Cabin section and machining method thereof

A processing method and cabin technology, applied in the cabin and its processing field, can solve the problems of high cost and complicated welding process operation

Inactive Publication Date: 2018-03-13
XIAN FANGYUANMING TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, the welding process included in this processing technology is complicated to operate and the cost is too high; the proc

Method used

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  • Cabin section and machining method thereof
  • Cabin section and machining method thereof
  • Cabin section and machining method thereof

Examples

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Effect test

Embodiment 1

[0024] Embodiments of the present invention provide a cabin processing method, refer to figure 1 As shown, the method includes:

[0025] S101. Extrude or forge the round ingot to be processed to form a blank tube, and the material of the round ingot to be processed is a lightweight structural material.

[0026] The specific method for forming the round ingot to be processed is not limited here, and it can be made by die casting or continuous casting. In order to ensure the quality of the round ingot to be processed, the latter is preferred. That is, the round ingot to be processed is preferably a continuous casting round ingot. In addition, there is no limitation on the diameter of the round ingot to be processed, which can be selected according to actual needs.

[0027] Here, there is no limitation on the specific type of lightweight structural material, which may be aluminum alloy, magnesium alloy, titanium alloy or metal matrix composite material.

[0028] S102. Perform ...

Embodiment 2

[0049]An embodiment of the present invention provides a cabin section, and the cabin section is manufactured by any one of the processing methods provided in the first embodiment. This cabin section can be applied to spaceships and missiles, and is an important component. The compartment is characterized by low cost and high quality. At the same time, the cabin section is made of lightweight structural materials, which also has the characteristics of light weight.

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Abstract

The invention provides a cabin section and a processing method thereof, which relate to the technical field of mechanical processing. The cabin section manufactured by the processing method has the characteristics of low cost and high quality. A processing method for a cabin section, the method comprising: extruding or forging a round ingot to be processed to form a rough tube, the material of the round ingot to be processed is a lightweight structural material; performing at least one pretreatment on the rough tube Treatment; the pretreatment includes: first heat treatment, drawing and second heat treatment; machining the blank tube after at least one pretreatment to form a cabin section. The invention is applicable to the manufacture of cabin sections.

Description

technical field [0001] The invention relates to the technical field of mechanical processing, in particular to a cabin section and a processing method thereof. Background technique [0002] As an important part of spaceships and missiles, cabins are widely used in the military field. In the traditional technology, the cabin section is manufactured using the processing technology of "plate curling→welding→machining". However, the welding process included in this processing technology is complicated to operate and the cost is too high; the processing technology of the traditional cabin can no longer meet the requirements of current military equipment for low cost. How to reduce the production cost of the cabin under the premise of ensuring the quality of the cabin has become an urgent problem to be solved. Contents of the invention [0003] Embodiments of the present invention provide a cabin section and a processing method thereof, and the cabin section manufactured by th...

Claims

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Application Information

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IPC IPC(8): B23P15/00B64G1/22C21D9/08C22F1/00
CPCB23P15/00B23P2700/01B64G1/22C21D9/08C22F1/00
Inventor 刘瑶宋方
Owner XIAN FANGYUANMING TECH CO LTD
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