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A kind of equipment for manufacturing cast magnesium structural parts of large spacecraft

A technology for spacecraft and structural parts, applied in casting and forming equipment, manufacturing tools, metal processing equipment, etc., can solve the problems of difficult production and large area, and achieve the effect of simple sand box and small area.

Active Publication Date: 2017-09-29
SHANXI SHENZHOU AEROSPACE SCI & TECH CO LTD
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0006] The technical problem to be solved by the present invention is that in the prior art, the manufacture of cast magnesium structural parts of spacecraft needs to be made with upper and lower sand box structures, which occupies a large area and is difficult to produce. Simple, easy-to-operate combined sand box system

Method used

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  • A kind of equipment for manufacturing cast magnesium structural parts of large spacecraft
  • A kind of equipment for manufacturing cast magnesium structural parts of large spacecraft
  • A kind of equipment for manufacturing cast magnesium structural parts of large spacecraft

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Embodiment Construction

[0048] The equipment for manufacturing large-scale spacecraft cast magnesium structural parts according to the invention comprises a sand box unit, a sand core unit and a casting unit.

[0049] The flask unit includes a flat flask 1 at the bottom, an outer flask 2 , a first inner flask 3 and a second inner flask 4 .

[0050] Flat sand box 1, see figure 1 As shown, there is a circular flask support, the support includes a ring-shaped nested first ring 5, and a second ring 6 concentric with the first ring 5 and located inside the first ring 5; Between the circular ring 5 and the second circular ring 6, there are a plurality of evenly distributed radial connectors 7 for connecting the two circular rings; as a preferred embodiment, the preferred planar flask 1 consists of several equally Planar sand box 8 is formed, most preferably is made up of 8 equally divided plane sand boxes 8;

[0051] Outer sand box 2, see figure 2 As shown, it is an annular support, and the inner diame...

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Abstract

The present invention relates to a kind of equipment for manufacturing cast magnesium structural parts of large-scale spacecraft, which comprises a sand box unit, a sand core unit and a casting unit, and the sand box unit is composed of a plane sand box, an outer round sand box, a first inner round sand box and a second round sand box Two inner sand boxes; the sand core unit is composed of base sand core, inner sand core and surface sand core; the casting unit is composed of drainage sprue and sprue basin. Through the effective combination of the sand box unit, the sand core unit and the casting unit, the equipment effectively uses the combination of the sand box and the sand core to realize the purpose of a set of sand box being simple, efficient, and occupying less land, and solves the problems in the prior art .

Description

technical field [0001] The invention relates to equipment for manufacturing large-scale spacecraft cast magnesium structural parts, which is used for manufacturing spacecraft propulsion module structure instrument discs, and belongs to the field of casting technology. Background technique [0002] Since the beginning of the 21st century, my country's aerospace industry has achieved considerable development, and the dimensions of spacecraft such as satellites are gradually increasing, and the platform structure is required to be lightweight. Among metal structural materials, magnesium alloys with the lowest density are widely used in large spacecraft platforms due to their good biocompatibility, highest specific stiffness and specific strength, excellent process performance, and good corrosion resistance. [0003] With the rapid development of my country's aerospace industry, in-depth exploration, the establishment of space stations, and the demand for large launch vehicles h...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): B22C9/02B22C9/08B22C9/10B22C21/00
Inventor 化宜文张高龙邓智燕王玉凤王登峰王利平张军高斌武鹏毕瑞祺
Owner SHANXI SHENZHOU AEROSPACE SCI & TECH CO LTD
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