CN101603134A - A kind of titanium alloy that is used for laser solid forming and laser forming reparation - Google Patents

A kind of titanium alloy that is used for laser solid forming and laser forming reparation Download PDF

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Publication number
CN101603134A
CN101603134A CNA200910023285XA CN200910023285A CN101603134A CN 101603134 A CN101603134 A CN 101603134A CN A200910023285X A CNA200910023285X A CN A200910023285XA CN 200910023285 A CN200910023285 A CN 200910023285A CN 101603134 A CN101603134 A CN 101603134A
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laser
alloy
titanium
present
forming
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CN101603134B (en
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黄卫东
薛蕾
陈静
林鑫
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Xi'an Northwestern Polytechnical University Asset Management Co., Ltd.
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Northwestern Polytechnical University
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Abstract

The present invention is a kind of titanium alloy that is used for laser solid forming and laser forming reparation, comprises titanium, aluminium and vanadium, wherein, aluminium 3.6-5.0wt%, vanadium 2.1-3.4wt%, all the other are titanium, and total amount is no more than absolutely.With respect to TC4 alloy of the prior art, the present invention has reduced aluminium, content of vanadium, has reduced the solution strengthening effect in titanium of aluminium, vanadium, and its intensity reduces, and plasticity improves, and is suitable with the intensity and the plasticity of TC4 alloy forged piece.The mechanical property of the titanium alloy laser deposition attitude that the present invention proposes is: tensile strength 910~980MPa, yield strength 840~915MPa, unit elongation 13~17%, relative reduction in area 39~50%.The present invention not only can be used for laser forming and reparation, and can be used for high energy beam stream processing technologies such as electron beam deposition shaping, electron beam built-up welding, plasma surfacing and shaping.

Description

A kind of titanium alloy that is used for laser solid forming and laser forming reparation
One, technical field
The present invention relates to metal material field, specifically is a kind of titanium alloy that is used for laser solid forming and laser forming reparation.
Two, background technology
The laser solid forming technology is that a kind of advanced person's of growing up over past ten years 3 D auto increases the material manufacturing technology, is used for the quick manufacturing of compact metal part and the regeneration manufacturing of injuring part (laser forming reparation).At present, laser forming and the selected material of reparation mostly are the powdered material of existing alloy, and alloy species comprises wrought alloy, casting alloy, spray powders alloy or the like.But, the technological process of laser forming and reparation is different from complete processings such as forging, casting, therefore use wrought alloy, casting alloy to wait and carry out laser forming and reparation, formation is different from the microstructure of forging and casting, and then obtain to be different from the mechanical property of forging and foundry goods.Expectation obtains higher mechanical property to the laser forming of metal parts with repairing all, and for example, the performance of expectation laser solid forming spare reaches the forging standard, and the performance behind the expectation laser repairing forging still keeps the forging level.
Titanium alloy since its excellent comprehensive performance in the application in fields such as Aeronautics and Astronautics, navigation more and more widely, the TC4 alloy is a kind of titanium alloy gold the most commonly used.Laser solid forming TC4 alloy directly deposits the mechanical property of attitude and compares the characteristic that presents " high-strength low moulding " with this alloy forged piece, need carry out solid-solution and aging heat treatment and just can make the mechanical property of drip molding and forging suitable.Laser forming reparation for the TC4 alloy forged piece, because part is processed or is used, make that repairing postheat treatment is restricted, repair forging if adopt the TC4 powdered alloy, will there be notable difference in the performance of laser repairing district and forging matrix, the whole use properties, particularly fatigue property of back part repaired in influence.How to make the mechanical property of laser repairing district deposition attitude, only the simple thermal treatment through stress relief annealing just can reach the level suitable with forging, is to realize that the titanium alloy forging high-performance repairs the problem of the necessary solution of institute.The key that addresses this problem be exactly make laser repairing district and forging matrix mechanical property as far as possible approaching.Operational characteristic according to laser solid forming and laser forming recovery technique, adopt the TC4 alloy to form or repair, obtain the performance suitable with forging after being difficult in stress relief annealing, therefore developing a kind of titanium alloy that is used for laser solid forming and laser forming reparation is an important channel that obtains strong mechanical performance.
Three, summary of the invention
Be mechanical property and the unmatched deficiency of TC4 alloy forged piece that overcomes the laser direct deposition TC4 alloy that exists in the prior art, the present invention proposes a kind of titanium alloy that is used for laser solid forming and laser forming reparation.
The present invention comprises titanium, aluminium and vanadium for a kind of titanium alloy that is used for laser solid forming and laser forming reparation, wherein, aluminium 3.6-5.0wt%, vanadium 2.1-3.4wt%, all the other are titanium, and total amount is no more than absolutely.
With respect to the TC4 alloy, the present invention has reduced aluminium, content of vanadium, has reduced the solution strengthening effect in titanium of aluminium, vanadium, the present invention can compare with the laser deposition state property of TC4 alloy, intensity decreases, and plasticity increases, and is suitable with the intensity and the plasticity of TC4 alloy forged piece.The mechanical property of described titanium alloy laser deposition attitude is: tensile strength 910~980MPa, yield strength 840~915MPa, unit elongation 13~17%, relative reduction in area 39~50%.As shown in the table with the contrast of TC4 alloy forged piece standard and measured value:
Type σ b/(MPa) σ 0.2/(MPa) δ/(%) Ψ/(%)
The laser deposition attitude of described titanium alloy 910~980 840~915 13~17 39~50
The actual measurement of TC4 alloy forged piece 930~965 870~920 14.5~17.5 39~43.5
TC4 alloy forged piece standard ≥895 ≥825 ≥8~10 ≥25
The present invention not only can be used for laser forming and reparation, and can be used for high energy beam stream processing technologies such as electron beam deposition shaping, electron beam built-up welding, plasma surfacing, shaping.
Four, description of drawings
Accompanying drawing 1 is the laser deposition attitude microstructure of titanium alloy of the present invention.
Accompanying drawing 2 is laser deposition attitude microstructures of titanium alloy of the present invention.
Accompanying drawing 3 is laser deposition attitude microstructures of titanium alloy of the present invention.
Five, embodiment
Embodiment one
The room-temperature mechanical property of present embodiment laser deposition attitude is: tensile strength 910MPa, yield strength 840MPa, unit elongation 17.0%, relative reduction in area 50%.The present invention is a kind of laser solid forming and the special-purpose titanium alloy of reparation, and described titanium alloy comprises titanium, aluminium, vanadium, and in the present embodiment, the proportioning of each alloy compositions is: aluminium 3.6wt%, and vanadium 2.1%, all the other are titanium, and total amount is no more than absolutely.
Embodiment two
The room-temperature mechanical property of present embodiment laser deposition attitude is: tensile strength 935MPa, yield strength 870MPa, unit elongation 15.0%, relative reduction in area 46%.The present invention is a kind of laser solid forming and the special-purpose titanium alloy of reparation, and described titanium alloy comprises titanium, aluminium, vanadium, and in the present embodiment, the proportioning of each alloy compositions is: aluminium 3.9wt%, and vanadium 2.8%, all the other are titanium, and total amount is no more than absolutely.
Embodiment three
The room-temperature mechanical property of present embodiment laser deposition attitude is: tensile strength 980MPa, yield strength 915MPa, unit elongation 13.0%, relative reduction in area 39%.The present invention is a kind of laser solid forming and the special-purpose titanium alloy of reparation, and described titanium alloy comprises titanium, aluminium, vanadium, and in the present embodiment, the proportioning of each alloy compositions is: aluminium 5.0wt%, and vanadium 3.4%, all the other are titanium, and total amount is no more than absolutely.
Embodiment four
The room-temperature mechanical property of present embodiment electron beam deposition attitude is: tensile strength 970MPa, yield strength 910MPa, unit elongation 13.5%, relative reduction in area 42%.The present invention is a kind of laser solid forming and the special-purpose titanium alloy of reparation, and described titanium alloy comprises titanium, aluminium, vanadium, and in the present embodiment, the proportioning of each alloy compositions is: aluminium 4.8wt%, and vanadium 3.2%, all the other are titanium, and total amount is no more than absolutely.
Embodiment five
The room-temperature mechanical property of present embodiment electron beam built-up welding is: tensile strength 930MPa, yield strength 880MPa, unit elongation 15.0%, relative reduction in area 45%.The present invention is a kind of laser solid forming and the special-purpose titanium alloy of reparation, and described titanium alloy comprises titanium, aluminium, vanadium, and in the present embodiment, the proportioning of each alloy compositions is: aluminium 3.9wt%, and vanadium 2.5%, all the other are titanium, and total amount is no more than absolutely.
Embodiment six
The room-temperature mechanical property of present embodiment plasma surfacing is: tensile strength 950MPa, yield strength 905MPa, unit elongation 15.5%, relative reduction in area 48%.The present invention is a kind of laser solid forming and the special-purpose titanium alloy of reparation, and described titanium alloy comprises titanium, aluminium, vanadium, and in the present embodiment, the proportioning of each alloy compositions is: aluminium 4.5wt%, and vanadium 3.2%, all the other are titanium, and total amount is no more than absolutely.
Embodiment seven
The room-temperature mechanical property that the present embodiment plasma is shaped is: tensile strength 940MPa, yield strength 885MPa, unit elongation 16.0%, relative reduction in area 49%.The present invention is a kind of laser solid forming and the special-purpose titanium alloy of reparation, and described titanium alloy comprises titanium, aluminium, vanadium, and in the present embodiment, the proportioning of each alloy compositions is: aluminium 4.3wt%, and vanadium 3.0%, all the other are titanium, and total amount is no more than absolutely.

Claims (1)

1. a titanium alloy that is used for laser solid forming and laser forming reparation comprises titanium, aluminium and vanadium, it is characterized in that aluminium is 3.6-5.0wt%, and vanadium is 2.1-3.4wt%, and all the other are titanium.
CN200910023285XA 2009-07-10 2009-07-10 Titanium alloy for laser solid forming and laser shaping repairing Active CN101603134B (en)

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CN101603134B CN101603134B (en) 2011-07-20

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Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2443800C1 (en) * 2010-07-09 2012-02-27 Учреждение Российской академии наук Институт ядерной физики им. Г.И. Будкера Сибирского отделения РАН (ИЯФ СО РАН) Formation method of corrosion-resistant coating on titanium items
CN104232992A (en) * 2013-06-09 2014-12-24 东港市东方高新金属材料有限公司 Titanium alloy No. dfgx-6 rolled tube and preparation method
JP2015148016A (en) * 2015-03-11 2015-08-20 テイタニウム メタルス コーポレイシヨンTitanium Metals Corporation LOW COST α-β TITANIUM ALLOY HAVING GOOD PROJECTILE PATH AND MECHANICAL PROPERTIES
RU2621745C2 (en) * 2015-08-20 2017-06-07 Федеральное государственное бюджетное учреждение науки Институт ядерной физики им. Г.И. Будкера Сибирского отделения РАН (ИЯФ СО РАН) Method of producing casing of chemical industry apparatus resistant to concentrated acids, from titanium sheets with internal anti-corrosion coating
CN107723517A (en) * 2017-11-08 2018-02-23 大连理工大学 A kind of Ti Al based alloys and its application with good increasing material manufacturing forming property
CN108070740A (en) * 2017-12-28 2018-05-25 沈阳大陆激光技术有限公司 A kind of laser repairing material for repairing titanium alloy spool and valve seat
CN109351978A (en) * 2018-12-11 2019-02-19 苏州大学 Laser melting coating accumulates the method for horizontal rib on not contour section
CN110983103A (en) * 2019-12-05 2020-04-10 江西瑞曼增材科技有限公司 3D printing laser repair method for TB6 titanium alloy
CN113020624A (en) * 2021-03-10 2021-06-25 西北工业大学 Heat treatment method of laser stereo-forming TC4 titanium alloy
CN115094270A (en) * 2022-07-12 2022-09-23 承德石油高等专科学校 High-strength additive manufacturing Ti-Al-V alloy containing Ni, Co and Sc and preparation method thereof

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2443800C1 (en) * 2010-07-09 2012-02-27 Учреждение Российской академии наук Институт ядерной физики им. Г.И. Будкера Сибирского отделения РАН (ИЯФ СО РАН) Formation method of corrosion-resistant coating on titanium items
CN104232992A (en) * 2013-06-09 2014-12-24 东港市东方高新金属材料有限公司 Titanium alloy No. dfgx-6 rolled tube and preparation method
JP2015148016A (en) * 2015-03-11 2015-08-20 テイタニウム メタルス コーポレイシヨンTitanium Metals Corporation LOW COST α-β TITANIUM ALLOY HAVING GOOD PROJECTILE PATH AND MECHANICAL PROPERTIES
RU2621745C2 (en) * 2015-08-20 2017-06-07 Федеральное государственное бюджетное учреждение науки Институт ядерной физики им. Г.И. Будкера Сибирского отделения РАН (ИЯФ СО РАН) Method of producing casing of chemical industry apparatus resistant to concentrated acids, from titanium sheets with internal anti-corrosion coating
CN107723517A (en) * 2017-11-08 2018-02-23 大连理工大学 A kind of Ti Al based alloys and its application with good increasing material manufacturing forming property
CN108070740A (en) * 2017-12-28 2018-05-25 沈阳大陆激光技术有限公司 A kind of laser repairing material for repairing titanium alloy spool and valve seat
CN109351978A (en) * 2018-12-11 2019-02-19 苏州大学 Laser melting coating accumulates the method for horizontal rib on not contour section
CN110983103A (en) * 2019-12-05 2020-04-10 江西瑞曼增材科技有限公司 3D printing laser repair method for TB6 titanium alloy
CN113020624A (en) * 2021-03-10 2021-06-25 西北工业大学 Heat treatment method of laser stereo-forming TC4 titanium alloy
CN115094270A (en) * 2022-07-12 2022-09-23 承德石油高等专科学校 High-strength additive manufacturing Ti-Al-V alloy containing Ni, Co and Sc and preparation method thereof

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