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Cargo hold mooring structure

A tethering and cargo compartment technology, applied to equipment for loading and unloading cargo, aircraft parts, transportation and packaging, etc., can solve the problems of lack of airtightness, versatility, and poor interchangeability, and achieve versatility and ease of use Production and assembly, the effect of simple structure

Inactive Publication Date: 2019-05-24
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] The mooring structure is mainly combined with the mooring net or arresting net to ensure the fixation of the goods in the cargo compartment, so as to ensure that the goods will not collide with the main structure of the aircraft due to the vibration of the aircraft, but it does not have airtight characteristics, and its versatility and interchangeability are poor

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 mooring structure of the cargo compartment of the present ...

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Abstract

The invention provides a cargo hold mooring structure. The cargo hold mooring structure comprising a quick release joint (1), a mooring base (3), an airtight bowl (4), an airtight gasket (5), and a body connector (7); the airtight bowl (4) is composed of the outer edge of a ring and a basin-type cavity connected with the inner diameter of the outer edge of the ring; the mooring base (3) with the quick release joint (1) embedded therein is arranged on the concave side of the basin-type cavity; the body connector (7) for connecting the body is disposed on the convex side of the basin-type cavity; the mooring base (3), the basin-type cavity and the body connector (7) are fixedly mounted through multiple sets of bolt assemblies; the round airtight gasket (5) is bonded on the outer edge of thering and near the convex side of the basin-type cavity. The cargo hold mooring structure has the advantages of not only guaranteeing the airtightness of the cargo hold and facilitating the connectionof a mooring net or arresting net but also being simple in structure, light in weight and easy to disassemble.

Description

technical field [0001] The invention belongs to the field of aircraft structure design, and in particular relates to a mooring structure of a cargo hold. Background technique [0002] The mooring structure is mainly used together with the mooring net or arresting net to ensure the fixation of the cargo in the cargo compartment, so as to ensure that the cargo will not collide with the main structure of the aircraft due to the vibration of the aircraft, but it does not have airtight characteristics, and its versatility and interchangeability are poor. Contents of the invention [0003] The object of the present invention is to provide a mooring structure for a cargo hold, which overcomes or alleviates at least one of the above-mentioned drawbacks of the prior art. [0004] The purpose of the present invention is achieved through the following technical solutions: a mooring structure for a cargo hold, including a quick-release joint, a mooring base, an airtight bowl, an airti...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): B64D9/00
Inventor 李国彬伍小亮孙虎彬马志强
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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