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HK1066832A1 - Metastable beta-titanium alloy - Google Patents

Metastable beta-titanium alloy Download PDF

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Publication number
HK1066832A1
HK1066832A1 HK04109637A HK04109637A HK1066832A1 HK 1066832 A1 HK1066832 A1 HK 1066832A1 HK 04109637 A HK04109637 A HK 04109637A HK 04109637 A HK04109637 A HK 04109637A HK 1066832 A1 HK1066832 A1 HK 1066832A1
Authority
HK
Hong Kong
Prior art keywords
alloy
titanium alloy
ductility
balance
iron
Prior art date
Application number
HK04109637A
Other languages
German (de)
French (fr)
Chinese (zh)
Other versions
HK1066832B (en
Inventor
Vladislav Valentinovich Tetyukhin
Igor Vasilievich Levin
Denis Valeryevich Sosnovsky
Original Assignee
Vsmpo-Avisma Corporation
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Vsmpo-Avisma Corporation filed Critical Vsmpo-Avisma Corporation
Publication of HK1066832A1 publication Critical patent/HK1066832A1/en
Publication of HK1066832B publication Critical patent/HK1066832B/en

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Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys 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)
  • Springs (AREA)
  • Heat Treatment Of Articles (AREA)
  • Ceramic Products (AREA)
  • Forging (AREA)

Abstract

Metastable beta -titanium alloy contains, in mass %: from 1.5 to 3.5 aluminum; from 4.5 to 8.0 molybdenum; from 1.0 to 3.5 vanadium; from 1.5 to 3.8 iron; titanium balance. This alloy combines high strength and ductility. This allows to use it for production of a wide range of critical parts including fastener components and different coil springs (e.g. in automobile industry).

Description

Field of the invention
This invention relates to the non-ferrous metallurgy, and more particularly to the development of new titanium-base alloys combining high strength and ductility properties using relatively low-cost alloying elements. The alloys of this invention can be applied in a wide range of products especially fasteners and different coil springs.
Prior state of art
One of the known titanium alloys is the alloy containing (mass %): 2-6 Al; 6-9 Mo; 1-3 V; 0.5-2 Cr; 0-1.5 Fe; Ti balance. Ref: USSR Inventor's Certificate No. 180351, Class C22C 14/00, 1966.
However, this alloy has insufficient ductility due to the high content of Al and the presence of Cr. Besides this alloy is rather expensive.
The other known titanium alloy contains (mass %): 4-6.3 Al; 4.5-5.9 V; 4.5-5.9 Mo; 2.0-3.6 Cr; 0.2-0.5 Fe; Ti balance. Ref: RF Patent No. 2169204, Class C22C 14/00, published 2001.
The said alloy as-heat treated has high strength properties in heavy section forgings, but its ductility is insufficient and so the alloy cannot be used for production of such parts as coil springs.
The alloy most close to the claimed invention is the metastable β-titanium alloy containing (mass %): 4-5 Fe; 4-7 Mo; 1-2 Al; O2 up to 0.25; Ti balance. Ref: US Patent No. 5,294,267, Class C22C 14/00, published 1994. This alloy will be the prototype. US patent No. 3,615,378 discloses a high-strength metastable beta-titanium alloy with good ductility, which contains one of Fe, Mn, Cr and Co as the beta-eutecnoid elements and a V-content of 4-9 atomic %.
This alloy has high machinability, demands relatively low costs and is widely used for production of coil cylindrical springs in automotive industry.
However, said alloy has low especially elongation, which reduces the application of this alloy and is of importance during manufacture of some types of coil springs and fastener components.
Disclosure of the invention
The object of this invention is to provide a titanium alloy with combination of high ductility and strength properties in a heat treated condition, which can be produced using low cost alloying elements.
In accordance with the invention this is achieved by addition of vanadium to the metastable β-titanium alloy containing aluminum, molybdenum and iron at the following content of components (mass %):
Aluminum 1.5 - 3.5
Molybdenum 4.5-8.0
Vanadium 1.0-3.5
Iron 1.5-3.8
Titanium balance
The addition of 1.0-3.5% vanadium increases the alloy ductility as required.
To achieve high strength properties this alloy has higher content of aluminum than the prototype. The content of aluminum of less than 3.5% does not significantly influence on the alloy ductility. The contents of aluminum greater than 3.5% and iron greater than 3.8% increases the α-phase quantity, causes hardening and reduces ductility lower than desired. The lower content of iron (< 4%) than in the prototype ensures greater phase stability during thermal cycles (deformation and heat treatment). The desired strength properties cannot be achieved with aluminum below 1.5%. The content of molybdenum below 4.5% and iron below 1.5% reduces β-phase quantity and does not allow to achieve high strength of the as-heat treated alloy.
The increase in the content of such β-stabilizers as molybdenum and vanadium exceeding the specified limits reduces the alloy stability in hardened and aged conditions and increases the grain size during heat treatment, which significantly reduces the alloy ductility (β < 4%; Ψ < 7%).
Molybdenum is added as ferromolybdenum with 55-75% of molybdenum and iron balance.
Vanadium is added as ferrovanadium with 65-85 % of vanadium and iron balance or Ti-Al-V system scrap.
Embodiments of the invention
To study the properties of the alloy, ingots with the composition shown in Table 1 were melted in a vacuum arc furnace and 20 mm diameter bars were made from these ingots. The bars were heat treated under the following conditions: heating to temperature of 30 °C below beta transus temperature, water cooling, heating to 480 °C for 8 hours, air cooling. Then tensile specimens were tested according to ASTM E 8. Mechanical properties of the produced bars from the evaluated alloys are shown in Table 2. Table 1
Example Element Content (wt %)
Al Mo V Fe Ti
1 1.5 4.5 1.0 1.5 balance
2 2.5 5.5 2.0 2.5 balance
3 3.0 6.5 3.0 3.5 balance
4 3.5 8.0 3.5 3.8 balance
Table 2
Example Mechanical Properties
Elongation δ, % Reduction of Area Ψ, %
1 1100 1020 25.1 58.7
2 1250 1190 20.2 46.4
3 1440 1390 6.1 10.2
4 1520 1480 4.9 7.3
Commercial practicability
The claimed metastable β-titanium alloy as compared to the known alloys has the specified optimal combination of beta and alpha stabilizing alloying elements, which ensure high strength and ductility of the as-heat treated alloy. It is low cost and can be used for production of a wide range of critical parts, especially fastener components and different coil springs.

Claims (1)

  1. Metastable β-titanium alloy containing aluminum, molybdenum and iron, wherein it additionally contains vanadium, at the following content of components (mass %): Aluminum 1.5-3.5 Molybdenum 4.5-8.0 Vanadium 1.0-3.5 Iron 1.5-3.8 Titanium balance
HK04109637.6A 2001-11-22 2002-11-18 Metastable beta-titanium alloy HK1066832B (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
RU2001131383 2001-11-22
RU2001131383/02A RU2211873C2 (en) 2001-11-22 2001-11-22 METASTABLE β-TITANIUM ALLOY
PCT/RU2002/000502 WO2003044234A1 (en) 2001-11-22 2002-11-18 Metastable $g(b)-titanium alloy

Publications (2)

Publication Number Publication Date
HK1066832A1 true HK1066832A1 (en) 2005-04-01
HK1066832B HK1066832B (en) 2006-09-22

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Also Published As

Publication number Publication date
US20060039819A1 (en) 2006-02-23
RU2211873C2 (en) 2003-09-10
ATE326554T1 (en) 2006-06-15
ES2261754T3 (en) 2006-11-16
US20080199350A1 (en) 2008-08-21
EP1449929B1 (en) 2006-05-17
DE60211548T2 (en) 2006-09-14
EP1449929A1 (en) 2004-08-25
DK1449929T3 (en) 2006-06-12
WO2003044234A1 (en) 2003-05-30
EP1449929A4 (en) 2005-02-02
DE60211548D1 (en) 2006-06-22

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Legal Events

Date Code Title Description
PC Patent ceased (i.e. patent has lapsed due to the failure to pay the renewal fee)

Effective date: 20091118