices and occupying space.

Inactive Publication Date: 2019-02-26
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

[0002] In the aircraft cabin, some life-saving facilities, especially oxygen cylinders, need to be placed. Necessary protective measures must be taken for the placed oxygen cylinders. The existing protective devices are heavy and occupy a large space. At the same time, the placed oxygen cylinders are shaken during the flight process. potential risks

Method used

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Embodiment Construction

[0015] In order to make the objectives, technical solutions and advantages of the present invention clearer, the technical solutions in the embodiments of the present invention will be described in more detail below in conjunction with the drawings in the embodiments of the present invention. In the drawings, the same or similar reference numerals denote the same or similar elements or elements having the same or similar functions throughout. The described embodiments are some, but not all, embodiments of the invention. The embodiments described below by referring to the figures are exemplary and are intended to explain the present invention and should not be construed as limiting the present invention. Based on the embodiments of the present invention, all other embodiments obtained by persons of ordinary skill in the art without creative efforts fall within the protection scope of the present invention.

[0016] The oxygen cylinder compartment of the present invention will ...

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Abstract

The invention provides an oxygen cylinder compartment which is formed by five rectangular thin plates by splicing. The long sides of the wall panels B, C are equal to the long sides of the wall panelA (1), and the short sides of the two panels are shorter than the short sides of the panel A (1); the long sides of the panels D, E are equal and shorter than the short sides of the panel A (2); the two long sides of the panel A (1) are respectively aligned at an angle to one of the long sides of the panel B and the panel C, and the two panels are located on the same side of the panel A (1); a short side of the wall panel A (1) is spliced at an angle with a long side of the wall panel D (4), wherein the wall panel D (4) is located on the same side of the wall panels B and C; the other long side of the wall panel D (4) is aligned with the long side of the wall panel E (5) at an angle such that the panel E (5) and the panel A (1) are arranged at a 90 DEG angle; a plurality of reinforcing grooves are arranged on the wall panel A (1). The oxygen cylinder compartment provided by the invention ensures that the strength of the oxygen cylinder compartment is qualified, and the rivet connectionfacilitates the splicing of the wall panel.

Description

technical field [0001] The invention belongs to the field of aircraft structure design, and in particular relates to an oxygen cylinder compartment. Background technique [0002] In the aircraft cabin, some life-saving facilities, especially oxygen cylinders, need to be placed. Necessary protective measures must be taken for the placed oxygen cylinders. The existing protective devices are heavy and occupy a large space. At the same time, the placed oxygen cylinders are shaken during the flight process. potential risks. Contents of the invention [0003] The object of the present invention is to provide an oxygen cylinder compartment which overcomes or alleviates at least one of the above-mentioned defects of the prior art. [0004] The object of the present invention is achieved through the following technical solutions: an oxygen cylinder compartment, which is composed of wall panels A, wall panels B, wall panels C, wall panels D and wall panels E, and the five wall pane...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D13/00
CPCB64D13/00
Inventor 刘蓬田旭竞范林
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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