CN103084564A - Process for preparing composite wear-resistant component - Google Patents
Process for preparing composite wear-resistant component Download PDFInfo
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- CN103084564A CN103084564A CN201210388190XA CN201210388190A CN103084564A CN 103084564 A CN103084564 A CN 103084564A CN 201210388190X A CN201210388190X A CN 201210388190XA CN 201210388190 A CN201210388190 A CN 201210388190A CN 103084564 A CN103084564 A CN 103084564A
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Abstract
The invention discloses a process for preparing a composite wear-resistant component. The process comprises the following steps of: putting one or more metal and non-metal materials into a heating container, and uniformly mixing; heating an obtained mixed material to a temperature at which at least one material is completely fused; fully stirring fused materials and unfused materials to obtain a mixture; pre-heating a mould to a temperature approaching the temperature at which at least one material is completely fused; pouring the obtained mixture into the mould, covering the mould by using a mould cover, and uniformly mixing the mixture in the mould by rotation and vibration of a mechanical device; downwards pressing the mould cover; performing pressing on the upper part of the mould, and gradually reducing the temperature of the mould; when the temperature of the mould is reduced to the normal temperature, standing for a moment for fully cooling; and opening the mould cover to obtain the composite wear-resistant component. Compared with the prior art, the process has the advantages that problems of low strength, narrow application range and the like of the conventional composite wear-resistant material are solved.
Description
Technical field
The present invention relates to the method for manufacturing technology in component of machine manufacturing technology field, particularly a kind of wearing piece.
Background technology
Existing composite wear-resistant part is to adopt welding or bonding method that high-abrasive material is fixed on matrix mostly, this method with welding or the high-abrasive material that is adhesively fixed, there are the defectives such as gap due to bond strength between not high and high-abrasive material, easily cause high-abrasive material to come off, have a strong impact on its service life.As both combining with traditional casting technique, because high-abrasive material is general and physical property difference matrix material is larger, after the matrix material fusing can occurring, high-abrasive material is because fusing point is higher lower with density, always float over the matrix material end face this phenomenon that has melted, therefore, existing casting technique can't will both combine equably.
Summary of the invention
The invention provides a kind of composite wear-resistant part method of manufacturing technology, it can solve in metal casting technique, and the nonmetallic materials of different performance material can't fuse the problem in metallic matrix.
In order to address the above problem, the technical scheme of this composite wear-resistant part method of manufacturing technology is: this composite wear-resistant part method of manufacturing technology, include following steps: step 101: batch mixing is placed on one or more metal and one or more nonmetallic materials in a heating container and mixes; Step 102: heat up, the composite material of gained in above-mentioned steps 101 is heated to the temperature that at least a material wherein melts fully; Step 103: stir, material and unfused material that above-mentioned steps 102 is melted stir, and make it abundant mixing, obtain compound; Step 104: mould and die preheating, described mould has bed die, this bed die is provided with the cavity of upper opening, described mould and die preheating to above-mentioned steps 102 in the temperature that approaches of the complete fusion temperature of the material of fusing fully at first; Step 105: pour mould into, after the compound of above-mentioned steps 103 gained being poured in the described mold bottom die cavity of above-mentioned steps 104, cover die cover, the bottom end face of this die cover is corresponding with described mold bottom die cavity, and the lateral surface of described die cover is provided with bulge loop; Step 106: mold rotation and vibration, described mould are rotated by mechanical device and are vibrated and make within it that the material of section mixes; Step 107: mould pressurizing, in the pressurization of the top of described die cover, make the inside of described mould produce pressure, the other materials that swims on the material surface that melts is fully compressed in the material of fusing fully; Step 108: the slow cooling of pressurize, described mould keep certain pressure constant, and reduce rallentando the heating-up temperature of described mould; Step 109: normal temperature is standing, after described mold temperature drops to normal temperature, standing a period of time, makes it fully cooling; Step 110: the demoulding, open described die cover, namely get this composite wear-resistant part.
Owing to adopting technique scheme, the present invention compared with prior art has following beneficial effect:
The present invention has high-abrasive material and matrix material in conjunction with closely, evenly, and the advantage such as have wide range of applications.
Description of drawings
Fig. 1 is schematic flow sheet of the present invention.
Fig. 2 is the structural representation of the embodiment of the present invention 1.
The specific embodiment
Embodiments of the present invention is further illustrated below in conjunction with accompanying drawing:
Composite wear-resistant part method of manufacturing technology shown in Figure 1, include following steps: step 101: batch mixing is placed on one or more metal such as iron, manganese and one or more nonmetallic materials such as aluminium oxide ceramics, zirconia ceramics by a certain percentage in a heating container and mixes; Step 102: heat up, the composite material of gained in above-mentioned steps 101 is heated to the temperature that at least a material wherein melts fully; Step 103: stir, material and unfused material that above-mentioned steps 102 is melted stir, and make it abundant mixing, obtain compound; Step 104: mould and die preheating, mould have bed die 1, and this bed die 1 is provided with the cavity of upper opening, mould and die preheating to above-mentioned steps 102 in the temperature that approaches of the complete fusion temperature of the material of fusing fully at first; Step 105: pour mould into, after the compound of above-mentioned steps 103 gained being poured in mold bottom die 1 cavity of above-mentioned steps 104, cover die cover 2, the bottom end face of this die cover 2 is corresponding with mold bottom die 1 cavity, and the lateral surface of die cover 2 is provided with bulge loop; Step 106: mold rotation and vibration, mould are namely vibrated the rotation of turntable 3 and vibration by mechanical device makes within it that the material of section mixes; Step 107: mould pressurizing, progressively be forced into setting value on the top of die cover 2, the pressure setting scope is 0.01-0.2MPa, makes the inside of mould produce pressure, and the other materials that swims on the material surface that melts is fully compressed in the material of fusing fully; Step 108: the slow cooling of pressurize, mould keep certain pressure constant, and reduce rallentando the heating-up temperature of mould; Step 109: normal temperature is standing, after mold temperature drops to normal temperature, standing a period of time, makes it fully cooling; Step 110: the demoulding, open die cover 2, namely get this composite wear-resistant part.
Claims (1)
1. composite wear-resistant part method of manufacturing technology is characterized in that including following steps:
Step 101: batch mixing is placed on one or more metal and one or more nonmetallic materials in a heating container and mixes;
Step 102: heat up, the composite material of gained in above-mentioned steps 101 is heated to the temperature that at least a material wherein melts fully;
Step 103: stir, material and unfused material that above-mentioned steps 102 is melted stir, and make it abundant mixing, obtain compound;
Step 104: mould and die preheating, described mould has bed die, this bed die is provided with the cavity of upper opening, described mould and die preheating to above-mentioned steps 102 in the temperature that approaches of the complete fusion temperature of the material of fusing fully at first;
Step 105: pour mould into, after the compound of above-mentioned steps 103 gained being poured in the described mold bottom die cavity of above-mentioned steps 104, cover die cover, the bottom end face of this die cover is corresponding with described mold bottom die cavity, and the lateral surface of described die cover is provided with bulge loop;
Step 106: mold rotation and vibration, described mould are rotated by mechanical device and are vibrated and make within it that the material of section mixes;
Step 107: mould pressurizing, in the pressurization of the top of described die cover, make the inside of described mould produce pressure, the other materials that swims on the material surface that melts is fully compressed in the material of fusing fully;
Step 108: the slow cooling of pressurize, described mould keep certain pressure constant, and reduce rallentando the heating-up temperature of described mould;
Step 109: normal temperature is standing, after described mold temperature drops to normal temperature, standing a period of time, makes it fully cooling;
Step 110: the demoulding, open described die cover, namely get this composite wear-resistant part.
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CN103084564B CN103084564B (en) | 2015-02-25 |
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Citations (8)
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JPS61104039A (en) * | 1984-10-25 | 1986-05-22 | Toshiba Corp | Manufacture of whisker reinforced metallic composite material |
JPH0293031A (en) * | 1988-09-27 | 1990-04-03 | Idea Res:Kk | Manufacture of fiber reinforced composite material |
CN1099073A (en) * | 1993-08-14 | 1995-02-22 | 林清彬 | A kind of method and apparatus of making matrix material |
CN1126123A (en) * | 1995-08-29 | 1996-07-10 | 华南理工大学 | Surface strengthening method for aluminium and its alloy |
CN1144849A (en) * | 1995-09-07 | 1997-03-12 | 哈尔滨工业大学 | Simple and direct inter metallic compound preparation and forming method |
JP2006188735A (en) * | 2005-01-07 | 2006-07-20 | Am Technology:Kk | Rotor with excellent creep characteristic |
CN101578149A (en) * | 2007-01-11 | 2009-11-11 | 盖茨公司 | Method of reinforcing low melting temperature cast metal parts |
CN102108450A (en) * | 2009-12-25 | 2011-06-29 | 清华大学 | Method for preparing magnesium-based composite material |
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2012
- 2012-10-15 CN CN201210388190.XA patent/CN103084564B/en active Active
Patent Citations (8)
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JPS61104039A (en) * | 1984-10-25 | 1986-05-22 | Toshiba Corp | Manufacture of whisker reinforced metallic composite material |
JPH0293031A (en) * | 1988-09-27 | 1990-04-03 | Idea Res:Kk | Manufacture of fiber reinforced composite material |
CN1099073A (en) * | 1993-08-14 | 1995-02-22 | 林清彬 | A kind of method and apparatus of making matrix material |
CN1126123A (en) * | 1995-08-29 | 1996-07-10 | 华南理工大学 | Surface strengthening method for aluminium and its alloy |
CN1144849A (en) * | 1995-09-07 | 1997-03-12 | 哈尔滨工业大学 | Simple and direct inter metallic compound preparation and forming method |
JP2006188735A (en) * | 2005-01-07 | 2006-07-20 | Am Technology:Kk | Rotor with excellent creep characteristic |
CN101578149A (en) * | 2007-01-11 | 2009-11-11 | 盖茨公司 | Method of reinforcing low melting temperature cast metal parts |
CN102108450A (en) * | 2009-12-25 | 2011-06-29 | 清华大学 | Method for preparing magnesium-based composite material |
Non-Patent Citations (2)
Title |
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杨涛林等: "颗粒增强金属基复合材料的研究进展", 《铸造技术》, vol. 27, no. 08, 31 August 2006 (2006-08-31), pages 871 - 873 * |
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