CN1978682A - High-strength high-elasticity modulus titanium alloy suitable for preparing foil material - Google Patents
High-strength high-elasticity modulus titanium alloy suitable for preparing foil material Download PDFInfo
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- CN1978682A CN1978682A CN 200510127749 CN200510127749A CN1978682A CN 1978682 A CN1978682 A CN 1978682A CN 200510127749 CN200510127749 CN 200510127749 CN 200510127749 A CN200510127749 A CN 200510127749A CN 1978682 A CN1978682 A CN 1978682A
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Abstract
The invention relates to high intensity high elastic modulus titanium alloy which suits for foil making and is alpha + beta two phase one. Its components are as follows: 4.5-9.0wt% aluminum, 0.2-1.5wt% boron, and 0.5-5wt% beta stable element. Its features are that the beta phase accounts for 10-20vol%; the TiB phase is 4-10vol%; the rest is alpha phase. The titanium alloy foil has high intensity, and high elastic modulus which is isotropy.
Description
Technical field
The present invention relates to a kind of titanium alloy, particularly a kind of titanium alloy that is suitable for preparing the high-strength high-elasticity modulus of foil.
Background technology
When the recoverable deformation of metallic substance satisfied hooke's law fully, the ratio of its stress and strain was Young's modulus.Young's modulus is the physical parameter that characterizes solid interatomic bond intensity in essence, and atomic radius and ionic radius are more little, the material that valence is high more, and its Young's modulus is just big more.For the material that composition is selected, Young's modulus is insensitive to organizing.
Because titanium alloy has good specific tenacity and erosion resistance, therefore, it has been widely used in such as fields such as aviation, military affairs, space, deep-sea detecting and chemical plant.The Young's modulus of titanium alloy has only half of ferrous materials approximately, generally between 110～125GPa.
The Young's modulus of alpha titanium alloy is higher than the Young's modulus of beta titanium alloy.The Young's modulus of commercial alpha titanium alloy is about 120GPa, and the Young's modulus of commercial beta-titanium alloy is about 110GPa.Except that pure titanium, the process plastic of alpha titanium alloy is poor than beta titanium alloy, and the deflection in a cold rolling cycle has only 8%.
Beta stable element is not obvious to the raising of β phase Young's modulus.And α phase stable element aluminium (Al) commonly used is the α phase stable element that the most generally uses in the titanium alloy, and it can significantly increase the Young's modulus of α phase.Do not forming α
2(weight percent of aluminium will form ordered phase (TiAl greater than 8% in the scope of phase
3) be α
2Phase), the Al of every increase by 1 weight %, the Young's modulus of α phase increases 1.4GPa.
Boron (B) is though element is a α phase stable element, but it α mutually with the solubleness all very little (less than 0.2 atom %) of β in mutually, it exists with the form of TiB phase second phase in titanium alloy, its Young's modulus is up to 355GPa, and there is the Young's modulus that can improve titanium alloy in the titanium alloy significantly in it.In pure titanium, when the volume fraction of TiB phase increased to 15% by 0%, Young's modulus increased to 139Gpa by 110GPa.In Ti-6Al-4V (weight percent) alloy (a kind of multiduty alpha+beta alloy), when the volume fraction of TiB phase increased to 10% by 0%, Young's modulus increased to 140GPa by 116GPa.TiB exists with the form of the second phase particle in titanium alloy, and the time spent of doing that is subjected to external stress, it was indeformable substantially, and the compatibility of deformation ability between matrix.When the existence of TiB phase improves the titanium alloy elastic modulus significantly, the processing characteristics of titanium alloy, plasticity index are worsened.
Summary of the invention
The purpose of this invention is to provide and a kind ofly have high-strength high-elasticity modulus and don't make the titanium alloy processing characteristics and the titanium alloy that is suitable for preparing foil that plasticity index worsens.
For achieving the above object, the present invention takes following technical scheme:
A kind of titanium alloy that is suitable for preparing the high-strength high-elasticity modulus of foil, it is the alpha+beta diphasic titanium alloy, in the time will all counting 100 weight %, contain the main ingredient titanium, the aluminium of 4.5～9.0 weight %, 0.2 the boron of～1.5 weight %, 0.5 the beta stable element of～5 weight % is characterized in that, described titanium alloy contains the β phase of 10～20 volume %, the TiB phase of 4～10 volume %, surplus is the α phase.
A kind of optimal technical scheme is characterized in that, described beta stable element is one or more the mixing of arbitrary proportion in molybdenum, niobium, vanadium, chromium, the iron; When being the mixing of arbitrary proportion of multiple beta stable element, wherein the content of each beta stable element is not less than 0.5 weight %.
A kind of optimal technical scheme is characterized in that, also contains the neutral element of 0～3 weight % in the titanium alloy of the described high-strength high-elasticity modulus that is suitable for preparing foil.
A kind of optimal technical scheme is characterized in that, described neutral element is tin, zirconium, hafnium.
A kind of optimal technical scheme is characterized in that, also contains hydrocarbon oxygen nitrogen interstitial element in the titanium alloy of the described high-strength high-elasticity modulus that is suitable for preparing foil.
A kind of optimal technical scheme is characterized in that, the content of described oxygen is 0.05～0.25 weight %.
The diphasic titanium alloy control routinely of the amount of other interstitial element.
The titanium alloy that is suitable for preparing the high-strength high-elasticity modulus of foil of the present invention can utilize multiple melting method meltings such as vacuum consumable smelting, skull melting, beam-plasma melting, electron beam melting, shower furnace melting with commercially available pure metal or master alloy, also can adopt the combination melting of these melting method.Described pure metal comprises titanium, zirconium, aluminium, iron, chromium, vanadium and hafnium; Described master alloy comprises aluminium molybdenum alloy, aluminum-vanadium alloy and Ti-B alloy.
Beneficial effect
1) its tensile strength of titanium alloy of the present invention Rm＞1000MPa, modulus in tension E 〉=130GPa, unit elongation＞7%.
2) alloy of the present invention can be accomplished TiB phase an amount of, that self have high elastic coefficient, has increased the Young's modulus of alloy, does not significantly worsen the plasticity index and the processing characteristics of alloy simultaneously.
3) alloy of the present invention have enough volumes per-cent (70～80%) and by alloying element strengthen simultaneously again can texture strengthening the α phase.
4) alloy of the present invention has certain volume (10～20 volume %) and is had the β phase of certain Young's modulus again by the alloying element reinforcement, ensures the process plastic of alloy.
Embodiment
Embodiment 1
Titanium sponge, zirconium sponge, fine aluminium, pure hafnium, aluminium vanadium master alloy, aluminium molybdenum master alloy, aluminium niobium master alloy and titanium boron master alloy are pressed composition Ti-4.5Al-3Zr-0.5Hf-4Mo-1V-1Nb-1.2B-0.06O batching compacting electrode respectively, adopt skull melting and consumable electrode vacuum furnace melting, be smelted into ingot casting twice.Ingot casting is through hot cogging and slab rolling, and being prepared into thickness is 1.2 millimeters slabs, and slab is made 0.3 millimeter foil through the cold rolling and middle vacuum annealing that circulates.Foil is prepared into the standard tensile sample by standard GB/T228-2000 after adopting 1000 ℃/1h/FC vacuum annealing to handle, and carries out Mechanics Performance Testing on the AG50KNE universal testing machine of Tianjin, island, the tensile strength Rm of gained, unit elongation A
5E sees Table 1 with modulus in tension.Record with the quantitative metallography method, β accounts for 15% of cumulative volume mutually in the microstructure; The TiB phase of 6 volume %.
Embodiment 2
Titanium sponge, zirconium sponge, fine aluminium, pure iron, pure chromium, aluminium molybdenum master alloy, aluminium niobium master alloy and titanium boron master alloy are pressed composition Ti-6Al-2Mo-2Cr-2Zr-0.5Fe-0.6B-0.22O batching compacting electrode respectively, adopt consumable electrode vacuum furnace to be smelted into ingot casting twice.Ingot casting is through hot cogging and slab rolling, and being prepared into thickness is 1.2 millimeters slabs, and slab is made 0.3 millimeter foil through the cold rolling and middle vacuum annealing that circulates.Foil is prepared into the standard tensile sample by standard GB/T228-2000 after adopting 1000 ℃/1h/FC vacuum annealing to handle, and carries out Mechanics Performance Testing on the AG50KNE universal testing machine of Tianjin, island, the tensile strength Rm of gained, unit elongation A
5E sees Table 1 with modulus in tension.Record with the quantitative metallography method, β accounts for 19% of cumulative volume mutually in the microstructure; The TiB phase of 4 volume %.
Embodiment 3
Titanium sponge, fine aluminium, pure chromium, aluminium vanadium master alloy, aluminium molybdenum master alloy and titanium boron master alloy are pressed composition Ti-8Al-2Mo-2V-1Cr-0.7B-0.12O batching compacting electrode respectively, adopt plasma melting and vacuum consumable smelting, be smelted into ingot casting twice.Ingot casting is through hot cogging and slab rolling, and being prepared into thickness is 1.2 millimeters slabs, and slab is made 0.3 millimeter foil through the cold rolling and middle vacuum annealing that circulates.Foil is prepared into the standard tensile sample by standard GB/T228-2000 after adopting 1000 ℃/1h/FC vacuum annealing to handle, and carries out Mechanics Performance Testing on the AG50KNE universal testing machine of Tianjin, island, the tensile strength Rm of gained, unit elongation A
5E sees Table 1 with modulus in tension.Record with the quantitative metallography method, β accounts for 11% of cumulative volume mutually in the microstructure; The TiB phase of 5 volume %.
Embodiment 4
Titanium sponge, zirconium sponge, fine aluminium, pure iron, pure chromium, titanium tin master alloy, aluminium molybdenum master alloy and titanium boron master alloy are pressed composition Ti-6Al-1Sn-2Zr-2Mo-2Cr-0.5Fe-0.3B-0.10O batching respectively, adopt the shower furnace melting, be smelted into ingot casting.Ingot casting is through hot cogging and slab rolling, and being prepared into thickness is 1.2 millimeters slabs, and slab is made 0.3 millimeter foil through the cold rolling and middle vacuum annealing that circulates.Foil is prepared into the standard tensile sample by standard GB/T228-2000 after adopting 1000 ℃/1h/FC vacuum annealing to handle, and carries out Mechanics Performance Testing on the AG50KNE universal testing machine of Tianjin, island, the tensile strength Rm of gained, unit elongation A
5E sees Table 1 with modulus in tension.Record with the quantitative metallography method, β accounts for 15% of cumulative volume mutually in the microstructure; The TiB phase of 3 volume %.
The tensile property of table 1 embodiment interalloy
| Alloy | Rm(MPa) | A 5(％) | E(GPa) |
| Ti-4.5Al-3Zr-0.5Hf-4Mo-1V-1Nb-1.2B-0.06O | 1180 | 7.5 | 136 |
| Ti-6Al-2Mo-2Cr-2Zr-0.5Fe-0.6B-0.22O | 1150 | 9 | 138 |
| Ti-8Al-2Mo-2V-1Cr-0.7B-0.12O | 1180 | 7.5 | 136 |
| Ti-6Al-1Sn-2Zr-2Mo-2Cr-0.5Fe-0.3B-0.10O | 1050 | 10 | 132 |
Can its tensile strength Rm＞1000MPa from last table, modulus in tension E 〉=130GPa, unit elongation＞7%.
Claims (6)
1, a kind of titanium alloy that is suitable for preparing the high-strength high-elasticity modulus of foil, it is the alpha+beta diphasic titanium alloy, in the time will all counting 100 weight %, contain the main ingredient titanium, the aluminium of 4.5～9.0 weight %, 0.2 the boron of～1.5 weight %, 0.5 the beta stable element of～5 weight % is characterized in that, described titanium alloy contains the β phase of 10～20 volume %, the TiB phase that also contains 4～10 volume %, surplus is the α phase.
2, the titanium alloy that is suitable for preparing the high-strength high-elasticity modulus of foil according to claim 1 is characterized in that, described beta stable element is one or more the mixing of arbitrary proportion in molybdenum, niobium, vanadium, chromium, the iron; When being the mixing of arbitrary proportion of multiple beta stable element, wherein the content of each beta stable element is not less than 0.5 weight %.
3, the titanium alloy that is suitable for preparing the high-strength high-elasticity modulus of foil according to claim 1 is characterized in that, also contains the neutral element of 0～3 weight % in the titanium alloy of the described high-strength high-elasticity modulus that is suitable for preparing foil.
4, the titanium alloy that is suitable for preparing the high-strength high-elasticity modulus of foil according to claim 1 is characterized in that described neutral element is tin, zirconium, hafnium.
5, the titanium alloy that is suitable for preparing the high-strength high-elasticity modulus of foil according to claim 1 is characterized in that, also contains interstitial element oxygen in the titanium alloy of the described high-strength high-elasticity modulus that is suitable for preparing foil.
6, the titanium alloy that is suitable for preparing the high-strength high-elasticity modulus of foil according to claim 5 is characterized in that the content of described oxygen is 0.05～0.25 weight %.
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| Application Number | Priority Date | Filing Date | Title |
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| CNB2005101277493A CN100415913C (en) | 2005-12-06 | 2005-12-06 | High-strength high-elasticity modulus titanium alloy suitable for preparing foil material |
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| CNB2005101277493A CN100415913C (en) | 2005-12-06 | 2005-12-06 | High-strength high-elasticity modulus titanium alloy suitable for preparing foil material |
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| CN1978682A true CN1978682A (en) | 2007-06-13 |
| CN100415913C CN100415913C (en) | 2008-09-03 |
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Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105400993A (en) * | 2015-12-22 | 2016-03-16 | 北京有色金属研究总院 | High-speed-impact-resistant and low-cost titanium alloy |
| CN108929962A (en) * | 2018-08-10 | 2018-12-04 | 宝鸡市博信金属材料有限公司 | The low modulus high-precision Ultra-fine Grained foil preparation method of new type beta type titanium alloy |
| CN112695262A (en) * | 2020-12-11 | 2021-04-23 | 西安理工大学 | Titanium alloy-based composite material with micro-structure and preparation method thereof |
-
2005
- 2005-12-06 CN CNB2005101277493A patent/CN100415913C/en active Active
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105400993A (en) * | 2015-12-22 | 2016-03-16 | 北京有色金属研究总院 | High-speed-impact-resistant and low-cost titanium alloy |
| CN105400993B (en) * | 2015-12-22 | 2017-08-25 | 北京有色金属研究总院 | A kind of low-cost titanium alloy of resistance to high speed impact |
| CN108929962A (en) * | 2018-08-10 | 2018-12-04 | 宝鸡市博信金属材料有限公司 | The low modulus high-precision Ultra-fine Grained foil preparation method of new type beta type titanium alloy |
| CN112695262A (en) * | 2020-12-11 | 2021-04-23 | 西安理工大学 | Titanium alloy-based composite material with micro-structure and preparation method thereof |
| CN112695262B (en) * | 2020-12-11 | 2021-10-22 | 西安理工大学 | Titanium alloy-based composite material with micro-structure and preparation method thereof |
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| Publication number | Publication date |
|---|---|
| CN100415913C (en) | 2008-09-03 |
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Effective date of registration: 20190626 Address after: 101407 No. 11 Xingke East Street, Yanqi Economic Development Zone, Huairou District, Beijing Patentee after: Research Institute of engineering and Technology Co., Ltd. Address before: 100088, 2, Xinjie street, Beijing Patentee before: General Research Institute for Nonferrous Metals |