ES2261754T3 - ALLOY OF BETA-TITANIUM METAESTABLE. - Google Patents

ALLOY OF BETA-TITANIUM METAESTABLE.

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Publication number
ES2261754T3
ES2261754T3 ES02783880T ES02783880T ES2261754T3 ES 2261754 T3 ES2261754 T3 ES 2261754T3 ES 02783880 T ES02783880 T ES 02783880T ES 02783880 T ES02783880 T ES 02783880T ES 2261754 T3 ES2261754 T3 ES 2261754T3
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ES
Spain
Prior art keywords
alloy
titanium
ductility
beta
iron
Prior art date
Legal status (The legal status 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 status listed.)
Expired - Lifetime
Application number
ES02783880T
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Spanish (es)
Inventor
Vladislav Valentinovich Tetyukhin
Igor Vasilievich Levin
Denis Valeryevich Sosnovsky
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
VSMPO Avisma Corp PSC
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VSMPO Avisma Corp PSC
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Filing date
Publication date
Application filed by VSMPO Avisma Corp PSC filed Critical VSMPO Avisma Corp PSC
Application granted granted Critical
Publication of ES2261754T3 publication Critical patent/ES2261754T3/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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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

Aleación de \beta-Titanio metaestable.Β-Titanium Alloy metastable

Campo de la invenciónField of the Invention

Esta invención se refiere a la metalurgia no férrica, y con más detalle al desarrollo de nuevas aleaciones a base de titanio que combinan propiedades de alta resistencia y de ductilidad usando elementos de aleación relativamente baratos. Las aleaciones de esta invención pueden ser aplicadas en una amplia gama de productos especialmente cierres y diferentes muelles helicoidales.This invention relates to metallurgy not ferric, and in more detail to the development of new alloys to titanium base that combine high strength properties and Ductility using relatively cheap alloy elements. The Alloys of this invention can be applied in a wide product range especially closures and different springs helical

Estado de la técnica anteriorPrior art

Una de las aleaciones de titanio conocidas es la aleación que contiene (% en masa): 2-6 Al; 6-9 Mo; 1-3 V; 0,5-2 Cr; 0-1.5 Fe; Ti resto. Ref: USSR Certificado de inventor N°. 180351, Clase C22C 14/00,1966.One of the known titanium alloys is the alloy containing (% by mass): 2-6 Al; 6-9 Mo; 1-3 V; 0.5-2 Cr; 0-1.5 Faith; Ti rest. Ref: USSR Certificate of inventor no. 180351, Class C22C 14 / 00,1966.

No obstante, esta aleación tiene una ductilidad insuficiente debido al alto contenido de Al y la presencia de Cr. Además esta aleación es más bien cara. La otra aleación de titanio conocida contiene (% en masa): 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 resto. Ref: Patente RF N°. 2169204, Clase C22C 14/00, publicada 2001.However, this alloy has a ductility insufficient due to the high content of Al and the presence of Cr. In addition this alloy is rather expensive. The other titanium alloy known contains (% by mass): 4-6.3 Al; 4.5-5.9V; 4.5-5.9 Mo; 2.0-3.6 Cr; 0.2-0.5 Fe; Ti rest. Ref: RF Patent No. 2169204, Class C22C 14/00, published 2001.

Dicha aleación cuando es tratada térmicamente tiene altas propiedades de resistencia en los forjados de secciones duras, pero su ductilidad es insuficiente por lo que la aleación no puede ser usada para la producción de este tipo de piezas como muelles helicoidales.Said alloy when heat treated It has high strength properties in section slabs hard, but its ductility is insufficient so the alloy does not It can be used for the production of such parts as coil springs.

La aleación más cercana a la invención reivindicada es la aleación de \beta-titanio metaestable que contiene (% en masa): 4-5 Fe; 4-7 Mo; 1-2 Al; O_{2} hasta 0,25; Ti resto. Ref: Patente de EEUU N°. 5,294,267, Clase C22C 14/00, publicada 1994. Esta aleación será el prototipo. La Patente de EEUU N°. 3,615,378 expone una aleación de beta-titanio metaestable de alta resistencia con buena ductilidad, que contiene uno de Fe, Mn, Cr y Co como elemento eutectoide beta y un contenido de V de 4-9% atómico.The alloy closest to the invention claimed is the β-titanium alloy metastable containing (mass%): 4-5 Fe; 4-7 Mo; 1-2 Al; O2 up to 0.25; Ti rest. Ref: US Patent No. 5,294,267, Class C22C 14/00, published 1994. This alloy will be the prototype. US Pat. No. 3,615,378 exposes a beta-titanium alloy high strength metastable with good ductility, which contains one of Fe, Mn, Cr and Co as beta eutectoid element and a content of V of 4-9% atomic.

Esta aleación tiene alta maquinabilidad, requiere costes relativamente bajos y es extensamente usada para la producción de muelles cilíndricos helicoidales en la industria automovilística.This alloy has high machinability, it requires relatively low costs and is widely used for production of helical cylindrical springs in the industry car.

No obstante, dicha aleación tiene propiedades de ductilidad bajas, especialmente elongación, que reduce la aplicación de esta aleación y es importante en la producción de algunos tipos de muelles helicoidales y componentes de cierres.However, said alloy has properties of low ductility, especially elongation, which reduces the application of this alloy and is important in the production of some types of coil springs and components of closures.

El objeto de esta invención es proporcionar una aleación de titanio que combine alta ductilidad y propiedades en condiciones de tratamiento térmico que pueda ser producida usando elementos de aleación baratos.The object of this invention is to provide a titanium alloy that combines high ductility and properties in heat treatment conditions that can be produced using cheap alloy elements.

Según la invención esto se consigue por adición de vanadio a la aleación de \beta-titanio metaestable conteniendo aluminio, molibdeno y hierro con el siguiente contenido de componentes (% en masa):According to the invention this is achieved by addition vanadium to β-titanium alloy metastable containing aluminum, molybdenum and iron with the following component content (mass%):

AluminioAluminum 1,5-3,51.5-3.5 MolibdenoMolybdenum 4,5-8,04.5-8.0 VanadioVanadium 1,0-3,51.0-3.5 HierroIron 1,5-3,81.5-3.8 TitanioTitanium restorest

La adición de 1,0-3,5% de vanadio aumenta la ductilidad de la aleación como se requiere.The addition of 1.0-3.5% of Vanadium increases the ductility of the alloy as required.

Para conseguir altas propiedades de resistencia esta aleación tiene un contenido más alto de aluminio que el prototipo. El contenido de aluminio inferior a 3,5% no influye significativamente sobre la ductilidad de la aleación. El contenido de aluminio superior a 3,5% y hierro superior a 3,8% aumenta la cantidad de fase a, causa endurecimiento y reduce la ductilidad menos de lo deseado. El contenido inferior de hierro (<4%) que en el prototipo asegura una mayor estabilidad de la fase durante los ciclos térmicos, (deformación y tratamiento térmico). Las propiedades de resistencia deseadas no pueden ser conseguidas con aluminio por debajo de 1,5%. El contenido de molibdeno por debajo de 4.5% y hierro por debajo de 1.5% reduce la cantidad de fase \beta y no permite conseguir una alta resistencia de la aleación tratada térmicamente.To achieve high resistance properties This alloy has a higher aluminum content than the prototype. Aluminum content less than 3.5% does not influence significantly on the ductility of the alloy. The content of aluminum greater than 3.5% and iron greater than 3.8% increases the amount of phase a, causes hardening and reduces ductility less than desired The lower iron content (<4%) than in the prototype ensures greater phase stability during thermal cycles, (deformation and heat treatment). The desired resistance properties cannot be achieved with aluminum below 1.5%. Molybdenum content below 4.5% and iron below 1.5% reduces the amount of phase β and does not allow to achieve high alloy strength heat treated.

El aumento en el contenido de este tipo de estabilizadores \beta como molibdeno y vanadio excediendo los límites especificados reduce la estabilidad de la aleación en condiciones endurecidas y envejecidas y aumenta el tamaño del grano durante el tratamiento térmico, lo que significativamente reduce la ductilidad de la aleación - (\beta <4%; y \Psi < 7%).The increase in the content of this type of β stabilizers such as molybdenum and vanadium exceeding specified limits reduces the stability of the alloy by hardened and aged conditions and increases grain size during heat treatment, which significantly reduces the alloy ductility - (β <4%; and \ Psi <7%).

El molibdeno se añade como ferromolibdeno con 55-75% de molibdeno y resto de hierro.Molybdenum is added as ferromolibdene with 55-75% molybdenum and iron rest.

El vanadio se añade como ferrovanadio con 65-85 % de vanadio y resto de hierro o restos de manufacturas de sistema Ti-Al-V.Vanadium is added as ferrovanadium with 65-85% vanadium and rest of iron or remains of Ti-Al-V system manufactures.

Formas de realización de la invenciónEmbodiments of the invention

Para estudiar las propiedades de la aleación, se derritieron lingotes con la composición mostrada en la tabla 1 en un horno de arco al vacío y se hicieron barras de 20 mm de diámetro de estos lingotes. Las barras fueron tratadas térmicamente bajo las condiciones siguientes: calentamiento a temperatura de 30°C por debajo de la temperatura de beta transus, refrigeración con agua, calentamiento a 480°C durante 8 horas, refrigeración con aire. Entonces se evaluaron las muestras de tracción según ASTM E 8.To study the properties of the alloy, we melted ingots with the composition shown in table 1 in a vacuum arc furnace and 20 mm diameter bars were made of these ingots. The bars were heat treated under the following conditions: heating at a temperature of 30 ° C by below the temperature of beta transus, water cooling, heating at 480 ° C for 8 hours, air cooling. The tensile samples were then evaluated according to ASTM E 8.

En la Tabla 2 se muestran las propiedades mecánicas de las barras producidas de las aleaciones valoradas.Table 2 shows the properties mechanics of the bars produced from the alloys rated.

TABLA 1TABLE 1

Contenido de elementos (% en peso)Content of elements (% by weight) EjemploExample AlTo the MoMo VV FeFaith TiYou 1one 1,51.5 4,54,5 1,01.0 1,51.5 restorest 22 2,52.5 5,55.5 2,02.0 2,52.5 restorest 33 3,03.0 6,56.5 3,03.0 3,53.5 restorest 44 3,53.5 8,08.0 3,53.5 3,83.8 restorest

TABLA 2TABLE 2

Propiedades MecánicasMechanical properties EjemploExample Resistencia Definitiva,Definitive Resistance, Resistencia a laResistance to ElongaciónElongation Reducción deReduction from \sigma_{B}MPa\ sigma_ {B} MPa conformación,conformation, \delta, %\delta, % Area \Psi,%Area \Psi,% \sigma_{o,2}. MPa\ sigma_ {o, 2}. MPa 1one 11001100 1020 -1020 - 25,125.1 58,758.7 22 12501250 11901190 20,220.2 46,446.4 33 14401440 13901390 6,16.1 10,210.2 44 15201520 14801480 4,94.9 7,37.3

Practicabilidad comercialCommercial Practicability

La aleación de \beta-titanio metaestable reivindicada en comparación con las aleaciones conocidas tiene la combinación óptima especificada de elementos de aleación estabilizantes alfa y beta, lo que asegura alta resistencia y ductilidad de la aleación térmicamente tratada. Ésta es barata y puede ser usada para la producción de una amplia gama de piezas fundamentales, particularmente componentes de cierres y muelles helicoidales diferentes.Β-titanium alloy claimed metastable compared to alloys known has the specified optimal combination of elements of Alloy alpha and beta stabilizers, which ensures high strength and ductility of the heat treated alloy. This one is cheap and It can be used for the production of a wide range of parts fundamental, particularly components of closures and springs different helical

Claims (1)

1. Aleación de \beta-titanio metaestable, conteniendo aluminio, molibdeno y hierro, conteniendo adicionalmente vanadio, en el contenido siguiente de componentes (% en masa):1. β-titanium alloy metastable, containing aluminum, molybdenum and iron, containing additionally vanadium, in the following content of components (% mass): AluminioAluminum 1,5-3,51.5-3.5 MolibdenoMolybdenum 4,5-8,04.5-8.0 VanadioVanadium 1,0-3,51.0-3.5 HierroIron 1,5-3,81.5-3.8 TitanioTitanium restorest
ES02783880T 2001-11-22 2002-11-18 ALLOY OF BETA-TITANIUM METAESTABLE. Expired - Lifetime ES2261754T3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU2001131383/02A RU2211873C2 (en) 2001-11-22 2001-11-22 METASTABLE β-TITANIUM ALLOY
RU2001131383 2001-11-22

Publications (1)

Publication Number Publication Date
ES2261754T3 true ES2261754T3 (en) 2006-11-16

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Country Status (9)

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US (2) US20060039819A1 (en)
EP (1) EP1449929B1 (en)
AT (1) ATE326554T1 (en)
DE (1) DE60211548T2 (en)
DK (1) DK1449929T3 (en)
ES (1) ES2261754T3 (en)
HK (1) HK1066832A1 (en)
RU (1) RU2211873C2 (en)
WO (1) WO2003044234A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102005052918A1 (en) * 2005-11-03 2007-05-16 Hempel Robert P Cold-formable Ti alloy
RU2425164C1 (en) 2010-01-20 2011-07-27 Открытое Акционерное Общество "Корпорация Всмпо-Ависма" Secondary titanium alloy and procedure for its fabrication
CN102586639A (en) * 2012-03-16 2012-07-18 广州有色金属研究院 Method for preparing titanium alloy through high-speed pressing formation
GB201701251D0 (en) * 2017-01-25 2017-03-08 Univ Oxford Innovation Ltd A titanium-based alloy

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU180351A1 (en) * 1965-01-06 1966-03-21 TITANIUM BASED ALLOY
US3615378A (en) * 1968-10-02 1971-10-26 Reactive Metals Inc Metastable beta titanium-base alloy
GB1333729A (en) * 1970-10-23 1973-10-17 Lockheed Aircraft Corp Titanium base alloy
DE3425055C1 (en) * 1984-07-07 1985-07-25 Daimler-Benz Ag, 7000 Stuttgart Getter substance
JP2737498B2 (en) * 1991-12-24 1998-04-08 日本鋼管株式会社 Titanium alloy for high density powder sintering
JP2803455B2 (en) * 1992-04-15 1998-09-24 日本鋼管株式会社 Manufacturing method of high density powder sintered titanium alloy
US5294267A (en) * 1992-12-04 1994-03-15 Titanium Metals Corporation Metastable beta titanium-base alloy
US5980655A (en) * 1997-04-10 1999-11-09 Oremet-Wah Chang Titanium-aluminum-vanadium alloys and products made therefrom
US5855697A (en) * 1997-05-21 1999-01-05 Imra America, Inc. Magnesium alloy having superior elevated-temperature properties and die castability
RU2169204C1 (en) * 2000-07-19 2001-06-20 ОАО Верхнесалдинское металлургическое производственное объединение Titanium-based alloy and method of thermal treatment of large-size semiproducts from said alloy
RU2269584C1 (en) * 2004-07-30 2006-02-10 Открытое Акционерное Общество "Корпорация Всмпо-Ависма" Titanium-base alloy
US20060045789A1 (en) * 2004-09-02 2006-03-02 Coastcast Corporation High strength low cost titanium and method for making same

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ATE326554T1 (en) 2006-06-15
DK1449929T3 (en) 2006-06-12
WO2003044234A1 (en) 2003-05-30
EP1449929A4 (en) 2005-02-02
HK1066832A1 (en) 2005-04-01
DE60211548D1 (en) 2006-06-22
DE60211548T2 (en) 2006-09-14
US20080199350A1 (en) 2008-08-21
EP1449929B1 (en) 2006-05-17
US20060039819A1 (en) 2006-02-23
RU2211873C2 (en) 2003-09-10
EP1449929A1 (en) 2004-08-25

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