CN101545029B - Method for improving corrosion performance of bulk amorphous alloy through oxidizing annealing in air atmosphere - Google Patents

Method for improving corrosion performance of bulk amorphous alloy through oxidizing annealing in air atmosphere Download PDF

Info

Publication number
CN101545029B
CN101545029B CN2009100979764A CN200910097976A CN101545029B CN 101545029 B CN101545029 B CN 101545029B CN 2009100979764 A CN2009100979764 A CN 2009100979764A CN 200910097976 A CN200910097976 A CN 200910097976A CN 101545029 B CN101545029 B CN 101545029B
Authority
CN
China
Prior art keywords
amorphous alloy
bulk amorphous
air atmosphere
block amorphous
alloy
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.)
Expired - Fee Related
Application number
CN2009100979764A
Other languages
Chinese (zh)
Other versions
CN101545029A (en
Inventor
蒋建中
聂西鹏
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.)
Zhejiang University ZJU
Original Assignee
Zhejiang University ZJU
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 Zhejiang University ZJU filed Critical Zhejiang University ZJU
Priority to CN2009100979764A priority Critical patent/CN101545029B/en
Publication of CN101545029A publication Critical patent/CN101545029A/en
Application granted granted Critical
Publication of CN101545029B publication Critical patent/CN101545029B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

Abstract

The invention discloses a method for improving the corrosion performance of bulk amorphous alloy through oxidizing annealing in an air atmosphere. The method comprises the following steps: firstly, after polishing the surface of a bulk amorphous alloy, washing the surface of the bulk amorphous alloy with alcohol; secondly, placing the bulk amorphous alloy in a muffle furnace to heat the bulk amorphous alloy to between 286 and 336 DEG C at a speed of 10 DEG C/min; and thirdly, keeping the temperature constant for 5 to 10 hours to form a metallic oxide ceramic layer with high corrosion resistance on the surface of the bulk amorphous alloy. Compared with other common methods for improving the corrosion resistance of the bulk amorphous alloy, the technology has the advantages of greatly improving the corrosion resistance of the bulk amorphous alloy without influencing the glass forming ability of the alloy, along with simplicity, easy implementation and low cost. The process avoids changes in the original dimension and shape of a workpiece, ensures an excellent bonding force between a formed oxide layer and a substrate, and is applicable to the final processing of parts and products.

Description

The air atmosphere oxidizing annealing improves the method for block amorphous alloy corrosive nature
Technical field
The present invention relates to the surface anticorrosion technology of amorphous alloy, relate in particular to the method that a kind of air atmosphere oxidizing annealing improves the block amorphous alloy corrosive nature.
Background technology
The eighties of last century the eighties, the Inoue study group of the Turnbull of the U.S. and northeastern Japan university has developed separately and has had good glass forming ability, critical size reaches several millimeters multicomponent alloy system, thereby has opened the flourish prelude of block amorphous alloy research.To having become one of most active subject of metallic substance research field as block amorphous alloy research.Since non-crystaline amorphous metal structurally singularity thereby make especially mechanical property of its physics, chemistry, magnetics with a series of excellences, as high strength, low modulus, high compression plasticity or the like.Non-crystaline amorphous metal has been used as sports equipment, high-performance spring and other miniature instruments etc. and has obtained application at present.
Recently, the Zr base noncrystal alloy that has the good mechanical performance and have a big glass forming ability is developed, and has represented extraordinary application prospect.But before using, its erosion resistance must be considered.The Zr base block amorphous alloy has good anti-corrosion in pure acid and soda ash solution, but erosion resistance is relatively poor in the aqueous solution of chloride ion-containing, and this has limited the development of Zr base noncrystal alloy in application facet to a certain extent.The method of traditional raising non-crystaline amorphous metal erosion resistance mainly contains microalloying method and surface-modification method such as ion implantation.But microalloying method usually can reduce glass forming ability, and the restriction of alloy element will be subjected to alloying rules such as thermodynamics balances each other, solid solubility, and the ion implantation cost is higher, is difficult to large-scale application.Therefore develop a kind of simple and easy to doly, neither reduce the method that glass forming ability can significantly improve block amorphous alloy erosion resistance in the aqueous solution again, be to the research of block amorphous alloy or use important meaning is all arranged.
Summary of the invention
At the deficiency that exists in the background technology, the purpose of this invention is to provide the method that a kind of air atmosphere oxidizing annealing improves the block amorphous alloy corrosive nature.Make the non-crystaline amorphous metal surface generate the anti-corrosion metal oxide ceramic layer of one deck by oxidizing annealing, greatly improve the corrosion resistance nature of non-crystaline amorphous metal in the aqueous solution.
The technical solution adopted for the present invention to solve the technical problems is as follows:
After the block amorphous alloy surface finish, use alcohol wash, put into retort furnace then and be warming up to 286~336 ℃, be incubated 5~10 hours then with 10 ℃/minute speed, block amorphous alloy is taken out, generate the surface oxide layer of strong corrosion resistant on the block amorphous alloy surface.
The block amorphous alloy composition that is adopted is Zr 64.13Cu 15.75Ni 10.12Al 10Or Zr 46Cu 37.6Ag 8.4Al 8
Used Zr 64.13Cu 15.75Ni 10.12Al 10The diameter of block amorphous alloy is the 1-5 millimeter; Used Zr 46Cu 37.6Ag 8.4Al 8The diameter of block amorphous alloy is the 1-20 millimeter.
The beneficial effect that the present invention has is:
1) improved the erosion resistance of block amorphous alloy in the aqueous solution especially chloride ion-containing aqueous solution greatly;
2) do not influence the glass forming ability of former alloy;
3) zone of oxidation and matrix bond closely do not have tangible separation surface;
4) annealing temperature is lower, helps saving cost;
5) adopt air atmosphere annealing, method is simple, and mechanical deformation does not generally take place processed parts, thereby very be suitable for the last processing of part and product.
Description of drawings
Fig. 1 is Zr 64.13Cu 15.75Ni 10.12Al 10Before the non-crystaline amorphous metal annealing, annealing back and the worn XRD figure of falling behind the surface oxide layer;
Fig. 2 is the resulting Zr that reaches before anneal after air atmosphere annealing 64.13Cu 15.75Ni 10.12Al 10Sample is at 0.5N NaCl and 1N H 2SO 4Corrosion polarization curve in the solution.
Fig. 3 is Zr 46Cu 37.6Ag 8.4Al 8Before the non-crystaline amorphous metal annealing, annealing back and the worn XRD figure of falling behind the surface oxide layer;
Fig. 4 is the resulting Zr that reaches before anneal after air atmosphere annealing 46Cu 37.6Ag 8.4Al 8Sample is at 0.5N NaCl and 1N H 2SO 4Corrosion polarization curve in the+0.01N NaCl solution.
Embodiment
Embodiment 1:
This embodiment adopts annealed method under the air atmosphere, makes Zr 64.13Cu 15.75Ni 10.12Al 10Non-crystaline amorphous metal surface generate one deck densification with ZrO 2And Al 2O 3Oxide ceramic layer for main component.
Step 1: with purity is 99.8% Zr, 99.9% Cu, and 99.8% Ni and 99.99% Al (being mass percent) press Zr 64.13Cu 15.75Ni 10.12Al 10Proportioning is arc melting in the argon atmospher of titanium absorption, obtains the alloy spindle that mixes.
Step 2: melting on the water cooled copper mould of spindle in the smelting furnace of argon shield of step 1 acquisition.Utilize pressure difference will obtain alloy liquid then and inject the water cooled copper mould of internal diameter, thereby make the block amorphous alloy that diameter is 3mm for 3mm.
Step 3: with of the diamond sand paper polishing of block amorphous alloy sample, be polished to minute surface then, use alcohol wash, in air, expose more than 24 hours with continuous order number.
Step 4: step 3 gained sample is put into retort furnace, be warming up to 320 ℃, be incubated after 5 to 10 hours and take out, at room temperature naturally cooling with 10 ℃/minute speed.
Step 5: characterize the structure that this block amorphous alloy is handled front and back with the x ray diffraction method, Fig. 1 is its x x ray diffration pattern x.
Step 6: characterize Zr with electrochemical method 64.13Cu 15.75Ni 10.12Al 10Block amorphous alloy anneal front and back are at NaCl and H 2SO 4Corrosion behavior in the solution, Fig. 2 (a) be preceding and annealing back Zr for annealing 64.13Cu 15.75Ni 10.12Al 10The electrokinetic potential polarization curve of alloy sample in 0.5N NaCl solution; Fig. 2 (b) reaches the Zr after the annealing for annealing is preceding 64.13Cu 15.75Ni 10.12Al 10Alloy sample is at 1N H 2SO 4Electrokinetic potential polarization curve in the solution.
Embodiment 2:
This embodiment adopts annealed method under the air atmosphere, makes Zr 46Cu 37.6Ag 8.4Al 8Non-crystaline amorphous metal surface generate one deck densification with ZrO 2Oxide ceramic layer for main component.
Step 1: with purity is 99.8% Zr, 99.9% Cu, and 99.9% Ag and 99.99% Al (being mass percent) press Zr 46Cu 37.6Ag 8.4Al 8Proportioning is arc melting in the argon atmospher of titanium absorption, obtains the alloy spindle that mixes.
Step 2: melting on the water cooled copper mould of spindle in the smelting furnace of argon shield of step 1 acquisition.Utilize pressure difference will obtain alloy liquid then and inject the water cooled copper mould of internal diameter, thereby make the block amorphous alloy that diameter is 5mm for 5mm.
Step 3: with of the diamond sand paper polishing of block amorphous alloy sample, be polished to minute surface then, use alcohol wash, in air, expose more than 24 hours with continuous order number.
Step 4: step 3 gained sample is put into retort furnace, be warming up to 286 or 336 ℃, be incubated after 5 hours and take out, at room temperature naturally cooling with 10 ℃/minute speed.
Step 5: characterize the structure that this block amorphous alloy is handled front and back with the x ray diffraction method, Fig. 3 is its x x ray diffration pattern x.
Step 6: characterize Zr with electrochemical method 46Cu 37.6Ag 8.4Al 8Block amorphous alloy anneal front and back are at NaCl and H 2SO 4Corrosion behavior in the+NaCl solution, Fig. 4 (a) be preceding and annealing back Zr for annealing 46Cu 37.6Ag 8.4Al 8The electrokinetic potential polarization curve of alloy sample in 0.5N NaCl solution; Fig. 4 (b) reaches the Zr after the annealing for annealing is preceding 46Cu 37.6Ag 8.4Al 8Alloy sample is at 1N H 2SO 4Electrokinetic potential polarization curve in the+0.01N NaCl solution.

Claims (2)

1. an air atmosphere oxidizing annealing improves the method for block amorphous alloy corrosive nature, it is characterized in that: after the block amorphous alloy surface finish, use alcohol wash, put into retort furnace then and be warming up to 286~336 ℃ with 10 ℃/minute speed, be incubated 5~10 hours then, block amorphous alloy is taken out, generate the surface oxide layer of strong corrosion resistant on the block amorphous alloy surface;
The block amorphous alloy composition that is adopted is Zr 64.13Cu 15.75Ni 10.12Al 10Or Zr 46Cu 37.6Ag 8.4Al 8
Adopt annealed method under the air atmosphere, make Zr 64.13Cu 15.75Ni 10.12Al 10Non-crystaline amorphous metal surface generate one deck densification with ZrO 2And Al 2O 3Oxide ceramic layer for main component;
Adopt annealed method under the air atmosphere, make Zr 46Cu 37.6Ag 8.4Al 8Non-crystaline amorphous metal surface generate one deck densification with ZrO 2Oxide ceramic layer for main component.
2. a kind of air atmosphere oxidizing annealing according to claim 1 improves the method for block amorphous alloy corrosive nature, it is characterized in that: used Zr 64.13Cu 15.75Ni 10.12Al 10The diameter of block amorphous alloy is the 1-5 millimeter; Used Zr 46Cu 37.6Ag 8.4Al 8The diameter of block amorphous alloy is the 1-20 millimeter.
CN2009100979764A 2009-04-27 2009-04-27 Method for improving corrosion performance of bulk amorphous alloy through oxidizing annealing in air atmosphere Expired - Fee Related CN101545029B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN2009100979764A CN101545029B (en) 2009-04-27 2009-04-27 Method for improving corrosion performance of bulk amorphous alloy through oxidizing annealing in air atmosphere

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN2009100979764A CN101545029B (en) 2009-04-27 2009-04-27 Method for improving corrosion performance of bulk amorphous alloy through oxidizing annealing in air atmosphere

Publications (2)

Publication Number Publication Date
CN101545029A CN101545029A (en) 2009-09-30
CN101545029B true CN101545029B (en) 2011-01-05

Family

ID=41192405

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009100979764A Expired - Fee Related CN101545029B (en) 2009-04-27 2009-04-27 Method for improving corrosion performance of bulk amorphous alloy through oxidizing annealing in air atmosphere

Country Status (1)

Country Link
CN (1) CN101545029B (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN108387423A (en) * 2018-02-23 2018-08-10 深圳顺络电子股份有限公司 A method of improving ltcc substrate salt fog reliability
CN111705204A (en) * 2020-07-30 2020-09-25 常熟市市南模具有限责任公司 Oxidation heat treatment process for glass mold

Also Published As

Publication number Publication date
CN101545029A (en) 2009-09-30

Similar Documents

Publication Publication Date Title
CN102061406B (en) Novel high-elasticity Cu-Ni-Mn alloy and preparation method thereof
CN106191525B (en) A kind of high strength erosion resistant titanium alloy and preparation method
CN108456799B (en) A kind of high-performance copper ferroalloy materials and its electroslag remelting preparation method
CN101899632B (en) Production method of 3003 aluminum alloy deep-drawing wafer
CN109266901B (en) Preparation method of Cu15Ni8Sn high-strength wear-resistant alloy rod/wire
CN112391587B (en) Preparation method and application of amorphous alloy material toughened in cryogenic cycle combined pre-deformation mode
CN107805741A (en) A kind of preparation method of ti-ni shape memory alloy thin plate
CN108149062A (en) A kind of strong high conductive copper alloy of superelevation and preparation method thereof
CN1818109A (en) Copper alloy materials with high-strength and conducting performances and production thereof
CN104388859A (en) Method for simultaneously improving strength and plasticity of copper aluminum alloy
CN109290371B (en) Cold rolling manufacturing method of copper-aluminum composite plate strip
CN107931354A (en) A kind of short flow process of high-ductility low yield strength titanium plate
CN108977693A (en) A kind of recrystallization high-strength titanium alloy and preparation method thereof
CN111304566B (en) Heat treatment method of hard GH5605 superalloy cold-rolled strip
CN109487116A (en) High-strength CTB alloy band and preparation method suitable for electrically conductive elastic component
CN104451484A (en) Thermo-mechanical treatment strengthening technology of magnesium alloy sheet
CN101545029B (en) Method for improving corrosion performance of bulk amorphous alloy through oxidizing annealing in air atmosphere
CN102424927A (en) Magnesium-aluminum alloy and preparation method thereof
CN109504865A (en) It is applicable in the high-strength CTB alloy shaped silk and preparation method of electrically conductive elastic component
CN101307429A (en) Process for preparing high-purity metallic nickel target of superfine crystal particle
CN109732087B (en) Preparation method of powder metallurgy Ti-Ta binary metal-based layered composite material
CN109112355B (en) A kind of nearly α phase high-strength corrosion-resistant erosion titanium alloy and preparation method thereof
CN115449692B (en) High-damping high-entropy steel plate with TWIP effect and preparation method thereof
WO2023036206A9 (en) Preparation method for titanium metal bipolar plate substrate of hydrogen fuel cell
CN103421980A (en) High strength elastic brass 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
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20110105

Termination date: 20110427