CN102560293B - Composite type chromium carbide base hard alloy - Google Patents
Composite type chromium carbide base hard alloy Download PDFInfo
- Publication number
- CN102560293B CN102560293B CN 201210019139 CN201210019139A CN102560293B CN 102560293 B CN102560293 B CN 102560293B CN 201210019139 CN201210019139 CN 201210019139 CN 201210019139 A CN201210019139 A CN 201210019139A CN 102560293 B CN102560293 B CN 102560293B
- Authority
- CN
- China
- Prior art keywords
- chromium carbide
- section
- hard alloy
- nuclear
- composite type
- Prior art date
- Legal status (The legal status 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 status listed.)
- Active
Links
Images
Landscapes
- Powder Metallurgy (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Abstract
The invention relates to a composite type chromium carbide base hard alloy, and belongs to the technical field of powder metallurgy. According to the present invention, nickel is adopted as a binder; the alloy comprises a core part and a shell part, wherein the core part is columnar, the shell part is annular, the core part is arranged inside the shell part, components of the core part comprise, by weight, 6-15% of nickel and 85-94% of chromium carbide, components of the shell part comprise, by weight, 20-40% of nickel and 60-80% of chromium carbide, and a volume ratio of the core part to the shell part is 1:5-5:1. The alloy of the present invention provides higher strength and hardness than the conventional chromium carbide base hard alloy, and has a wide use range.
Description
Technical field
The invention belongs to powder metallurgical technology, particularly a kind of composite type chromium carbide base hard alloy.
Background technology
Wimet is described as the tooth of modern industry owing to have good wear resistance.Conventional Wimet is mainly tungsten carbide base carbide alloy (code name is YG), and take cobalt as binding agent, it is under the free from corrosion condition of normal temperature, excellent property, behaviour in service is good, yet in the work condition environment of high temperature corrosion, wolfram varbide is easy to oxidation, greatly reduces its work-ing life.
Type chromium carbide base hard alloy (code name is CN) is take chromium carbide as matrix, take nickel as binding agent, compare with tungsten carbide base carbide alloy, have good chemical stability and high thermal resistance, but acid-and base-resisting, seawater, oil and other corrosive medium, heating was not any change in 2 hours under 1000 ℃ of air conditionses, and tungsten carbide base carbide alloy has begun oxidation, modification, has broken in the time of 600 ℃, and its proportion is lighter, nearly be half of tungsten carbide base carbide alloy, greatly saved starting material.But traditional type chromium carbide base hard alloy relative density is lower, and bending strength is relatively poor, has greatly limited its range of application.
Summary of the invention
The object of the present invention is to provide a kind of composite type chromium carbide base hard alloy, take nickel as binding agent, formed by nuclear section and shell section; Nuclear section is column, shell section in the form of a ring, nuclear section is contained in the shell section; Nuclear section composition is: nickel: 6%~15%, and chromium carbide 855%~94%; Shell section composition is: nickel: 20%~40%, and chromium carbide: 60%~80%; Be weight percentage; Shell section is enclosed in and consists of the conjugated fibre that cross-sectional dimension is 50~1000 μ m around the nuclear section, and nuclear section is column, shell section in the form of a ring, nuclear section is contained in the shell section; Its center section and shell section volume ratio are 1: 5~5: 1, and this conjugated fibre stack consists of the structure of this composite type chromium carbide base hard alloy.
The below describes the preparation process of this composite type chromium carbide base hard alloy in detail:
At first adopt conventional powder metallurgical technique, wet-milling after the batching, mix wax, prepare level nuclear section and shell section by die forming, nuclear section is column, shell section in the form of a ring, nuclear section can be contained in the shell section, nuclear section and shell section are grouped together, carry out hot extrusion, the blank that squeezes out is grouped together to reload carries out hot extrusion in the hot-extrusion mold, the like, the conjugated fibre that cross-sectional dimension is 50~1000 μ m finally obtained through the repeatedly hot extrusion of several times, this conjugated fibre is superimposed together and forms this composite type chromium carbide base hard alloy extrusion billet, through dewaxing, namely prepare this composite type chromium carbide base hard alloy behind the high temperature sintering.
This composite type chromium carbide base hard alloy is because shell section nickel content is higher, so have higher intensity, and because core nickel content is lower, so have higher hardness, therefore this composite type chromium carbide base hard alloy material has higher intensity in addition when having higher hardness, the use range of type chromium carbide base hard alloy be can greatly widen, technical progress and the industry development of China's cemented carbide industry are conducive to.
Description of drawings:
Fig. 1 is composite type chromium carbide base hard alloy structure partial cross sectional representation, and black part is divided into nuclear section among the figure, and white portion is shell section.
Fig. 2 is composite type chromium carbide base hard alloy structure partial vertical section synoptic diagram, and black part is divided into nuclear section among the figure, and white portion is shell section.
Embodiment
Example 1
(be nickeliferous weight ratio 6% with CN6, surplus is chromium carbide) for examining, (be nickeliferous weight ratio 20% with CN20, surplus is chromium carbide) be shell, nucleocapsid volume ratio 1: 1, the conjugated fibre cross-sectional dimension is 1000 μ m, and this composite type chromium carbide base hard alloy material mechanical performance is as shown in the table:
Density (g/cm 3) | Hardness (HRA) | Bending strength (MPa) |
6.85~6.95 | >89 | >1050 |
Example 2
(be nickeliferous weight ratio 6% with CN6, surplus is chromium carbide) for examining, (be nickeliferous weight ratio 30% with CN30, surplus is chromium carbide) be shell, pressed the nucleocapsid volume ratio 1: 3, the conjugated fibre cross-sectional dimension is 400 μ m, and this composite type chromium carbide base hard alloy material mechanical performance is as shown in the table:
Density (g/cm 3) | Hardness (HRA) | Bending strength (MPa) |
7.1~7.2 | >87 | >1150 |
Example 3
(be nickeliferous weight ratio 6% with CN6, surplus is chromium carbide) for examining, (be nickeliferous weight ratio 40% with CN40, surplus is chromium carbide) be shell, pressed the nucleocapsid volume ratio 5: 1, the conjugated fibre cross-sectional dimension is 50 μ m, and this composite type chromium carbide base hard alloy material mechanical performance is as shown in the table:
Density (g/cm 3) | Hardness (HRA) | Bending strength (MPa) |
6.85~6.95 | >88 | >1050 |
Example 4
(be nickeliferous weight ratio 10% with CN10, surplus is chromium carbide) for examining, (be nickeliferous weight ratio 20% with CN20, surplus is chromium carbide) be shell, nucleocapsid volume ratio 1: 1, the conjugated fibre cross-sectional dimension is 1000 μ m, and this composite type chromium carbide base hard alloy material mechanical performance is as shown in the table:
Density (g/cm 3) | Hardness (HRA) | Bending strength (MPa) |
6.9~7.0 | >88 | >1050 |
Example 5
(be nickeliferous weight ratio 10% with CN10, surplus is chromium carbide) for examining, (be nickeliferous weight ratio 30% with CN30, surplus is chromium carbide) be shell, nucleocapsid volume ratio 1: 4, the conjugated fibre cross-sectional dimension is 400 μ m, and this composite type chromium carbide base hard alloy material mechanical performance is as shown in the table:
Density (g/cm 3) | Hardness (HRA) | Bending strength (MPa) |
7.1~7.2 | >87 | >1150 |
Example 6
(be nickeliferous weight ratio 10% with CN10, surplus is chromium carbide) for examining, (be nickeliferous weight ratio 40% with CN40, surplus is chromium carbide) be shell, nucleocapsid volume ratio 2: 1, the conjugated fibre cross-sectional dimension is 50 μ m, and this composite type chromium carbide base hard alloy material mechanical performance is as shown in the table:
Density (g/cm 3) | Hardness (HRA) | Bending strength (MPa) |
6.9~7.0 | >88 | >1050 |
Example 7
(be nickeliferous weight ratio 15% with CN15, surplus is chromium carbide) for examining, (be nickeliferous weight ratio 20% with CN20, surplus is chromium carbide) be shell, nucleocapsid volume ratio 1: 1, the conjugated fibre cross-sectional dimension is 1000 μ m, and this composite type chromium carbide base hard alloy material mechanical performance is as shown in the table:
Density (g/cm 3) | Hardness (HRA) | Bending strength (MPa) |
7.0~7.5 | >88 | >1100 |
Example 8
(be nickeliferous weight ratio 15% with CN15, surplus is chromium carbide) for examining, (be nickeliferous weight ratio 30% with CN30, surplus is chromium carbide) be shell, nucleocapsid volume ratio 1: 5, the conjugated fibre cross-sectional dimension is 400 μ m, and this composite type chromium carbide base hard alloy material mechanical performance is as shown in the table:
Density (g/cm 3) | Hardness (HRA) | Bending strength (MPa) |
7.15~7.20 | >87 | >1150 |
Example 9
(be nickeliferous weight ratio 15% with CN15, surplus is chromium carbide) for examining, (be nickeliferous weight ratio 40% with CN40, surplus is chromium carbide) be shell, nucleocapsid volume ratio 3: 1, the conjugated fibre cross-sectional dimension is 50 μ m, and this composite type chromium carbide base hard alloy material mechanical performance is as shown in the table:
Density (g/cm 3) | Hardness (HRA) | Bending strength (MPa) |
7.0~7.1 | >87 | >1100 |
Claims (1)
1. a composite type chromium carbide base hard alloy is characterized in that: take nickel as binding agent, be comprised of nuclear section and shell section; Nuclear section is column, shell section in the form of a ring, nuclear section is contained in the shell section; Nuclear section composition is: nickel: 6% ~ 15%, and chromium carbide 85%~94%; Shell section composition is: nickel: 20% ~ 40%, and chromium carbide: 60%~80%; Be weight percentage; Nuclear section and shell section volume ratio are 1:5 ~ 5:1;
Shell section is enclosed in around the nuclear section, consists of conjugated fibre, and cross-sectional dimension is 50 ~ 1000 μ m, and these conjugated fibres are superimposed and consist of the structure of this composite type chromium carbide base hard alloy;
The preparation process of this composite type chromium carbide base hard alloy is as follows:
At first adopt conventional powder metallurgical technique, wet-milling after the batching, mix wax, prepare level nuclear section and shell section by die forming, nuclear section is column, shell section in the form of a ring, nuclear section is contained in the shell section, nuclear section and shell section are grouped together, carry out hot extrusion, the blank that squeezes out is grouped together to reload carries out hot extrusion in the hot-extrusion mold, the like, the conjugated fibre that cross-sectional dimension is 50~1000 μ m finally obtained through the repeatedly hot extrusion of several times, this conjugated fibre is superimposed together and forms this composite type chromium carbide base hard alloy extrusion billet, through dewaxing, namely prepare this composite type chromium carbide base hard alloy behind the high temperature sintering.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201210019139 CN102560293B (en) | 2012-01-20 | 2012-01-20 | Composite type chromium carbide base hard alloy |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN 201210019139 CN102560293B (en) | 2012-01-20 | 2012-01-20 | Composite type chromium carbide base hard alloy |
Publications (2)
Publication Number | Publication Date |
---|---|
CN102560293A CN102560293A (en) | 2012-07-11 |
CN102560293B true CN102560293B (en) | 2013-05-29 |
Family
ID=46406890
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN 201210019139 Active CN102560293B (en) | 2012-01-20 | 2012-01-20 | Composite type chromium carbide base hard alloy |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN102560293B (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104726729B (en) * | 2013-12-24 | 2017-01-11 | 湖南博云东方粉末冶金有限公司 | Method for adjusting pressing condition of hard alloy |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS6293323A (en) * | 1985-10-17 | 1987-04-28 | Kobe Steel Ltd | Whisker-reinforced al alloy composite material |
JPH03267329A (en) * | 1990-03-19 | 1991-11-28 | Tokai Carbon Co Ltd | Production of high heat-resistant al alloy composite material |
-
2012
- 2012-01-20 CN CN 201210019139 patent/CN102560293B/en active Active
Non-Patent Citations (2)
Title |
---|
JP平3-267329A 1991.11.28 |
JP昭62-093323A 1987.04.28 |
Also Published As
Publication number | Publication date |
---|---|
CN102560293A (en) | 2012-07-11 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CN103882275B (en) | A kind of toughness reinforcing Wimet and preparation method thereof | |
CN101285371B (en) | Fabrication technology of diamond positioning and arrangement impregnated rock bit | |
CN102335746B (en) | Powder metallurgy sedan synchronizer gear hub and production method thereof | |
CN101418394A (en) | Superhard composite material and method for preparation thereof | |
CN104342592B (en) | High-titanium-carbide steel bond hard alloy mold material | |
CN102828096B (en) | Metal ceramic cutting tool material and preparation method thereof | |
CN104213012A (en) | Bicrystal structure anticorrosion hard alloy and preparation method thereof | |
CN102605290A (en) | Powder metallurgy material used for pressing and sintering exhaust seat ring | |
CN106180732B (en) | Diamond compact and production method | |
CN102513539A (en) | Manufacture method for tire casing of diamond wire saw sintered type bead | |
CN106392907A (en) | Method for quickly preparing dense and superhard grinding and drilling tool based on self-propagating reaction | |
CN103691959A (en) | Composite structure hard alloy gear and preparation method thereof | |
CN103774023A (en) | Titanium carbonitride metal ceramic sealing element and preparation method thereof | |
CN102560293B (en) | Composite type chromium carbide base hard alloy | |
CN102943196A (en) | Wear and corrosion resistant material for environmental protection engineering and preparation method | |
CN104088897A (en) | Radial bearing of screw rod drill | |
CN104550985A (en) | Low-apparent-density copper zinc alloy brass powder and preparing method thereof | |
CN102965532B (en) | Preparation method for fully-compact W-Ni-Mn heavy alloy | |
CN104190918B (en) | Powder sintering porous filter alloy, preparation method thereof and pre-pressing molding body for preparing powder sintering porous filter alloy | |
CN103014544A (en) | Highly-wear-resistant powder metallurgy valve seat | |
CN103084572A (en) | Forming stamping mold with wear-resistant coating | |
RU2010125194A (en) | METHOD FOR PRODUCING SINTERED POROUS ARTICLES FROM PSEUM ALLOY ON THE BASIS OF TUNGSTEN | |
CN104190935B (en) | The preparation method of powder sintered porous body and prepare the pre-molding body of the sintered body | |
CN103938048B (en) | Carbon aluminium titanium base electric contact material and its production and use | |
CN104100638A (en) | Bearing for oil and gas development drilling |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
C06 | Publication | ||
PB01 | Publication | ||
C10 | Entry into substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
C14 | Grant of patent or utility model | ||
GR01 | Patent grant |