CN101899590A - Titanium-aluminum-iron alloy - Google Patents
Titanium-aluminum-iron alloy Download PDFInfo
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- CN101899590A CN101899590A CN 201010241013 CN201010241013A CN101899590A CN 101899590 A CN101899590 A CN 101899590A CN 201010241013 CN201010241013 CN 201010241013 CN 201010241013 A CN201010241013 A CN 201010241013A CN 101899590 A CN101899590 A CN 101899590A
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Abstract
The invention discloses a titanium-aluminum-iron alloy. The titanium-aluminum-iron alloy is characterized by consisting of the following components in percentage by weight: 91 to 96 percent of Ti, 3 to 6 percent of Al, 0.6 to 2 percent of Fe, 0.1 to 0.3 percent of O, 0.01 to 0.06 percent of N, 0.01 to 0.015 percent of H and 0.01 to 0.05 percent of C. In the invention, because the alloy comprises Al, the thermal processing performance is between that of ASTM pure titanium and that of Ti-6Al-4V, namely the thermal deformation resistance is greater than that of the Gr4 pure titanium and less than that of Ti-6Al-4V and the fatigue strength is higher than that of Ti-6Al-4V. Thus the Ti-Al-Fe alloy has the advantages of superior thermal processing performance to the conventional high-strength titanium alloys, tensile strength of 1,000MPa which is equivalent to that of Ti-6Al-4V, superplasticity, wide temperature range for superplastic deformation and easy molding.
Description
Technical field
The present invention relates to low-cost and high-performance titanium alloy material field, especially make the titanium alloy of automobile component with low-cost and high-performance about a kind of being mainly used in.
Background technology
The metal titanium excellent characteristic mainly is meant high strength, low density, outstanding solidity to corrosion, and the isostructural steel of homophase are compared, and titanium alloy material generally can alleviate component weight about 50%.Document announcement is arranged, if car mass reduces by 10%, fuel efficiency can improve 6%~8%.This shows, follow lightweight and the outstanding advantage of coming is the remarkable reduction of oil consumption, also will reduce the emission of automobile wastes amount, reach the purpose of energy-saving and environmental protection.
When titanium alloy uses as the trolley part material, half that is characterized in that tensile strength and yield strength are big, fatigue strength is big, density is little, Young's modulus is steel approximately, thermal expansivity are low, be approximately stainless steel and aluminium half, non magnetic, thermal conductivity is low, be easy to generate sintering, environmentally safe etc.After automobile industry is with titanium, can greatly alleviate vehicle weight, reduce its fuel consumption, reduce the noise and the vibration of engine, protection environment and reduction noise.Utilize titanium alloy to make auto parts machinery, but not only weight reduction save fuel oil, and power transmission is effective, helps good dynamic performance, operational stability.The reliability height increases the service life.The automobile titanium is a very huge market, and according to design and material behavior, titanium mainly is distributed on engine components and the vehicle chassis component in the application on the automobile.Can make elements such as valve, valve spring, valve spring bearing and connecting rod in engine system with titanium, the improvement of performance shows the minimizing of changeing distance, output rating and interconnecting piece distortion.Titanium purposes beyond the engine: be mainly spring, exhaust system, semiaxis, middle suspension spring, gas barrier with titanium at vehicle chassis component, bent axle and other fastening piece class are to the use of titanium, available titanium is made valve class, coupling shaft, valve spring and its bearing tool in the trolley part, and these all are the key parts on the automobile.Therefore it is extremely urgent to research and develop titanium alloy.
Summary of the invention
At above problem, the object of the present invention is to provide a kind of titanium ferroaluminium, be the β element V that in known alloy, does not use high price, adopt cheap Fe, adapt to the application of low-cost and high-performance Ti-Al-Fe alloy material in temperature changing process.
Technical scheme of the present invention realizes in the following manner: a kind of titanium ferroaluminium, represent with weight percent, it is characterized in that: form: Ti 91-96%, Al 3-6%, Fe 0.6-2%, O 0.1-0.3%, N 0.01-0.06%, H 0.01-0.015%, C0.01-0.05% by following composition.
The present invention, because of containing Al in the alloy ingredient, hot workability is in the middle of pure titanium of ASTM and the Ti-6Al-4V, and the instant heating resistance to deformation is bigger than the pure titanium of Gr4, and littler than Ti-6Al-4V, fatigue strength is higher than Ti-6Al-4V.Therefore the Ti-Al-Fe alloy has than the better hot workability of high strength titanium alloy in the past, and its tensile strength reaches 1000MPa, and is suitable with Ti-6Al-4V, have superly to mould behavior, and the temperature range of superplastic deformation is very wide, is easy to forming process.
Embodiment
Embodiment 1:
A kind of Ti-5Al-1Fe titanium ferroaluminium is represented with weight percent, is made up of following composition: Ti 93.875%, Al 5%, Fe 1%, O 0.2%, N 0.04%, H 0.015%, C 0.05%.
Embodiment 2:
A kind of Ti-3.5Al-1Fe titanium ferroaluminium is represented with weight percent, is made up of following composition: Ti 95.3%, Al 3.5%, Fe 1%, O 0.16%, N 0.02%, H 0.01%, C 0.01%.
Embodiment 3:
A kind of Ti-5.5Al-1Fe titanium ferroaluminium is represented with weight percent, is made up of following composition: Ti 92.65%, Al 5.5%, Fe 1%, O 0.3%, N 0.5%, H 0.013%, C 0.037%.
Test shows: the hot relative reduction in area of Ti-3.5Al-1Fe is suitable with the pure titanium of Gr4; Ti-5Al-1Fe, its tensile strength reaches 1000MPa, and it is suitable with Ti-6Al-4V that intensity exceeds the about 200MPa. of pure titanium material, the Ti-Al-Fe alloy is because of containing Al, hot workability is in the middle of pure titanium of ASTM and the Ti-6Al-4V, and the instant heating resistance to deformation is bigger than the pure titanium of Gr4, and is littler than Ti-6Al-4V.The hot relative reduction in area of Ti-5.5Al-1Fe is than Ti-6Al-4V height, so the Ti-Al-Fe alloy has than the better hot workability of high strength titanium alloy in the past.Fatigue strength is higher than Ti-6Al-4V.Superplasticity; Ti-Al-Fe such as has at the axle microscopic structure, and is the same with general alpha+beta titanium alloys, and the temperature range of superplastic deformation is very wide, is easy to forming process.The present invention is mainly used in the low-cost and high-performance Ti-Al-Fe alloy material of automobile and motorcycle, from the melting of titanium ingot to forging, the processing and the industrialization of rod, silk coiled material.
Performance index are as follows:
Claims (4)
1. a titanium ferroaluminium is represented with weight percent, it is characterized in that: be made up of following composition: Ti 91-96%, Al 3-6%, Fe 0.6-2%, O 0.1-0.3%, N 0.01-0.06%, H 0.01-0.015%, C 0.01-0.05%.
2. a kind of titanium ferroaluminium according to claim 1, it is characterized in that: described composition is made up of following: Ti 93.875%, Al 5%, Fe 1%, O 0.2%, N 0.04%, H 0.015%, C 0.05%.
3. a kind of titanium ferroaluminium according to claim 1, it is characterized in that: described composition is made up of following: Ti 95.3%, Al 3.5%, Fe 1%, O 0.16%, N 0.02%, H 0.01%, C 0.01%.
4. a kind of titanium ferroaluminium according to claim 1, it is characterized in that: described composition is made up of following: Ti 92.65%, Al 5.5%, Fe 1%, O 0.3%, N 0.5%, H 0.013%, C 0.037%.
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CN 201010241013 CN101899590A (en) | 2010-07-29 | 2010-07-29 | Titanium-aluminum-iron alloy |
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CN 201010241013 CN101899590A (en) | 2010-07-29 | 2010-07-29 | Titanium-aluminum-iron alloy |
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Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102566425A (en) * | 2011-12-26 | 2012-07-11 | 南昌航空大学 | Isothermal superplastic forming method for constructing titanium alloy with optimal deformation rate |
WO2014040408A1 (en) * | 2012-09-14 | 2014-03-20 | 北京工业大学 | Low-cost high-strength ti-alloy and heat-treating process therefor |
CN104136639A (en) * | 2012-02-24 | 2014-11-05 | 新日铁住金株式会社 | Titanium alloy for use in golf-club face |
JP2015004100A (en) * | 2013-06-20 | 2015-01-08 | 新日鐵住金株式会社 | α+β TYPE TITANIUM ALLOY MEMBER AND PRODUCTION METHOD THEREOF |
CN105088014A (en) * | 2015-09-15 | 2015-11-25 | 北京工业大学 | Low-cost and high-strength Ti-Fe alloy billet and preparing technology thereof |
CN105112723A (en) * | 2015-08-21 | 2015-12-02 | 燕山大学 | Titanium-iron-carbon alloy with low cost and high strength |
CN106544543A (en) * | 2016-10-25 | 2017-03-29 | 南京工业大学 | Titanium alloy with excellent hot-working performance and preparation method thereof |
Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
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CN1508272A (en) * | 2002-12-17 | 2004-06-30 | 中国乐凯胶片集团公司 | Titanium alloy coated mould material for photographic trade and manufacturing method thereof |
CN101386932A (en) * | 2007-09-14 | 2009-03-18 | 大同特殊钢株式会社 | Low density titanium alloy, golf club head, and process for prouducing low density titanium alloy part |
-
2010
- 2010-07-29 CN CN 201010241013 patent/CN101899590A/en active Pending
Patent Citations (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN1508272A (en) * | 2002-12-17 | 2004-06-30 | 中国乐凯胶片集团公司 | Titanium alloy coated mould material for photographic trade and manufacturing method thereof |
CN101386932A (en) * | 2007-09-14 | 2009-03-18 | 大同特殊钢株式会社 | Low density titanium alloy, golf club head, and process for prouducing low density titanium alloy part |
Cited By (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102566425A (en) * | 2011-12-26 | 2012-07-11 | 南昌航空大学 | Isothermal superplastic forming method for constructing titanium alloy with optimal deformation rate |
CN104136639A (en) * | 2012-02-24 | 2014-11-05 | 新日铁住金株式会社 | Titanium alloy for use in golf-club face |
CN104136639B (en) * | 2012-02-24 | 2016-11-23 | 新日铁住金株式会社 | Golf club face titanium alloy |
WO2014040408A1 (en) * | 2012-09-14 | 2014-03-20 | 北京工业大学 | Low-cost high-strength ti-alloy and heat-treating process therefor |
US9828662B2 (en) | 2012-09-14 | 2017-11-28 | Beijing University Of Technology | Low cost and high strength titanium alloy and heat treatment process |
JP2015004100A (en) * | 2013-06-20 | 2015-01-08 | 新日鐵住金株式会社 | α+β TYPE TITANIUM ALLOY MEMBER AND PRODUCTION METHOD THEREOF |
CN105112723A (en) * | 2015-08-21 | 2015-12-02 | 燕山大学 | Titanium-iron-carbon alloy with low cost and high strength |
CN105088014A (en) * | 2015-09-15 | 2015-11-25 | 北京工业大学 | Low-cost and high-strength Ti-Fe alloy billet and preparing technology thereof |
CN106544543A (en) * | 2016-10-25 | 2017-03-29 | 南京工业大学 | Titanium alloy with excellent hot-working performance and preparation method thereof |
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