CN102061420A - Alloy with low specific gravity and preparation method thereof - Google Patents

Alloy with low specific gravity and preparation method thereof Download PDF

Info

Publication number
CN102061420A
CN102061420A CN 201110035425 CN201110035425A CN102061420A CN 102061420 A CN102061420 A CN 102061420A CN 201110035425 CN201110035425 CN 201110035425 CN 201110035425 A CN201110035425 A CN 201110035425A CN 102061420 A CN102061420 A CN 102061420A
Authority
CN
China
Prior art keywords
alloy
percent
preparation
specific gravity
low specific
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.)
Pending
Application number
CN 201110035425
Other languages
Chinese (zh)
Inventor
邵化
彭忠元
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ZHUZHOU CHANGJIANG CARBIDE TOOLS CO Ltd
Original Assignee
ZHUZHOU CHANGJIANG CARBIDE TOOLS CO Ltd
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 ZHUZHOU CHANGJIANG CARBIDE TOOLS CO Ltd filed Critical ZHUZHOU CHANGJIANG CARBIDE TOOLS CO Ltd
Priority to CN 201110035425 priority Critical patent/CN102061420A/en
Publication of CN102061420A publication Critical patent/CN102061420A/en
Pending legal-status Critical Current

Links

Abstract

The invention discloses an alloy with low specific gravity and a preparation method thereof. The alloy with low specific gravity is prepared from the following components in percentage by weight: 8-9 percent of Co, 14.5-15.5 percent of TiC and the balance of WC, has the specific gravity smaller than 12.0g/cm<3>, the HV30 of 1550-1650 and the abrasive resistance test RS value of 50-65. The preparation method comprises the following steps of: selecting raw materials; blending the raw materials; carrying out ball milling; calendaring and sintering, and the preparation method is characterized in that the blending of the raw materials is carried out by firstly adding 30 percent by weight of WC powder with the Fsss granularity of 1.0-1.5 mum, then adding 35.15-40.75 percent of YT zinc melting stock of a less known brand and adding 0.05-0.055 percent of Co powder and 24.00-29.40 percent of composite carbide CK32 according to the weight percentage of all components of the alloy with the low specific gravity, wherein the carbon balance value is (-0.05)-(-0.1) percent in the case of blending calculation. The prepared alloy has low cost and meets the client requirement for the wearing resistance of anti-skid stud products.

Description

The low-gravity Alloy And Preparation Method
Technical field
The present invention relates to a kind of low-gravity alloy and preparation thereof, especially is the low-gravity Alloy And Preparation Method of main raw material with the reworked material.
Background technology
It is raw material (cobalt quality percentage composition is 8%, the surplus wolfram varbide) production that the safety stud product generally adopts conventional Wimet trade mark YG8, proportion 14.5 g/cm 3About, HV 301350~1450, raw materials cost and selling price are basic identical, and no profit can be sayed; Simultaneously, the safety stud product RS value of conventional YG8 trade mark preparation is 70~90, can not satisfy wear resistance RS value that safety stud improves constantly and be 50~65 requirement.
Summary of the invention
The purpose of this invention is to provide a kind of low specific weight hard Alloy And Preparation Method, the cost of alloy of preparation is cheap and satisfy the requirement of client to safety stud product wear resistance.
For achieving the above object, low specific weight hard alloy of the present invention comprises weight percent and is 8~9 %Co, 14.5~15.5% TiC, surplus are WC; Its proportion<12.0g/cm 3, HV 30Be 1550~1650, wearability test RS value 50~65.
Its preparation method, comprise raw-material selection, batching, ball milling, compacting, sintering, it is characterized in that: add earlier weight percent during batching and be 30%, the Fsss granularity is the WC powder of 1.0~1.5 μ m, add YT zinc melt 35.15~40.75% of inferior brand again, and add 0.05~0.055% Co powder, 24.00~29.40% composite carbide CK32 according to each weight percentages of components of described low-gravity alloy; During charge calculation, the carbon balance value is (0.05~-0.1) %.
Because added weight percent in the raw material and be 30%, the Fsss granularity is the WC of 1.0~1.5 μ m, the HV of the alloy of preparing 30Can between 1550~1650, the RS value between 50~60, wear resistance can satisfy the safety stud product requirement fully; Adopting YT class zinc melt of inferior brand is that regenerative raw materials is a main raw material, with low cost, and reduction along with alloy proportion, the grain number that the safety stud product grain number of every kilogram of production of this alloy is produced than the YG8 trade mark increases more than 15%, is that unit is sold and work as product with the grain number, again the product profit that further increases.
Embodiment
Embodiment 1: configuration 1000g raw material, and wherein the Fsss granularity is that the WC powder of 1.3 μ m is 300g, is that weight percent is 30%, selects YT zinc melt of inferior brand 388.5g again for use, wherein TiC 12.06%, Co 8.05%; The composition 8.5%Co of the low-gravity alloy that obtains according to ultimate demand, 15% TiC, surplus are WC again, add the Co of 53.7g and the composite carbide CK32 of 257.8g in raw material; Charge calculation, carbon balance value are-0.05%.Carry out ball milling granulation, compacting, sintering after the batching, wherein ball milling is done medium, ratio of grinding media to material 5:1,48 hours ball milling time with alcohol.Be pressed into SP2 intensity bar sample after the granulation, in hydrogen furnace, 1480 ℃ of sintering temperatures, the hart metal product of acquisition, wherein Co, TiC weight percent are respectively 8.48%, 15.05%, and surplus is WC; This alloy proportion is 11.24g/cm 3, HV 30: 1550, wearability test RS value is 56.
Embodiment 2: configuration 1000g raw material, and wherein the Fsss granularity is that the WC powder of 1.25 μ m is 300g, is that weight percent is 30%, selects YT zinc melt of inferior brand 407.2g again for use, wherein TiC 11.84%, Co 7.17%; The composition 8.0%Co of the low-gravity alloy that obtains according to ultimate demand, 14.5% TiC, surplus are WC again, add the Co of 50.8g and the composite carbide CK32 of 242g in raw material; Charge calculation, carbon balance value are-0.08%.Carry out ball milling granulation, compacting, sintering after the batching, wherein ball milling is done medium, ratio of grinding media to material 5:1,48 hours ball milling time with alcohol.Be pressed into SP2 intensity bar sample after the granulation, in hydrogen furnace, 1480 ℃ of sintering temperatures, the hart metal product of acquisition, wherein Co, TiC weight percent are respectively 8.04%, 14.52%, and surplus is WC; This alloy proportion is 11.26g/cm 3, HV 30: 1580, wearability test RS value is 53.
Embodiment 3: configuration 1000g raw material, and wherein the Fsss granularity is that the WC powder of 1.25 μ m is 300g, is that weight percent is 30%, selects YT zinc melt of inferior brand 351.8g again for use, wherein TiC 11.84%, Co 7.17%; The composition 9.0%Co of the low-gravity alloy that obtains according to ultimate demand, 15.5% TiC, surplus are WC again, add the Co of 54.8g and the composite carbide CK32 of 293.4g in raw material; Charge calculation, carbon balance value are-0.1%.Carry out ball milling granulation, compacting, sintering after the batching, wherein ball milling is done medium, ratio of grinding media to material 5:1,48 hours ball milling time with alcohol.Be pressed into SP2 intensity bar sample after the granulation, in hydrogen furnace, 1480 ℃ of sintering temperatures, the hart metal product of acquisition, wherein Co, TiC weight percent are respectively 8.97%, 15.48%, and surplus is WC; This alloy proportion is 11.18g/cm 3, HV 30: 1600, wearability test RS value is 62.

Claims (2)

1. low specific weight hard alloy, comprising weight percent is the TiC of 8~9%Co, 14.5~15.5 %, surplus is WC; Its proportion<12.0g/cm 3, HV 30Be 1550~1650, wearability test RS value 50~65.
2. the preparation method of low specific weight hard alloy as claimed in claim 1, comprise raw-material selection, batching, ball milling, compacting, sintering, it is characterized in that: add earlier weight percent during batching and be 30%, the Fsss granularity is the WC powder of 1.0~1.5 μ m, add YT zinc melt 35.15~40.75% of inferior brand again, and add 0.05~0.055% Co powder, 24.00~29.40% composite carbide CK32 according to each weight percentages of components of described low-gravity alloy; During charge calculation, the carbon balance value is (0.05~-0.1) %.
CN 201110035425 2011-02-10 2011-02-10 Alloy with low specific gravity and preparation method thereof Pending CN102061420A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 201110035425 CN102061420A (en) 2011-02-10 2011-02-10 Alloy with low specific gravity and preparation method thereof

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 201110035425 CN102061420A (en) 2011-02-10 2011-02-10 Alloy with low specific gravity and preparation method thereof

Publications (1)

Publication Number Publication Date
CN102061420A true CN102061420A (en) 2011-05-18

Family

ID=43996924

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 201110035425 Pending CN102061420A (en) 2011-02-10 2011-02-10 Alloy with low specific gravity and preparation method thereof

Country Status (1)

Country Link
CN (1) CN102061420A (en)

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0971835A (en) * 1995-09-01 1997-03-18 Toshiba Tungaloy Co Ltd High wear resistant and corrosion resistant cemented carbide
US5984996A (en) * 1995-02-15 1999-11-16 The University Of Connecticut Nanostructured metals, metal carbides, and metal alloys
JP2001081526A (en) * 1999-09-13 2001-03-27 Kohan Kogyo Kk Iron-base cemented carbide and its manufacture
CN1410575A (en) * 2002-12-02 2003-04-16 株洲硬质合金集团有限公司 Metal ceramic and its preparation method

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5984996A (en) * 1995-02-15 1999-11-16 The University Of Connecticut Nanostructured metals, metal carbides, and metal alloys
JPH0971835A (en) * 1995-09-01 1997-03-18 Toshiba Tungaloy Co Ltd High wear resistant and corrosion resistant cemented carbide
JP2001081526A (en) * 1999-09-13 2001-03-27 Kohan Kogyo Kk Iron-base cemented carbide and its manufacture
CN1410575A (en) * 2002-12-02 2003-04-16 株洲硬质合金集团有限公司 Metal ceramic and its preparation method

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
《吉林工业大学学报》 19900402 傅敦祺等 钴基硬质合金刀片的成分和质量的判断 80-87 1、2 , 第1期 2 *
《硬质合金》 20080315 张兴华等 再生碳化钨性能及应用 58-62 2 第25卷, 第1期 2 *

Similar Documents

Publication Publication Date Title
CN101121983B (en) Method for preparing coarse grain hard alloy and the coarse grain hard alloy
CN101912888B (en) Manufacturing method of die core of wire-drawing die
CN102140603B (en) Preparation method of hard alloy using nickel-aluminum intermetallic compound Ni3Al as bonding phase
CN102990069B (en) A kind of preparation method utilizing useless tungsten-cobalt alloy to make coarse-grain carbide alloy pick
CN102154582B (en) Preparation method of hard alloy taking nickel-aluminium intermetallic compound Ni3Al as binding phase
CN102676902A (en) Ultra-thick hard alloy, and preparation method and application thereof
CN102187005A (en) Molybdenum-contained alloy powders used to produce sintered hard metals based on tungsten carbide
CN101985717A (en) Method for preparing high-tenacity super-coarse-grained tungsten and cobalt hard alloy
CN102766796B (en) Hard alloy and preparation method thereof
CN103817150A (en) Gradient-structure hard alloy roll collar and manufacturing process thereof
CN103741001A (en) High-hardness and high-strength PY30T hard alloy and preparation method of high-hardness and high-strength PY30T hard alloy product
CN101381834A (en) Double crystal corrosion resistant cemented carbide material and manufacturing method thereof
US20210178476A1 (en) Grade powders and sintered cemented carbide compositions
CN102329975A (en) Super-hard material and preparation method thereof
CN101886229B (en) Ball dedicated for semi-autogenous mill and process method thereof
CN103586457A (en) Powder metallurgy tool and manufacturing method thereof
CN103243252A (en) Binder-phase wolfram-carbide (WC) hard alloy and preparation method thereof
CN102162058B (en) Hard alloy taking nickel-aluminum intermetallic compound Ni3Al as binding phase and preparation method thereof
CN105479039B (en) A kind of abrasion-resistant welding wire
CN102061420A (en) Alloy with low specific gravity and preparation method thereof
CN1420191A (en) Method for mfg. W-Co-Ti hard alloy
CN106756160A (en) A kind of preparation method of cermet material
CN102321837B (en) High-hardness composite material for cutter and preparation method
CN102453873A (en) Titanium target and manufacturing method thereof
CN103695750A (en) Powder metallurgy alloy cutting tool and preparation method thereof

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C02 Deemed withdrawal of patent application after publication (patent law 2001)
WD01 Invention patent application deemed withdrawn after publication

Application publication date: 20110518