Method of manufacturing stephanoporate metal honeycomb structure member

A honeycomb structure and porous metal technology, which is applied in the field of metal powder manufacturing powder metallurgy parts, can solve the problems of installation, clamping, cleaning and maintenance troubles, difficulty in adjusting the range of filtration accuracy, and difficulty in manufacturing, etc. The effect of high utilization

Inactive Publication Date: 2008-06-11
SHANGHAI RES INST OF MATERIAL
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AI-Extracted Technical Summary

Problems solved by technology

[0003] The traditional porous honeycomb is made of ceramic clay, and its filtration accuracy range is difficult to adjust, especially when a larger filter...
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Abstract

The invention relates to a process for preparing metal honeycomb structural components with multi holes. The process adopts a powder metallurgic method and comprises adding binding agent into metal powder or alloy powder, squeezing powder after mixing evenly, sintering pressed compacts in vacuum or protecting environment after drying and removing the binding agent, and thereby the metal honeycomb structural components with multi holes can be prepared. Compared with the prior art, the invention is characterized in that procedures are simple, material utilizing rate is high, technological processes are short, cost is low, mass productions are easy and the like.

Technology Topic

Powder metallurgyHoneycomb structure +4

Examples

  • Experimental program(3)

Example Embodiment

[0014] Example 1
[0015] A method for preparing a porous metal honeycomb structure. When the alloy powder used in the method is chromium-nickel, chromium-nickel-molybdenum stainless steel, the alloy powder and water-based binder prepared at a weight ratio of 80:20 Pre-mix in a mixer for 30 minutes, then mix on the mixer for 100-120 minutes to form a dough, put it into an extrusion die, and extrude under an extrusion force of <100MPa, and the extruded billet is at a temperature of <200°C Dry and vacuum sinter at a temperature of 1200-1350°C to form a porous metal honeycomb structure; the weight formula of the binder is 10% polyvinyl alcohol, 20% carboxymethyl cellulose, and 4% glycerin. Ethanol 3%, water 63%.

Example Embodiment

[0016] Example 2
[0017] A method for preparing porous metal honeycomb structure. When the alloy powder used in the method is tin bronze, 6-6-3 bronze, or iron-copper, the alloy powder prepared in a weight ratio of 60:40 and water-based adhesive The binder is pre-mixed in a mixer for 30 minutes, and then mixed on the mixer for 100-120 minutes to form a dough, which is placed in an extrusion die and extruded under an extrusion force of <100MPa. Drying at a temperature of ℃, sintering in an ammonia decomposition protective atmosphere at a temperature of 750-850℃, can be made into a porous metal honeycomb structure; the weight formula of the binder is 15% polyvinyl alcohol, carboxymethyl fiber Vegetarian 15%, glycerol 6%, ethanol 0.5%, water 63.5%.

Example Embodiment

[0018] Example 3
[0019] A method for preparing a porous metal honeycomb structure. When the alloy powder used in the method is an iron-chromium-aluminum heat-resistant alloy, the alloy powder and water-based binder prepared in a weight ratio of 90:10 are placed in a mixer Pre-mix for 30 minutes, then mix on a mixer for 100-120 minutes to form a dough, put it in an extrusion die, and extrude under an extrusion force of <100MPa, and dry the extruded at a temperature of <200°C. Vacuum or dry H at a temperature of 1250-1350℃ 2 (Dew point -60℃) sintered in an atmosphere, the porous metal honeycomb structure can be made; the weight formula of the binder is 5% of polyvinyl alcohol, 25% of carboxymethyl cellulose, 1% of glycerin, and 5% of ethanol. %, water 64%.

PUM

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Description & Claims & Application Information

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