WO2006134405A1 - Method of manufacturing aluminium-based composite material - Google Patents

Method of manufacturing aluminium-based composite material Download PDF

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Publication number
WO2006134405A1
WO2006134405A1 PCT/GE2006/000007 GE2006000007W WO2006134405A1 WO 2006134405 A1 WO2006134405 A1 WO 2006134405A1 GE 2006000007 W GE2006000007 W GE 2006000007W WO 2006134405 A1 WO2006134405 A1 WO 2006134405A1
Authority
WO
WIPO (PCT)
Prior art keywords
aluminium
crucible
fibers
accordance
basalt
Prior art date
Application number
PCT/GE2006/000007
Other languages
French (fr)
Inventor
Paata Gogoladze
Vazha Chagelishvili
Original Assignee
Paata Gogoladze
Vazha Chagelishvili
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Paata Gogoladze, Vazha Chagelishvili filed Critical Paata Gogoladze
Priority to DE112006001603T priority Critical patent/DE112006001603T5/en
Publication of WO2006134405A1 publication Critical patent/WO2006134405A1/en

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D21/00Casting non-ferrous metals or metallic compounds so far as their metallurgical properties are of importance for the casting procedure; Selection of compositions therefor
    • B22D21/002Castings of light metals
    • B22D21/007Castings of light metals with low melting point, e.g. Al 659 degrees C, Mg 650 degrees C
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C47/00Making alloys containing metallic or non-metallic fibres or filaments
    • C22C47/08Making alloys containing metallic or non-metallic fibres or filaments by contacting the fibres or filaments with molten metal, e.g. by infiltrating the fibres or filaments placed in a mould
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C49/00Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/14Alloys containing metallic or non-metallic fibres or filaments characterised by the fibres or filaments

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)

Abstract

The present invention relates to the field of Metalurgy and, more particularly, it relates to the method of manufacturing an aluminium-based composite material that can be used in producing structural materials having certain advantageous properties. In accordance with the method, melt aluminium is subject to reinforcement with fibers, wherein basalt fibers having diameter of 16-18 micrometers are used as fibers, which are disposed on a crucible bottom in the form a layer having thickness of 8-10 millimeters whereupon an aluminium layer of the same volume is disposed. The crucible together with its content is brought into a furnace and subject to heating up to the temperatures of 8000C - 85O0C, and to stirring continuously for 10-15 minutes at these temperatures by use of a stirring means, the crucible being brought out of the furnace afterwards, and thus manufactured desired product being casted into moulds and cooled.

Description

Method of Manufacturing Aluminium-based Composite
Material
Description Field of application
The present invention relates to the field of Metallurgy and, more particularly, it relates to the method of manufacturing an aluminium-based composite material that can be used in producing structural materials having certain advantageous properties.
Background of the invention
Aluminium alloys and composite materials based thereon are currently extensively used in various fields of technology, such as machine building and aircraft building, in manufacturing household articles and the like, due to their specific properties. It should be noted that each individual case of application of a big veriety of applications found in industry requires different parameters of characteristics. For example, in producing aircraft elements, properties such as mechanical strength and high-temperature strength is of great importance so as to obtain good operational performance. Such properties are achieved by reinforcing the aluminium alloy containig magnesium, silicium, copper, manganese, iron and other admixtures with steel fibers as is described in one of the cited document RU 2243289 (IPC: C22C 47/20). According to the another cited document RU 2217522 (IPC: C22C 49/06), high stiffness, resistance and size stability is achieved by reinforcing the aluminium alloy matrix with successively arranged layers of carbonaceous fibers in parallel to a given direction. According to the yet another cited document SU 1624851 (IPC: B28B 1/52), basalt fibers of 3 millimeters diameter are subject to partitioning, mixing thereof with freshly precipitated gel of aluminium hydroxide, drying and burning at the temperatures in the range of from 5000C to 55O0C so as to produce a heat insulating product. Still another technology known in the art which is disclosed in the Russian application RU 98122445 (IPC: B32B 15/14) teaches that a detail for use in outer space applications is made of magnesium containing aluminium alloy composite material wherein continuous carbonaceous fibers having ultra high value of Young's modulus take 55-65% part of the volume. The most relevant to the present invention is a method for manufacturing composite materials reinforced with a fibrous material, which is disclosed in the Soviet Union patent document SU 602306 (IPC: B22F 3/26), comprising the steps of periodic feeding boron fibers separated by a separating means to the matrix metal - melt of aluminium of mark A7, forming a composite material and, subsequently, recovering it. However, each of the known technologies are disadvantageous in many respects. In particular, complicated facilities, expensive materials and complex technological steps are required for their implementation and, most importantly, the products manufactured by use of these technologies are lack of high hardness as is shown with the data provided in the cited documents.
Technical result
Thus the object and, respectively, the result of the present invention is provision of simplified method for manufacturing an aluminium-based high hardness composite material.
The method in accordance with the present invention is advantageous in that it does not require designing of special-purpose facilities and can be performed by apparatuses that are extensively utilized in technique.
Substance of the invention
The method in accordance to the present invention is performed in the following manner. On a crucible bottom, already made basalt fibers of 10-15 millimeters length and 16-18 micrometers diameter are arranged as a layer of selected thickness, e.g. 8-10 millimeters. Upon the layer, aluminium layer of approximately the same volume is disposed. The crucible together with its content is entered into a furnace and is subject to heating up to the temperatures in the range of from 8000C to 85O0C. Continuous stirring is performed during 10-15 minutes at the above mentioned temperatures by a stirring means whereupon the crucible is brought out of the furnace, the slag is removed from the desired product which is casted into a mould and cooled. In order to provide higher hardness, optimum content of the basalt in the composite material should be 9-13%, the content being easily regulable by changing the ratio of aluminium and basalt masses.
In accordance with one embodiment of the present invention, a number of pairs of fibers and aluminium layers are disposed in succession (one after another) in the crucible. In accordance with another embodiment of the present invention, a crucible made of cast iron or graphite can be utilized. Advantage of such crucibles is their cheapness and substantially lack of adhesiveness with the desired product.
In accordance with still another embodiment of the present invention, a stirring means and moulds made of stainless steel can be utilized. Advantage of such a stirring means and moulds is high durability.
The product manufactured in accordance with the present invention is characterized by high hardness. Conducted Brilell tests revealed the composite material to have the hardness substantially higher then that of starting aluminium. In particular, the obtained hardness value is at least eight times as much as that of starting material. Moreover, the manufactured product is substantially homogenous and its properties considerably depend on nature of interaction occuring between aluminium and basalt, hi results of analysis carried out by means of a microscope, the basalt fibers grains linked to the aluminium by numerous direct bonds can be seen. Presumably, this can be accounted for not only by physical diffusion of aluminium molecules into basalt but also by a chemical reaction, specifically, by recovery of oxides contained in the basalt with aluminium, i.e. substitution of metal atoms contained therein, such as magnesium, iron, manganese atoms, with atoms of aluminium. Next, the recovered metal atoms diffuse into the aluminium. As a result of close bonds, linkage between the aluminium and basalt becomes very strong which apparently contributes to the mechanical properties of the desired material in a positive manner. Presumably, good mechanical properties of the material according to the present invention are accounted for also by proximity between the densities of aluminium and basalt (their values, at the temperatures from 8000C to 85O0C, are in the range of from about 2.3gr/cm3 to about 2.8gr/cm3) and high homogenity which is achieved during the melting process at the time the composite material is subject to continuous stirring. It should be noted that sizes of the basalt grains, their influence on hardness and, also, mechanical properties of the manufactured product have not yet studied in full and further research to be conducted is required. Examples Example 1. hi the process of aluminium reinforcement, stirring of said content of said crucible lasts 10 minutes at the high temperatures (minimum of duration of the process in accordance with the present invention). Besides, the ratio of the basalt and alluminium masses is as little as possible (1 kilogram aluminium versus 0.1 kilogram basalt). Hardness of the manufactured product is lGpa. Example 2.
In the process of aluminium reinforcement, stirring of said content of said crucible lasts 10 minutes at the high temperatures (minimum of duration of the process in accordance with the present invention). Besides, the ratio of the basalt and alluminium masses is as big as possible (1 kilogram aluminium versus 0.15 kilogram basalt). Hardness of the manufactured product is l.βGpa. Example 3.
In the process of aluminium reinforcement, stirring of said content of said crucible lasts 15 minutes at the high temperatures (maximum of duration of the process in accordance with the present invention). Besides, the ratio of the basalt and alluminium masses is as little as possible (1 kilogram aluminium versus 0.1 kilogram basalt). Hardness of the manufactured product is 1.2Gpa. Example 4.
In the process of aluminium reinforcement, stirring of said content of said crucible 15 minutes at the high temperatures (maximum of duration of the process in accordance with the present invention). Besides, the ratio of the basalt and alluminium masses is as big as possible (1 kilogram aluminium versus 0.15 kilogram basalt). Hardness of the manufactured product is 1.9Gpa.
The results set out in the above examples show that the manufactured product retains high hardness with variations of parameter values within the limits stipulated by the present invention.
Although this invention has been described based on its exemplary embodiments which are the most utilitarian and preferable ones, it will be readily appreciated that the above embodiments have been described for illustrative purposes only, and are not limiting. Many other variations, modifications and improvements are possible in the exemplary embodiments without departing from the scope of this invention.

Claims

1. A method of manufacturing an aluminium-based composite material, which comprises reinforcing melt aluminium with fibers, characterized by: using as said fibers basalt fibers having diameters of from 16 micrometers to 18 micrometers; disposing said basalt fibers onto a crucible bottom in the form of a layer; disposing a layer of aluminium material having volume approximately the same as that of said fibers onto said layer of fibers; bringing said crucible together with said content into a furnace; heating said crucible together with said content up to the temperatures in the range of from 8000C to 85O0C; continuously stirring said content of said crucible during 10-15 minutes at said temperatures; casting the manufactured desired product into moulds upon bringing said crucible out of said furnace; and cooling said product.
2. A method in accordance with claim 1, characterized in that said fibers and aluminium are disposed in said crucible as a number of pairs of said fibers and aluminium layers arranged one after another.
3. A method in accordance with claims 1 and 2, characterized in that said crucible is made of cast iron.
4. A method in accordance with claims 1 - 3, characterized in that said crucible is made of graphite.
5. A method in accordance with claims 1 - 4, characterized in that said stirring is performed by a stirring means made of stainless steel.
6. A method in accordance with claims 1 - 5, characterized in that said moulds are made of stainless steel.
PCT/GE2006/000007 2005-06-16 2006-06-16 Method of manufacturing aluminium-based composite material WO2006134405A1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE112006001603T DE112006001603T5 (en) 2005-06-16 2006-06-16 Process for the production of a composite based on aluminum

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GEAP2005008844 2005-06-16
GEAP2005008844 GEP20063997B (en) 2005-06-16 2005-06-16 Method for production of a composite material on the basis of aluminum

Publications (1)

Publication Number Publication Date
WO2006134405A1 true WO2006134405A1 (en) 2006-12-21

Family

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Application Number Title Priority Date Filing Date
PCT/GE2006/000007 WO2006134405A1 (en) 2005-06-16 2006-06-16 Method of manufacturing aluminium-based composite material

Country Status (3)

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DE (1) DE112006001603T5 (en)
GE (1) GEP20063997B (en)
WO (1) WO2006134405A1 (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013117241A1 (en) * 2012-02-10 2013-08-15 Adamco Ag Micro-torque material strengthening by fiber spot-pinning
RU2552464C1 (en) * 2013-11-28 2015-06-10 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Method for obtaining layered composite material based on aluminium alloys and low-alloyed steel
CN106086717A (en) * 2016-07-03 2016-11-09 河北工业大学 A kind of preparation method of foamed aluminium sound absorption acoustic dampening composite

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6183877B1 (en) * 1997-03-21 2001-02-06 Inco Limited Cast-alumina metal matrix composites

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6183877B1 (en) * 1997-03-21 2001-02-06 Inco Limited Cast-alumina metal matrix composites

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2013117241A1 (en) * 2012-02-10 2013-08-15 Adamco Ag Micro-torque material strengthening by fiber spot-pinning
RU2552464C1 (en) * 2013-11-28 2015-06-10 Российская Федерация, от имени которой выступает Министерство промышленности и торговли Российской Федерации (Минпромторг России) Method for obtaining layered composite material based on aluminium alloys and low-alloyed steel
CN106086717A (en) * 2016-07-03 2016-11-09 河北工业大学 A kind of preparation method of foamed aluminium sound absorption acoustic dampening composite

Also Published As

Publication number Publication date
GEP20063997B (en) 2006-12-11
DE112006001603T5 (en) 2008-05-08

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