CN106956090A - Surfacing cobalt-chromium-tungsten alloy powder and its application method - Google Patents
Surfacing cobalt-chromium-tungsten alloy powder and its application method Download PDFInfo
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- CN106956090A CN106956090A CN201710208756.9A CN201710208756A CN106956090A CN 106956090 A CN106956090 A CN 106956090A CN 201710208756 A CN201710208756 A CN 201710208756A CN 106956090 A CN106956090 A CN 106956090A
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- Prior art keywords
- chromium
- cobalt
- alloy powder
- tungsten alloy
- surfacing
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Classifications
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/40—Making wire or rods for soldering or welding
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Powder Metallurgy (AREA)
Abstract
The present invention relates to surfacing cobalt-chromium-tungsten alloy powder and its application method, include the component of following mass percent:C is that 3~4%, Cr is that 35~45%, Si is that 0.5~0.9%, W is that 15~17%, Fe is that 0.1~0.5%, Mn is that 1~2%, Mo is that 1~2%, Ni is that 4~5%, surplus is Co.Methods described step is as follows:The first step:Workpiece surface processing;Second step:The inspection of cobalt-chromium-tungsten alloy powder;3rd step:Drying process;4th step:Cobalt-chromium-tungsten alloy powder heap is welded in by workpiece surface using plasma arc powder surfacing equipment.The present invention has the premium properties such as heat-resisting, anti-corrosion, high red hardness.Impact strength is poor, and tearing tendency is sensitive in weld deposit process.Heap is welded in behind the surface of abrasion workpiece, it is possible to achieve the reparation to abrading section, realizes the recycling of abrasion workpiece;The present invention can also the new workpiece surface of built-up welding, so as to play a part of pre- protection.
Description
Technical field
The present invention relates to welding processing technical field, specifically surfacing cobalt-chromium-tungsten alloy powder and its application method.
Background technology
Spiral propeller, mounted in the accelerator of wheel quarter.In use for some time, mill occurs in spiral propeller
Damage, have influence on the normal of steamer and give it the gun, the service life for also resulting in spiral propeller drastically shortens.If more being renewed
Spiral propeller, cost is higher.
And for example pump leaf valve seat, bearing, no, it is necessary to timely be changed when producing a certain degree of abrasion when deployed
Then influence whether that normal install positions and motion transmission, but changing the cost that equipment can be caused to use again increases.
Three of the above part, according to replacing, the part after abrasion can be dropped, cause along the wasting of resources, urgently
Need it is a kind of the part of above-mentioned abrasion can be subjected to repairing sizes, so as to realize the material of recycling.
The content of the invention
In order to solve deficiency of the prior art, the present invention proposes surfacing cobalt-chromium-tungsten alloy powder and its application method.
The technical problems to be solved by the invention are realized using following technical scheme:
Surfacing cobalt-chromium-tungsten alloy powder, includes the component of following mass percent:
C is that 3~4%, Cr is that 35~45%, Si is that 0.5~0.9%, W is that 15~17%, Fe is that 0.1~0.5%, Mn is
1~2%, Mo is that 1~2%, Ni is that 4~5%, surplus is Co.
The surfacing application method of cobalt-chromium-tungsten alloy powder, methods described step is as follows:
The first step:Workpiece surface processing;
Second step:The inspection of cobalt-chromium-tungsten alloy powder:Moisture absorption phenomenon or storage period are checked whether there is whether more than 3 months;
3rd step:Drying process:Cobalt-chromium-tungsten alloy powder is incubated 2 hours in 150 DEG C of container;
4th step:Cobalt-chromium-tungsten alloy powder heap is welded in by workpiece surface using plasma arc powder surfacing equipment.
The beneficial effects of the invention are as follows:The invention belongs to face-centered cubic solid solution alloy, carbon and W content are high in alloy, make
The wear-resisting material abrasion characteristic of alloy is significantly improved.With premium properties such as heat-resisting, anti-corrosion, high red hardness.Impact strength is poor, heap
Tearing tendency is sensitive during weldering.Heap is welded in behind the surface of abrasion workpiece, it is possible to achieve the reparation to abrading section, realizes abrasion
The recycling of workpiece;The present invention can also the new workpiece surface of built-up welding, so as to play a part of pre- protection.
Embodiment
In order that the present invention technological means, creation characteristic, reached purpose and effect for realizing are easy to understand, below it is right
The present invention is expanded on further.
Embodiment one:
Surfacing cobalt-chromium-tungsten alloy powder, includes the component of following mass percent:
C be 3%, Cr be 35%, Si be 0.9%, W be 16%, Fe be 0.1%, Mn be 1%, Mo be 1%, Ni be 5%,
Surplus is Co.
The surfacing application method of cobalt-chromium-tungsten alloy powder, methods described step is as follows:
The first step:Workpiece surface processing;
Second step:The inspection of cobalt-chromium-tungsten alloy powder:Moisture absorption phenomenon or storage period are checked whether there is whether more than 3 months;
3rd step:Drying process:Cobalt-chromium-tungsten alloy powder is incubated 2 hours in 150 DEG C of container;
4th step:Cobalt-chromium-tungsten alloy powder heap is welded in by workpiece surface using plasma arc powder surfacing equipment.
Embodiment two:
Surfacing cobalt-chromium-tungsten alloy powder, includes the component of following mass percent:
C be 4%, Cr be 39%, Si be 0.7%, W be 15%, Fe be 0.5%, Mn be 2%, Mo be 2%, Ni be 4%,
Surplus is Co.
Surfacing is identical with embodiment one with the application method of cobalt-chromium-tungsten alloy powder.
Embodiment three:
Surfacing cobalt-chromium-tungsten alloy powder, includes the component of following mass percent:
C is that 3.6%, Cr is that 45%, Si is that 0.5%, W is that 17%, Fe is that 0.3%, Mn is that 1.5%, Mo is 1.4%, Ni
It is Co for 4.6%, surplus.
Surfacing is identical with embodiment one with the application method of cobalt-chromium-tungsten alloy powder.
Example IV:
Surfacing cobalt-chromium-tungsten alloy powder, includes the component of following mass percent:
C is that 3.2%, Cr is that 42%, Si is that 0.6%, W is that 17%, Fe is that 0.4%, Mn is that 1.6%, Mo is 1.7%, Ni
It is Co for 4.3%, surplus.
Surfacing is identical with embodiment one with the application method of cobalt-chromium-tungsten alloy powder.
In order to prove the actual effect and performance of the present invention, after spy implements embodiments of the invention one to embodiment three
Layer performance be tested, data statistics is as follows:
From above-mentioned experimental data, after technical scheme so that the hardness of overlay cladding is promoted to 52HRc
More than, bond strength is up to 90MPa, and the hardness and bond strength for the layer being made more than prior art are high, greatly improve
The wearability and corrosion resistance of layer, extend the service life of workpiece.Meanwhile, after technical scheme, layer
Oxidation resistance temperature up to 1100 DEG C, it is proposed that the temperature that workpiece is used be no more than 950 DEG C.
The present invention has also carried out corrosion resistance test in addition, and experiment test is as follows:
Wherein, 30% acetic acid, 80% formic acid are fluidized state, and 65% nitric acid, 50% phosphoric acid, 5% sulfuric acid are 66 DEG C,
Excellent, good, middle reflection is rotproofness performance of the layer for various Corrosive Materias.Can by the test of above-mentioned corrosion resistance test
Know, the present invention is after workpiece surface formation layer, and corrosion resistance is greatly improved.
General principle, principal character and the advantages of the present invention of the present invention has been shown and described above.The technology of the industry
Personnel are not it should be appreciated that the present invention is limited by step embodiment, and that described in step embodiment and specification is the present invention
Principle, without departing from the spirit and scope of the present invention, various changes and modifications of the present invention are possible, these change and
Improvement all fall within the protetion scope of the claimed invention.The claimed scope of the invention is by appending claims and its equivalent
Thing is defined.
Claims (2)
1. surfacing cobalt-chromium-tungsten alloy powder, it is characterised in that:Include the component of following mass percent:
C be 3~4%, Cr be 35~45%, Si be 0.5~0.9%, W be 15~17%, Fe be 0.1~0.5%, Mn be 1~
2%th, Mo is that 1~2%, Ni is that 4~5%, surplus is Co.
2. the surfacing application method of cobalt-chromium-tungsten alloy powder, it is characterised in that:Methods described step is as follows:
The first step:Workpiece surface processing;
Second step:The inspection of cobalt-chromium-tungsten alloy powder:Moisture absorption phenomenon or storage period are checked whether there is whether more than 3 months;
3rd step:Drying process:Cobalt-chromium-tungsten alloy powder is incubated 2 hours in 150 DEG C of container;
4th step:Cobalt-chromium-tungsten alloy powder heap is welded in by workpiece surface using plasma arc powder surfacing equipment.
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CN201710208756.9A CN106956090A (en) | 2017-03-31 | 2017-03-31 | Surfacing cobalt-chromium-tungsten alloy powder and its application method |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107322186A (en) * | 2017-08-26 | 2017-11-07 | 安徽鼎恒再制造产业技术研究院有限公司 | Steel rolling guide roller surfacing cobalt-based alloy powder and its welding procedure |
CN107322185A (en) * | 2017-08-19 | 2017-11-07 | 安徽鼎恒再制造产业技术研究院有限公司 | Gate valve built-up welding continuous casting casting rod and its welding procedure |
CN107350662A (en) * | 2017-08-26 | 2017-11-17 | 安徽鼎恒再制造产业技术研究院有限公司 | Valve repair iron-base self-fluxing alloy powder and its welding procedure |
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CN1038609A (en) * | 1989-05-12 | 1990-01-10 | 冶金工业部钢铁研究总院 | Alloy for surfacing |
JPH0584592A (en) * | 1991-09-27 | 1993-04-06 | Toyota Motor Corp | Cobalt-based filling alloy excellent in wear resistance and opponent attackability |
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KR20110096362A (en) * | 2010-02-22 | 2011-08-30 | 금용기계 주식회사 | High heat-resistance exhaust valve spindle of marine engine having excellent wear resistance and corrosion resistance |
CN103429773A (en) * | 2011-11-28 | 2013-12-04 | 福田金属箔粉工业株式会社 | Ni-fe-cr-based alloy and engine valve coated with same |
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2017
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CN1038609A (en) * | 1989-05-12 | 1990-01-10 | 冶金工业部钢铁研究总院 | Alloy for surfacing |
JPH0584592A (en) * | 1991-09-27 | 1993-04-06 | Toyota Motor Corp | Cobalt-based filling alloy excellent in wear resistance and opponent attackability |
JPH09206985A (en) * | 1996-01-29 | 1997-08-12 | Mitsubishi Materials Corp | Engine valve excellent in high temp. wear resistance |
CN1497050A (en) * | 2002-09-27 | 2004-05-19 | ŵ��Ƥ����ڿع�����˾ | Cobalt-base alloy for coating element corroded by fluid |
KR20110096362A (en) * | 2010-02-22 | 2011-08-30 | 금용기계 주식회사 | High heat-resistance exhaust valve spindle of marine engine having excellent wear resistance and corrosion resistance |
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Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN107322185A (en) * | 2017-08-19 | 2017-11-07 | 安徽鼎恒再制造产业技术研究院有限公司 | Gate valve built-up welding continuous casting casting rod and its welding procedure |
CN107322186A (en) * | 2017-08-26 | 2017-11-07 | 安徽鼎恒再制造产业技术研究院有限公司 | Steel rolling guide roller surfacing cobalt-based alloy powder and its welding procedure |
CN107350662A (en) * | 2017-08-26 | 2017-11-17 | 安徽鼎恒再制造产业技术研究院有限公司 | Valve repair iron-base self-fluxing alloy powder and its welding procedure |
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Application publication date: 20170718 |