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Lateral-directional single-hoop mounting structure for airplane gas cylinder

A technology of installation structure and horizontal direction, which is applied in the direction of mechanical equipment, gas/liquid distribution and storage, container discharge methods, etc., to facilitate disassembly and inspection and daily maintenance work, improve maintainability and safety, and maximize flexibility Effect

Inactive Publication Date: 2016-06-15
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 installation of traditional aircraft gas cylinders is to fix the gas cylinders by clamping the front end and the rear end of the gas cylinders with two clamps at the front and rear respectively. Although this installation method is simple, when installing and disassembling the gas cylinders, It needs to occupy the area of ​​the entire side of the gas cylinder to operate the front and rear clamps

Method used

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  • Lateral-directional single-hoop mounting structure for airplane gas cylinder
  • Lateral-directional single-hoop mounting structure for airplane gas cylinder
  • Lateral-directional single-hoop mounting structure for airplane gas cylinder

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Embodiment Construction

[0013] An aircraft gas cylinder horizontal direction single clamp installation structure, such as figure 1 , 2 , 3, it consists of a gas cylinder 1, a front bracket 2, a rear bracket 3, and a clamp 4. The neck of the gas cylinder 1 is firmly supported by the front bracket 2 and clamped by the clamp 4 to prevent its displacement. The bottom of 1 is limited by rear bracket 3 to prevent its axial and circumferential displacement. Front support 2 is made up of base 21, bowl holder 22, L support 23 and buffer pad 24, bowl holder 22 is connected with base 21 by screws, and the supporting surface of bowl holder 22 is a two-dimensional curved surface shape, which is completely consistent with the shape of cylinder 1 shoulder. Fitting to the maximum extent to ensure that the contact force with the cylinder surface is more uniform under overload conditions, and the cylinder is not worn while limiting; at the same time, there is a buffer pad 24 between the bowl holder 22 and the cylinde...

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PUM

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Abstract

The invention belongs to the design technology of aircraft mechanical systems, and relates to an installation structure of air cylinders on board an aircraft. The utility model relates to an aircraft gas cylinder horizontal direction single clamp installation structure, which is composed of a gas cylinder, a front support, a rear support and a clamp. The neck of the gas cylinder is firmly supported by the front bracket and clamped to prevent its displacement. The bottom of the gas cylinder is limited by the rear bracket with wrapping function to prevent its axial and circumferential displacement. After the gas cylinder is pushed into the rear bracket, the gas cylinder can be clamped on the front bracket with a clamp. When disassembling, it is only necessary to loosen the clamp on the front bracket, and the gas cylinder can be directly pulled out from the bracket.

Description

technical field [0001] The invention belongs to the aircraft mechanical system design technology, and relates to an installation design method of an aircraft air cylinder. Background technique [0002] The installation of traditional aircraft gas cylinders is to fix the gas cylinders by clamping the front end and the rear end of the gas cylinders with two clamps at the front and rear respectively. Although this installation method is simple, when installing and disassembling the gas cylinders, It needs to occupy the area of ​​the entire side of the gas cylinder to operate the front and rear clamps. Contents of the invention [0003] The object of the present invention is to provide a horizontal direction single clip mounting structure for an aircraft gas cylinder which is reliable in fixing and can greatly reduce the operating time and space for installing and dismounting the gas cylinder. [0004] Technical scheme of the present invention is: [0005] An aircraft gas cy...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F17C13/08
Inventor 王莉周慧红窦田天闫海兵张光明
Owner XIAN AIRCRAFT DESIGN INST OF AVIATION IND OF CHINA
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