CN106906380A - 3C product titanium alloy material - Google Patents
3C product titanium alloy material Download PDFInfo
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- CN106906380A CN106906380A CN201710223880.2A CN201710223880A CN106906380A CN 106906380 A CN106906380 A CN 106906380A CN 201710223880 A CN201710223880 A CN 201710223880A CN 106906380 A CN106906380 A CN 106906380A
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- CN
- China
- Prior art keywords
- titanium alloy
- alloy material
- product
- component
- product titanium
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C14/00—Alloys based on titanium
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Materials For Medical Uses (AREA)
Abstract
3C Product titanium alloy material, it is characterised in that:The material is comprising following each component and its corresponding weight hundred than (wt%):Ti is 90~99, Fe for 0.15~0.75,0 is that >=0.15, C is that≤0.08, N is that≤0.05, H is≤0.015.Among present invention is mainly applied to 3C Product, and >=530MPa is increased to tensile strength scope, offset yield strength increases to >=450MPa, and hardness increases to >=156HB, and elongation increases to the >=beneficial effect such as 16%.
Description
Technical field
The present invention relates to metal material field, more particularly to a kind of titanium alloy material suitable for making 3C Product metal shell
Material.
Background technology
3C Product, also known as information household appliances, generally comprise computer (computer), communication (communication) and disappear
Take electronic product (consumerelectronics) etc..
At present, the material of 3C Product conventional metals shell is mainly stainless steel or aluminum alloy material;Its advantage
It is low cost, it has the disadvantage, and hardness is smaller, quality is relatively low, does not adapt to the high-grade consumption demand of consumers in general.
It is because titanium alloy material has the characteristics such as hardness higher, tensile strength, offset yield strength but relatively costly,
Therefore only it is widely used in the special industries such as medical treatment, aviation, fails to obtain the popularization and application of broad spectrum.Meanwhile, it is existing
The titanium alloy material for having technology to prepare can not be directly applied among 3C Product, therefore how popularization and application titanium alloy material exists
Application in the middle of 3C Product, it has also become a current metal material field technical problem urgently to be resolved hurrily.
The content of the invention
The invention aims to solve titanium alloy material how among 3C Product the technology of more preferable popularization and application is asked
Topic, and then there is provided a kind of 3C Product titanium alloy material.
The present invention is for the solution technical scheme that is used of technical problem:
3C Product titanium alloy material, the material is comprising following each component and its corresponding weight hundred than (wt%):Ti is 90
~99, Fe is that 0.15~0.75, O is that >=0.15, C is that≤0.08, N is that≤0.05, H is≤0.015.
Because the metal shell general thickness of 3C Product is relatively thin, so needing increase tensile strength, offset yield strength, stretching
The minimum of the performance parameters such as rate long, hardness.The present invention is by adjusting the accurate proportioning of each component, then is aided with corresponding technique,
Its tensile strength scope can even be increased to by >=530MPa using existing technique, offset yield strength increases to >=
450MPa, hardness increases to >=156HB, and elongation increases to >=16% etc., therefore expands the application model of titanium alloy material
Enclose, be that the more preferable popularization and application of titanium alloy material is laid a good foundation.
Further, the material includes following each component and its corresponding weight hundred than (wt%):Ti is that 90, Fe is 0.75, C
For 0.04, N is that 0.05, H is 0.015, balance of 0.
Further, the material includes following each component and its corresponding weight hundred than (wt%):Ti is that 99, Fe is 0.15, C
For 0.08, N is that 0.04, H is 0.01, balance of 0.
Further, the material includes following each component and its corresponding weight hundred than (wt%):Ti is that 95, Fe is 0.5, C
For 0.05, N is that 0.05, H is 0.015, balance of 0.
Specific embodiment
The present invention is described in further details below in conjunction with specific embodiment.
3C Product titanium alloy material, its key component is Ti, Fe, O, C, N, H, while the percentage by weight of each component
(wt%) it is:Ti is that 90~99, Fe is that 0.15~0.75, O is that >=0.15, C is that≤0.08, N is that≤0.05, H is≤0.015.
It is of the invention carry out various performance parameters detection under the same conditions with existing titanium alloy material after, be shown by following table:
As seen from the above table, the present invention is by adjusting the accurate proportioning of each component, then is aided with corresponding technique, or even using existing
Its tensile strength scope can be increased to >=530MPa by some technique, and offset yield strength increases to >=450MPa, hardness
>=156HB is increased to, elongation increases to >=16% etc., therefore expands the range of application of titanium alloy material.
Embodiment 1
Weight hundred is taken than (wt%):Ti is that 90, Fe is that 0.75, C is that 0.04, N is that 0.05, H is 0.015, balance of 0, is adopted
Above-mentioned 3C Product titanium alloy material is obtained with existing process.
Embodiment 2
Weight hundred is taken than (wt%):Ti is that 99, Fe is that 0.15, C is that 0.08, N is that 0.04, H is 0.01, balance of 0, is used
Existing process is obtained above-mentioned 3C Product titanium alloy material.
Embodiment 3
Weight hundred is taken than (wt%):Ti is that 95, Fe is that 0.5, C is that 0.05, N is that 0.05, H is 0.015, balance of 0, is used
Existing process is obtained above-mentioned 3C Product titanium alloy material.
Claims (4)
1.3C product titanium alloy materials, it is characterised in that:The material compares comprising following each component and its corresponding weight hundred
(wt%):Ti is 90~99, Fe for 0.15~0.75,0 is that >=0.15, C is that≤0.08, N is that≤0.05, H is≤0.015.
2. 3C Product titanium alloy material as claimed in claim 1, it is characterised in that:The material comprising following each component and its
Corresponding weight hundred is than (wt%):Ti is that 90, Fe is that 0.75, C is that 0.04, N is that 0.05, H is 0.015, balance of 0.
3. 3C Product titanium alloy material as claimed in claim 1, it is characterised in that:The material comprising following each component and its
Corresponding weight hundred is than (wt%):Ti is that 99, Fe is that 0.15, C is that 0.08, N is that 0.04, H is 0.01, balance of 0.
4. 3C Product titanium alloy material as claimed in claim 1, it is characterised in that:The material comprising following each component and its
Corresponding weight hundred is than (wt%):Ti is that 95, Fe is that 0.5, C is that 0.05, N is that 0.05, H is 0.015, balance of 0.
Priority Applications (1)
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CN201710223880.2A CN106906380A (en) | 2017-04-10 | 2017-04-10 | 3C product titanium alloy material |
Applications Claiming Priority (1)
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CN201710223880.2A CN106906380A (en) | 2017-04-10 | 2017-04-10 | 3C product titanium alloy material |
Publications (1)
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CN106906380A true CN106906380A (en) | 2017-06-30 |
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CN201710223880.2A Pending CN106906380A (en) | 2017-04-10 | 2017-04-10 | 3C product titanium alloy material |
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Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3481428B2 (en) * | 1997-08-11 | 2003-12-22 | 新日本製鐵株式会社 | Method for producing Ti-Fe-ON-based high-strength titanium alloy sheet with small in-plane anisotropy |
CN106011714A (en) * | 2016-06-01 | 2016-10-12 | 洛阳双瑞精铸钛业有限公司 | Method for producing thin TA4 titanium material by roll type cold rolling method |
CN106480399A (en) * | 2016-12-13 | 2017-03-08 | 南京工程学院 | A kind of method for preparing gradient nano structure nitration case in titanium alloy surface |
-
2017
- 2017-04-10 CN CN201710223880.2A patent/CN106906380A/en active Pending
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP3481428B2 (en) * | 1997-08-11 | 2003-12-22 | 新日本製鐵株式会社 | Method for producing Ti-Fe-ON-based high-strength titanium alloy sheet with small in-plane anisotropy |
CN106011714A (en) * | 2016-06-01 | 2016-10-12 | 洛阳双瑞精铸钛业有限公司 | Method for producing thin TA4 titanium material by roll type cold rolling method |
CN106480399A (en) * | 2016-12-13 | 2017-03-08 | 南京工程学院 | A kind of method for preparing gradient nano structure nitration case in titanium alloy surface |
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Application publication date: 20170630 |
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