CN104046845A - Titanium alloy for casting - Google Patents
Titanium alloy for casting Download PDFInfo
- Publication number
- CN104046845A CN104046845A CN201410294938.9A CN201410294938A CN104046845A CN 104046845 A CN104046845 A CN 104046845A CN 201410294938 A CN201410294938 A CN 201410294938A CN 104046845 A CN104046845 A CN 104046845A
- Authority
- CN
- China
- Prior art keywords
- accounts
- casting
- titanium
- titanium alloy
- niobium
- 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
Links
- 229910001069 Ti alloy Inorganic materials 0.000 title claims abstract description 28
- 238000005266 casting Methods 0.000 title claims abstract description 27
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 claims abstract description 32
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 claims abstract description 17
- 239000010936 titanium Substances 0.000 claims abstract description 17
- 229910052719 titanium Inorganic materials 0.000 claims abstract description 17
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052782 aluminium Inorganic materials 0.000 claims abstract description 16
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052750 molybdenum Inorganic materials 0.000 claims abstract description 16
- 239000011733 molybdenum Substances 0.000 claims abstract description 16
- 229910052759 nickel Inorganic materials 0.000 claims abstract description 16
- 229910052758 niobium Inorganic materials 0.000 claims abstract description 16
- 239000010955 niobium Substances 0.000 claims abstract description 16
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 claims abstract description 16
- 229910052720 vanadium Inorganic materials 0.000 claims abstract description 16
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 claims abstract description 16
- 239000004411 aluminium Substances 0.000 claims description 14
- 239000000203 mixture Substances 0.000 claims description 10
- 229910052751 metal Inorganic materials 0.000 claims description 5
- 239000004615 ingredient Substances 0.000 claims description 3
- 239000002184 metal Substances 0.000 claims description 3
- 229910045601 alloy Inorganic materials 0.000 abstract description 7
- 239000000956 alloy Substances 0.000 abstract description 7
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 230000004927 fusion Effects 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000000284 resting effect Effects 0.000 description 1
- 239000010935 stainless steel Substances 0.000 description 1
- 229910001220 stainless steel Inorganic materials 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
Landscapes
- Turbine Rotor Nozzle Sealing (AREA)
Abstract
The invention discloses a titanium alloy for casting, which is composed of the following components in percentage by weight: 82.4-87.2% of titanium, 3.6-4.5% of vanadium, 5.6-6.8% of aluminum, 1.3-2.2% of molybdenum, 1.5-2.4% of niobium and 0.8-1.7% of nickel. By adding the vanadium, aluminum, molybdenum, niobium and nickel into the titanium-base alloy, the castability is enhanced, and the alloy has the advantages of excellent strength, excellent fracture toughness, higher product quality and wider application range.
Description
Technical field
The present invention relates to a kind of alloy, be specifically related to a kind of casting titanium alloy.
Background technology
Cast titanium alloy is the titanium alloy for being cast into definite shape foundry goods, and the use temperature of cast titanium alloy is generally 300～400 DEG C at present.General vacuum cooling-shell furnace and the graphite mould fusion casting of adopting produced.Be mainly used in casting the nonrotational property parts such as aero-engine casing, resting support, turning vane, also for rotation parts such as casting impellers, replace stainless steel and be used in chemical field.Along with the constant growth of productivity, existing cast titanium alloy cannot meet the user demand in market gradually.
Summary of the invention
The object of the present invention is to provide a kind ofly improve that castibility, intensity and fracture toughness property are high, the casting titanium alloy of the quality of improving product, quality that use range is wide.
Technical scheme of the present invention is, a kind of casting titanium alloy, described casting is combined by titanium, vanadium, aluminium, molybdenum, niobium and six kinds of metal ingredients of nickel with titanium alloy, described casting is respectively with the shared weight percent of each composition in titanium alloy: described titanium accounts for 82.4%-87.2%, described vanadium accounts for 3.6%-4.5%, and described aluminium accounts for 5.6%-6.8%, and described molybdenum accounts for 1.3%-2.2%, described niobium accounts for 1.5%-2.4%, and described nickel accounts for 0.8%-1.7%.
In a preferred embodiment of the present invention, described casting is specially with the shared weight percent of each composition in titanium alloy: described titanium accounts for 82.4%-87.2%, described vanadium accounts for 3.6%-4.5%, described aluminium accounts for 5.6%-6.8%, described molybdenum accounts for 1.3%-2.2%, described niobium accounts for 1.5%-2.4%, and described nickel accounts for 0.8%-1.7%.
In a preferred embodiment of the present invention, described casting is specially with the shared weight percent of each composition in titanium alloy: described titanium accounts for 82.4%-87.2%, described vanadium accounts for 3.6%-4.5%, described aluminium accounts for 5.6%-6.8%, described molybdenum accounts for 1.3%-2.2%, described niobium accounts for 1.5%-2.4%, and described nickel accounts for 0.8%-1.7%.
Of the present invention is a kind of casting titanium alloy, by add the metallic elements such as vanadium, aluminium, molybdenum, niobium and nickel in the titanium base alloy taking titanium as base, improve castibility, and there is good intensity and fracture toughness property, promoted quality and the use range of product.
Embodiment
Below preferred embodiment of the present invention is described in detail, thereby so that advantages and features of the invention can be easier to be it will be appreciated by those skilled in the art that, protection scope of the present invention is made to more explicit defining.
Of the present invention is a kind of casting titanium alloy, described casting is combined by titanium, vanadium, aluminium, molybdenum, niobium and six kinds of metal ingredients of nickel with titanium alloy, described casting is respectively with the shared weight percent of each composition in titanium alloy: described titanium accounts for 82.4%-87.2%, described vanadium accounts for 3.6%-4.5%, described aluminium accounts for 5.6%-6.8%, described molybdenum accounts for 1.3%-2.2%, and described niobium accounts for 1.5%-2.4%, and described nickel accounts for 0.8%-1.7%.
Further, described casting is specially with the shared weight percent of each composition in titanium alloy: described titanium accounts for 82.4%-87.2%, described vanadium accounts for 3.6%-4.5%, described aluminium accounts for 5.6%-6.8%, described molybdenum accounts for 1.3%-2.2%, described niobium accounts for 1.5%-2.4%, and described nickel accounts for 0.8%-1.7%.
Further, described casting is specially with the shared weight percent of each composition in titanium alloy: described titanium accounts for 82.4%-87.2%, described vanadium accounts for 3.6%-4.5%, described aluminium accounts for 5.6%-6.8%, described molybdenum accounts for 1.3%-2.2%, described niobium accounts for 1.5%-2.4%, and described nickel accounts for 0.8%-1.7%.
In addition, can be by regulating the Different Weight per-cent of each composition in alloy, the alloy property height obtaining is differed.
Of the present invention is a kind of casting titanium alloy, by add the metallic elements such as vanadium, aluminium, molybdenum, niobium and nickel in the titanium base alloy taking titanium as base, improve castibility, and there is good intensity and fracture toughness property, promoted quality and the use range of product.
The foregoing is only the specific embodiment of the present invention; but protection scope of the present invention is not limited to this; any those of ordinary skill in the art are in the disclosed technical scope of the present invention; the variation that can expect without creative work or replacement, within all should being encompassed in protection scope of the present invention.Therefore, protection scope of the present invention should be as the criterion with the protection domain that claims were limited.
Claims (3)
1. a casting titanium alloy, it is characterized in that: described casting titanium alloy is combined by titanium, vanadium, aluminium, molybdenum, niobium and six kinds of metal ingredients of nickel, described casting is respectively with the shared weight percent of each composition in titanium alloy: described titanium accounts for 82.4%-87.2%, described vanadium accounts for 3.6%-4.5%, described aluminium accounts for 5.6%-6.8%, described molybdenum accounts for 1.3%-2.2%, and described niobium accounts for 1.5%-2.4%, and described nickel accounts for 0.8%-1.7%.
2. casting titanium alloy according to claim 1, it is characterized in that: described casting shared weight percent of each composition in titanium alloy is specially: described titanium accounts for 82.4%-87.2%, described vanadium accounts for 3.6%-4.5%, described aluminium accounts for 5.6%-6.8%, described molybdenum accounts for 1.3%-2.2%, described niobium accounts for 1.5%-2.4%, and described nickel accounts for 0.8%-1.7%.
3. casting titanium alloy according to claim 1, it is characterized in that: described casting shared weight percent of each composition in titanium alloy is specially: described titanium accounts for 82.4%-87.2%, described vanadium accounts for 3.6%-4.5%, described aluminium accounts for 5.6%-6.8%, described molybdenum accounts for 1.3%-2.2%, described niobium accounts for 1.5%-2.4%, and described nickel accounts for 0.8%-1.7%.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410294938.9A CN104046845A (en) | 2014-06-27 | 2014-06-27 | Titanium alloy for casting |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410294938.9A CN104046845A (en) | 2014-06-27 | 2014-06-27 | Titanium alloy for casting |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104046845A true CN104046845A (en) | 2014-09-17 |
Family
ID=51500236
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410294938.9A Pending CN104046845A (en) | 2014-06-27 | 2014-06-27 | Titanium alloy for casting |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104046845A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110777283A (en) * | 2019-08-02 | 2020-02-11 | 宁波中星新材料研究院有限公司 | Titanium alloy for arc fuse additive manufacturing and preparation method thereof |
Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10306335A (en) * | 1997-04-30 | 1998-11-17 | Nkk Corp | Alpha plus beta titanium alloy bar and wire rod, and its production |
-
2014
- 2014-06-27 CN CN201410294938.9A patent/CN104046845A/en active Pending
Patent Citations (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH10306335A (en) * | 1997-04-30 | 1998-11-17 | Nkk Corp | Alpha plus beta titanium alloy bar and wire rod, and its production |
Non-Patent Citations (1)
| Title |
|---|
| 国家技术监督局: "铸造钛及钛合金牌号和化学成分", 《中华人民共和国国家标准GB/T 15073-94》, 1 December 1994 (1994-12-01) * |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110777283A (en) * | 2019-08-02 | 2020-02-11 | 宁波中星新材料研究院有限公司 | Titanium alloy for arc fuse additive manufacturing and preparation method thereof |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| MX2022007970A (en) | High strength titanium alloys. | |
| GB2494352B (en) | Grain refiner for magnesium and magnesium alloys and method for producing the same | |
| WO2019209368A3 (en) | Titanium alloy products and methods of making the same | |
| CN104046897A (en) | High-strength special steel alloy | |
| WO2018158509A8 (en) | Alloy for a fibre-forming plate | |
| CN104046845A (en) | Titanium alloy for casting | |
| CN104018042A (en) | Thermally conductive metal material | |
| CN103484719A (en) | Copper-nickel alloy metal pipe | |
| CN103469025A (en) | Aluminum alloy | |
| CN103205606B (en) | A kind of formula of compound wipla metal | |
| CN104046856B (en) | A kind of aluminum bronze magnesium system duralumin | |
| CN104046829A (en) | Gold-base alloy for jewelry | |
| CN107779668A (en) | A kind of titanium alloy die casting | |
| CN104451462B (en) | A kind of high-ductility alloy | |
| CN103555997A (en) | Titanium-magnesium-manganese alloy and preparation method thereof | |
| CN104032218A (en) | Metal alloy easy to passivate | |
| CN105296812A (en) | Anti-corrosion aluminum alloy | |
| CN104404400B (en) | A kind of abrasion-resistant stee | |
| JP6322145B2 (en) | Duplex steel with improved notched impact strength and machinability | |
| CN104046848A (en) | Nickel-base self-fluxing alloy powder | |
| WO2019027347A8 (en) | Corrosion-resistant alloy | |
| CN104046850A (en) | Cobalt-based high temperature alloy | |
| CN104046875A (en) | High-strength wear-resistant alloy | |
| CN104178656A (en) | Cu-Fe composite material | |
| CN104911463A (en) | Cast iron alloy casting |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20140917 |