ES2261754T3 - ALLOY OF BETA-TITANIUM METAESTABLE. - Google Patents
ALLOY OF BETA-TITANIUM METAESTABLE.Info
- 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
- Authority
- 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
Links
Classifications
-
- 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
Landscapes
- 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
Description
Aleación de \beta-Titanio metaestable.Β-Titanium Alloy metastable
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
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%):
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.
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.
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)
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 |
Family
ID=20254397
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES02783880T Expired - Lifetime ES2261754T3 (en) | 2001-11-22 | 2002-11-18 | ALLOY OF BETA-TITANIUM METAESTABLE. |
Country Status (9)
Country | Link |
---|---|
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)
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)
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 |
-
2001
- 2001-11-22 RU RU2001131383/02A patent/RU2211873C2/en active
-
2002
- 2002-11-18 DK DK02783880T patent/DK1449929T3/en active
- 2002-11-18 DE DE60211548T patent/DE60211548T2/en not_active Expired - Lifetime
- 2002-11-18 AT AT02783880T patent/ATE326554T1/en not_active IP Right Cessation
- 2002-11-18 US US10/496,493 patent/US20060039819A1/en not_active Abandoned
- 2002-11-18 WO PCT/RU2002/000502 patent/WO2003044234A1/en active IP Right Grant
- 2002-11-18 ES ES02783880T patent/ES2261754T3/en not_active Expired - Lifetime
- 2002-11-18 EP EP02783880A patent/EP1449929B1/en not_active Expired - Lifetime
-
2004
- 2004-12-06 HK HK04109637A patent/HK1066832A1/en not_active IP Right Cessation
-
2008
- 2008-02-11 US US12/069,496 patent/US20080199350A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
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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