[go: up one dir, main page]

EP1015650A1 - Alloy based on titanium aluminides - Google Patents

Alloy based on titanium aluminides

Info

Publication number
EP1015650A1
EP1015650A1 EP98948778A EP98948778A EP1015650A1 EP 1015650 A1 EP1015650 A1 EP 1015650A1 EP 98948778 A EP98948778 A EP 98948778A EP 98948778 A EP98948778 A EP 98948778A EP 1015650 A1 EP1015650 A1 EP 1015650A1
Authority
EP
European Patent Office
Prior art keywords
alloy
alloys
titanium
alloy based
niobium
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.)
Granted
Application number
EP98948778A
Other languages
German (de)
French (fr)
Other versions
EP1015650B1 (en
Inventor
Jonathan Paul
Fritz Appel
Richard Wagner
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.)
GKSS Forshungszentrum Geesthacht GmbH
Original Assignee
GKSS Forshungszentrum Geesthacht GmbH
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 GKSS Forshungszentrum Geesthacht GmbH filed Critical GKSS Forshungszentrum Geesthacht GmbH
Publication of EP1015650A1 publication Critical patent/EP1015650A1/en
Application granted granted Critical
Publication of EP1015650B1 publication Critical patent/EP1015650B1/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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

Definitions

  • the invention relates to an alloy based on Titanal u iniden.
  • alloys based on titanium aluminides for purposes in which on the one hand a very low weight and on the other hand a high strength of the material is required. Alloys based on titanium aniids therefore often replace ordinary nickel-based superalloys, which are currently still used in individual components, for example in turbines as turbine blades.
  • the alloys based on titanium tanimides do not always have all the properties of the above-mentioned superalloys, even though they are light in weight with high strength, and so far can also have the properties of these superallegi high technical standards.
  • a major disadvantage of the previously known alloys based on Ti tanal umi is that they have a significant decrease in the strengthening properties from an operating temperature of 700 ° C. This is particularly true at low deformation speeds, which are characteristic of a material stress under creep conditions.
  • the object is achieved according to the invention by an alloy composition of titanium, aluminum and niobium.
  • the advantage of the solution according to the invention is that, as tests have shown, significantly higher strengths up to the temperature range of 900 ° C. and higher, that is to say at operating temperatures to which the alloy according to the invention is exposed, can be achieved compared to previously known See alloys based on previously used Titanal umi ni dgemi.
  • the oxidation resistance of the alloy proposed according to the invention is very much greater than previous alloy mixtures of the generic type, i.e. overall, the alloys proposed according to the invention, because of their far higher temperature resistance than previous alloys of this type, can help to achieve technical solutions to which neither the nickel-based super alloys nor the titanium-based alloys have hitherto been capable.
  • the proportion of niobium in the alloy can vary, advantageously in such a way that 5 ⁇ x ⁇ 10, with an alloy composition corresponding to Ti-45Al-xNb.
  • Fig. 1 shows the variation of the flow resistance measured in the pressure test over the temperature of the alloy according to the invention and known alloys based on titanium uminides and
  • Fig. 2 shows the reciprocal activation volume (1 / V) after 1.25% plastic deformation under pressure of various alloys according to the invention and already known alloys based on Ti tanal umi ni with a different composition.
  • the alloys according to the invention with the composition Ti-45Al-xNb with 5 ⁇ x ⁇ 10 are produced by using conventional metallurgical casting methods or by powder metallurgical techniques known per se and can be processed, for example, by hot forging, hot pressing or hot extrusion and hot rolling.
  • the objects made from the alloys can also be used to increase the strength at high working temperatures, ie up to 900 ° C and moreover boron, and / or carbon are added in amounts less than 0.5 atomic%.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
  • Solid-Phase Diffusion Into Metallic Material Surfaces (AREA)
  • Materials For Medical Uses (AREA)
  • Chemical Treatment Of Metals (AREA)

Abstract

In an alloy on the basis of titanium aluminides niobium is included in the alloy of titanium and aluminum.

Description

Legierung auf der Basis von Ti tanal umi nidenAlloy based on titanium tan umides
Beschrei bungDescription
Die Erfindung betrifft eine Legierung auf der Basis von Titanal u iniden .The invention relates to an alloy based on Titanal u iniden.
Es ist bekannt, Legierungen auf der Basis von Titanalu- miniden für Zwecke einzusetzen, bei denen einerseits ein sehr geringes Gewicht und andererseits eine hohe Festigkeit des Werkstoffs erforderlich ist. Legierungen auf der Basis von Ti tanal umi niden ersetzen deshalb schon vielfach gewöhnliche Superl egi erungen auf Nickelbasis, die gegenwärtig noch in einzelnen Komponenten, beispielsweise in Turbinen als Turbinenschaufeln, Verwendung finden. Die Legierungen auf der Basis von Ti tanal umi niden haben allerdings, obwohl sie an sich bei hoher Festigkeit ein geringes Gewicht aufweisen, nicht in jedem Falle alle die Eigenschaften, die die zuvor genannten Superlegie- rungen aufweisen und können bisher auch die durch diese Superl egi erungen gesetzten hohen technischen Standards nicht vollständig erfüllen. Ein wesentlicher Nachteil der bisher bekannten Legierungen auf der Basis von Ti tanal umi niden ist der, daß sie ab einer Betriebstemperatur von 700° C eine deutliche Abnahme der Festigungseigenschaften aufweisen. Dies trifft insbesondere bei niedrigen Verformungsgeschwindigkeiten auf, die für eine Materi al beanspruchung unter Kriechbedingungen charakteristisch sind.It is known to use alloys based on titanium aluminides for purposes in which on the one hand a very low weight and on the other hand a high strength of the material is required. Alloys based on titanium aniids therefore often replace ordinary nickel-based superalloys, which are currently still used in individual components, for example in turbines as turbine blades. However, the alloys based on titanium tanimides do not always have all the properties of the above-mentioned superalloys, even though they are light in weight with high strength, and so far can also have the properties of these superallegi high technical standards. A major disadvantage of the previously known alloys based on Ti tanal umi is that they have a significant decrease in the strengthening properties from an operating temperature of 700 ° C. This is particularly true at low deformation speeds, which are characteristic of a material stress under creep conditions.
Es ist deshalb Aufgabe der vorliegenden Erfindung, eine Legierung auf der Basis von Ti tanal umi niden bereitzustellen, die diese Nachteile nicht hat, d.h. eine Legierung, die ebenfalls eine hohe Temperaturfestigkeit aufweist, so daß diese auch geeignet ist, als Ersatz für Legierungen auf Nickelbasis zu dienen, wobei die erfindungsgemäße Legierung dennoch einfach und kostengünstig herstellbar und verhältnismäßig einfach bearbeitbar sein soll .It is therefore an object of the present invention to provide an alloy based on titanium amides which does not have these disadvantages, i.e. an alloy which also has a high temperature resistance, so that it is also suitable to serve as a substitute for alloys based on nickel, the alloy according to the invention should nevertheless be simple and inexpensive to produce and relatively easy to machine.
Gelöst wird die Aufgabe gemäß der Erfindung durch eine Legierungszusammensetzung aus Titan, Aluminium und Niob.The object is achieved according to the invention by an alloy composition of titanium, aluminum and niobium.
Der Vorteil der erfindungsgemäßen Lösung besteht darin, daß, wie Versuche ergeben haben, signifikant höhere Festigkeiten bis in den Temperaturbereich von 900° C und höher, d.h. bei derartigen Betriebstemperaturen, denen die erfi ndungsgemäße Legierung ausgesetzt ist, erreicht werden können, und zwar gegenüber den bisher bekannten Legierungen auf der Basis von bisher verwendeten Titanal umi ni dgemi sehen .The advantage of the solution according to the invention is that, as tests have shown, significantly higher strengths up to the temperature range of 900 ° C. and higher, that is to say at operating temperatures to which the alloy according to the invention is exposed, can be achieved compared to previously known See alloys based on previously used Titanal umi ni dgemi.
Ein weiterer wesentlicher Vorteil, der sich durch die erfindungsgemäß vorgeschlagene Lösung ergeben hat, ist der, daß der Oxidati onswiderstand der erfindungsgemäß vorgeschlagenen Legierung sehr viel größer ist im Vergleich zu bisherigen Legierungsgemischen der gattungsgemäßen Art, d.h. insgesamt können die erfindungsgemäß vorgeschlagenen Legierungen aufgrund ihrer weit höheren Temperaturbeständigkeit gegenüber bisherigen Legierungen dieser Art zu technischen Lösungen verhelfen, zu denen bisher weder die Superl egi erungen auf Nickelbasis noch die Legierungen auf der Basis von Ti tanal umi niden befähigt waren.Another important advantage that has resulted from the solution proposed according to the invention is that the oxidation resistance of the alloy proposed according to the invention is very much greater than previous alloy mixtures of the generic type, i.e. overall, the alloys proposed according to the invention, because of their far higher temperature resistance than previous alloys of this type, can help to achieve technical solutions to which neither the nickel-based super alloys nor the titanium-based alloys have hitherto been capable.
Um die Festigkeit der Legierung noch weiter zu erhöhen, ist es vorteilhaft, der Legierungszusammensetzung aus Titan, Aluminium und Niob noch Komponenten aus Bor und/oder Kohlenstoff zuzufügen, wodurch sich die Legierung dann noch für weitere andere Einsatzfälle eignet, beispielsweise für den Einsatz in Hochleistungsturbinen für Strahltriebwerke in zivil und militärisch genutzten Fl ugzeugen .In order to increase the strength of the alloy even further, it is advantageous to add components made of boron and / or carbon to the alloy composition of titanium, aluminum and niobium, which then makes the alloy suitable for further other applications, for example for use in high-performance turbines for jet engines in civil and military aircraft.
Versuche haben ergeben, daß es vorteilhaft ist, dabei den Anteil an Bor und/oder Kohlenstoff in der Legierung unterhalb einer Konzentration von 0,5 Atom % zu wählen.Experiments have shown that it is advantageous to choose the proportion of boron and / or carbon in the alloy below a concentration of 0.5 atom%.
Der Anteil von Niob in der Legierung kann variieren, und zwar vorteilhafterweise derart, daß 5 < x < 10 ist und zwar bei einer Legierungszusammensetzung entsprechend Ti-45Al-xNb. Die Erfindung wird nun unter Bezugnahme zweier graphischer Darstellungen beschrieben. Darin zeigen:The proportion of niobium in the alloy can vary, advantageously in such a way that 5 <x <10, with an alloy composition corresponding to Ti-45Al-xNb. The invention will now be described with reference to two graphical representations. In it show:
Fig. 1 die Variation des im Druckversuch gemessenen Fließ-Widerstandes über die Temperatur der erfi nderungsgemäßen Legierung sowie bekannter Legierungen auf der Basis von Ti tanal uminiden undFig. 1 shows the variation of the flow resistance measured in the pressure test over the temperature of the alloy according to the invention and known alloys based on titanium uminides and
Fig. 2 das reziproke Aktivierungsvolumen (1/V) nach 1,25 % plastischer Verformung unter Druck verschiedener erfindungsgemäßer Legierungen sowie bereits bekannter Legierungen auf der Basis von Ti tanal umi ni den mit anderer Zusammensetzung .Fig. 2 shows the reciprocal activation volume (1 / V) after 1.25% plastic deformation under pressure of various alloys according to the invention and already known alloys based on Ti tanal umi ni with a different composition.
Die voraufgeführten Figuren zeigen, daß die erfindungsgemäßen Legierungen sehr viel höhere Festigkeitswerte als konventionelle Legierungen haben. Gleichzeitig ist jedoch das reziproke Aktivierungsvolumen der erfindungsgemäßen Legierungen mit dem konventioneller Legierungen vergleichbar. Das bedeutet, daß größere Festigkeit von Legierungen, die Niob neben Titan und Aluminium enthalten, auch bei hohen Temperaturen und niedrigen Verformungsgeschwindigkeiten aufrecht erhalten bleibt.The figures shown above show that the alloys according to the invention have much higher strength values than conventional alloys. At the same time, however, the reciprocal activation volume of the alloys according to the invention is comparable to that of conventional alloys. This means that greater strength of alloys that contain niobium in addition to titanium and aluminum is maintained even at high temperatures and low deformation rates.
Die erfindungsgemäßen Legierungen mit der Zusammensetzung Ti-45Al-xNb mit 5 < x < 10 werden durch Verwendung herkömmlicher metallurgischer Gießmethoden oder durch an sich bekannte pul ermetallurgische Techniken erzeugt und können beispielsweise durch Warmschmieden, Warmpressen bzw. Warmstrangpressen und Warmwalzen bearbeitet werden.The alloys according to the invention with the composition Ti-45Al-xNb with 5 <x <10 are produced by using conventional metallurgical casting methods or by powder metallurgical techniques known per se and can be processed, for example, by hot forging, hot pressing or hot extrusion and hot rolling.
Neben den Basiskomponenten der Legierung aus Titan, Aluminium und Niob kann auch noch zur Erhöhung der Festigkeit bei hohen Arbeitstemperaturen der aus den Legierungen hergestellten Gegenstände, d.h. bis 900° C und darüber hinaus Bor, und/oder Kohlenstoff in Mengen von weniger als 0,5 Atom % hinzugefügt werden. In addition to the basic components of the alloy made of titanium, aluminum and niobium, the objects made from the alloys can also be used to increase the strength at high working temperatures, ie up to 900 ° C and moreover boron, and / or carbon are added in amounts less than 0.5 atomic%.

Claims

Patentansprüche claims
1. Legierung auf der Basis von Ti tanal umi niden , gekennzeichnet durch eine Legierungszusammensetzung aus Titan, Aluminium und Niob.1. Alloy based on Ti tanal umi niden, characterized by an alloy composition of titanium, aluminum and niobium.
2. Legierung nach Anspruch 1, dadurch gekennzeichnet, daß diese Bor enthält.2. Alloy according to claim 1, characterized in that it contains boron.
3. Legierung nach einem oder beiden der Ansprüche 1 oder 2, dadurch gekennzeichnet, daß diese Kohlenstoff enthält.3. Alloy according to one or both of claims 1 or 2, characterized in that it contains carbon.
4. Legierung nach einem oder beiden der Ansprüche 2 oder 3, dadurch gekennzeichnet, daß der Anteil von Bor und/oder Kohlenstoff in der Legierung < 0,5 Atom % ist. 4. Alloy according to one or both of claims 2 or 3, characterized in that the proportion of boron and / or carbon in the alloy is <0.5 atom%.
5. Legierung nach einem oder mehreren der Ansprüche 1 bis 4, dadurch gekennzeichnet, daß deren Zusammensetzung Ti-45Al-xNb ist, wobei 5 < x < 10 ist. 5. Alloy according to one or more of claims 1 to 4, characterized in that its composition is Ti-45Al-xNb, where 5 <x <10.
EP98948778A 1997-08-19 1998-08-12 Alloy based on titanium aluminides Expired - Lifetime EP1015650B1 (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE19735841 1997-08-19
DE19735841A DE19735841A1 (en) 1997-08-19 1997-08-19 Titanium aluminide alloy contains niobium
PCT/DE1998/002323 WO1999009228A1 (en) 1997-08-19 1998-08-12 Alloy based on titanium aluminides

Publications (2)

Publication Number Publication Date
EP1015650A1 true EP1015650A1 (en) 2000-07-05
EP1015650B1 EP1015650B1 (en) 2004-01-07

Family

ID=7839366

Family Applications (1)

Application Number Title Priority Date Filing Date
EP98948778A Expired - Lifetime EP1015650B1 (en) 1997-08-19 1998-08-12 Alloy based on titanium aluminides

Country Status (7)

Country Link
US (1) US6524407B1 (en)
EP (1) EP1015650B1 (en)
CN (1) CN1115421C (en)
AT (1) ATE257521T1 (en)
DE (2) DE19735841A1 (en)
RU (1) RU2203339C2 (en)
WO (1) WO1999009228A1 (en)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP3915324B2 (en) * 1999-06-08 2007-05-16 石川島播磨重工業株式会社 Titanium aluminide alloy material and castings thereof
DE10058155A1 (en) * 2000-11-22 2002-05-23 Geesthacht Gkss Forschung Alloy based on titanium aluminides produced using a smelting and powder metallurgical process and containing an alloy composition made from titanium, aluminum and niobium has specified an aluminum content
DE102004056582B4 (en) * 2004-11-23 2008-06-26 Gkss-Forschungszentrum Geesthacht Gmbh Alloy based on titanium aluminides
DE102007060587B4 (en) 2007-12-13 2013-01-31 Helmholtz-Zentrum Geesthacht Zentrum für Material- und Küstenforschung GmbH titanium aluminide
US8858697B2 (en) 2011-10-28 2014-10-14 General Electric Company Mold compositions
US9011205B2 (en) 2012-02-15 2015-04-21 General Electric Company Titanium aluminide article with improved surface finish
US8932518B2 (en) 2012-02-29 2015-01-13 General Electric Company Mold and facecoat compositions
US8906292B2 (en) 2012-07-27 2014-12-09 General Electric Company Crucible and facecoat compositions
US8708033B2 (en) 2012-08-29 2014-04-29 General Electric Company Calcium titanate containing mold compositions and methods for casting titanium and titanium aluminide alloys
US8992824B2 (en) 2012-12-04 2015-03-31 General Electric Company Crucible and extrinsic facecoat compositions
CN103060610A (en) * 2012-12-28 2013-04-24 洛阳双瑞精铸钛业有限公司 A casting method for the preparation of thin-wall blades by using a titanium alloy containing trace amount of carbon
US9592548B2 (en) 2013-01-29 2017-03-14 General Electric Company Calcium hexaluminate-containing mold and facecoat compositions and methods for casting titanium and titanium aluminide alloys
RU2520250C1 (en) * 2013-03-14 2014-06-20 Федеральное государственное автономное образовательное учреждение высшего профессионального образования "Национальный исследовательский технологический университет "МИСиС" Gamma titanium aluminide-based alloy
US9192983B2 (en) 2013-11-26 2015-11-24 General Electric Company Silicon carbide-containing mold and facecoat compositions and methods for casting titanium and titanium aluminide alloys
US9511417B2 (en) 2013-11-26 2016-12-06 General Electric Company Silicon carbide-containing mold and facecoat compositions and methods for casting titanium and titanium aluminide alloys
US10391547B2 (en) 2014-06-04 2019-08-27 General Electric Company Casting mold of grading with silicon carbide
RU2592657C2 (en) * 2014-12-29 2016-07-27 Федеральное государственное унитарное предприятие "Всероссийский научно-исследовательский институт авиационных материалов" (ФГУП "ВИАМ") Heat-resistant titanium-based alloy and article made therefrom
EP3249064A1 (en) 2016-05-23 2017-11-29 MTU Aero Engines GmbH Additive manufacture of high temperature components from tial
EP3326746A1 (en) 2016-11-25 2018-05-30 Helmholtz-Zentrum Geesthacht Zentrum für Material- und Küstenforschung GmbH Method for joining and/or repairing substrates of titanium aluminide alloys
CN107699738A (en) * 2017-09-29 2018-02-16 成都露思特新材料科技有限公司 A kind of fine-grained TiAl alloy and preparation method thereof, aero-engine, automobile

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1179006B (en) * 1952-12-18 1964-10-01 Crucible Steel Internat Titanium alloys
US3203794A (en) * 1957-04-15 1965-08-31 Crucible Steel Co America Titanium-high aluminum alloys
JP2679109B2 (en) * 1988-05-27 1997-11-19 住友金属工業株式会社 Intermetallic compound TiA-based light-weight heat-resistant alloy
US4916028A (en) * 1989-07-28 1990-04-10 General Electric Company Gamma titanium aluminum alloys modified by carbon, chromium and niobium
CA2025272A1 (en) * 1989-12-04 1991-06-05 Shyh-Chin Huang High-niobium titanium aluminide alloys
US5080860A (en) * 1990-07-02 1992-01-14 General Electric Company Niobium and chromium containing titanium aluminide rendered castable by boron inoculations
US5082624A (en) * 1990-09-26 1992-01-21 General Electric Company Niobium containing titanium aluminide rendered castable by boron inoculations
US5264054A (en) * 1990-12-21 1993-11-23 General Electric Company Process of forming titanium aluminides containing chromium, niobium, and boron
US5204058A (en) * 1990-12-21 1993-04-20 General Electric Company Thermomechanically processed structural elements of titanium aluminides containing chromium, niobium, and boron
US5370839A (en) * 1991-07-05 1994-12-06 Nippon Steel Corporation Tial-based intermetallic compound alloys having superplasticity
US5205875A (en) * 1991-12-02 1993-04-27 General Electric Company Wrought gamma titanium aluminide alloys modified by chromium, boron, and nionium
DE69208837T2 (en) * 1991-12-02 1996-10-31 Gen Electric Titanium-aluminum alloys of the gamma type modified with chrome, tantalum and boron
US5213635A (en) * 1991-12-23 1993-05-25 General Electric Company Gamma titanium aluminide rendered castable by low chromium and high niobium additives
US5503798A (en) * 1992-05-08 1996-04-02 Abb Patent Gmbh High-temperature creep-resistant material
DE4224867A1 (en) * 1992-07-28 1994-02-03 Abb Patent Gmbh Highly heat-resistant material
JPH06116692A (en) * 1992-10-05 1994-04-26 Honda Motor Co Ltd TiAl intermetallic compound excellent in high temperature strength and method for producing the same
US5447680A (en) * 1994-03-21 1995-09-05 Mcdonnell Douglas Corporation Fiber-reinforced, titanium based composites and method of forming without depletion zones
JPH08283890A (en) * 1995-04-13 1996-10-29 Nippon Steel Corp TiAl-based intermetallic compound having excellent creep resistance and method for producing the same
RU2081929C1 (en) * 1995-08-10 1997-06-20 Московский авиационный технологический университет им.К.Э.Циолковского Titanium aluminide-based alloy

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO9909228A1 *

Also Published As

Publication number Publication date
US6524407B1 (en) 2003-02-25
DE19735841A1 (en) 1999-02-25
ATE257521T1 (en) 2004-01-15
CN1276021A (en) 2000-12-06
WO1999009228A1 (en) 1999-02-25
EP1015650B1 (en) 2004-01-07
CN1115421C (en) 2003-07-23
RU2203339C2 (en) 2003-04-27
DE59810561D1 (en) 2004-02-12

Similar Documents

Publication Publication Date Title
EP1015650A1 (en) Alloy based on titanium aluminides
DE2445462C3 (en) Use of a nickel alloy
DE3884887T2 (en) Heavy metal alloys made of tungsten-nickel-iron-cobalt with high hardness and process for producing these alloys.
EP1978120B1 (en) Aluminium-silicon alloy and method for production of same
DE69015021T2 (en) Gamma-titanium-aluminum alloys modified by chromium and tantalum and manufacturing processes.
DE69229971T2 (en) Chromium containing gamma titanium aluminides
DE3030962A1 (en) SINGLE AND POLYCRYSTALLINE ALLOY ON NICKEL OR COBALT BASE.
DE3921626C2 (en) High strength component with low fatigue crack propagation speed
DE2425994C2 (en) Material with directed fibrous design of tantalum and / or vanadium carbide
DE2456857C3 (en) Use of a nickel-based alloy for uncoated components in the hot gas part of turbines
DE2613255C2 (en) Use of an iron-molybdenum-nickel sintered alloy with the addition of phosphorus for the production of high-strength workpieces
DE2415035B2 (en) Process for the powder-metallurgical production of a sliding piece of high strength, in particular a crown seal for rotary piston machines
DE69219508T2 (en) Wear-resistant aluminum alloy and process for its processing
EP0760869B1 (en) Nickel-aluminium intermetallic basis alloy
DE2215607A1 (en) ALPHA / BETA - TITANIUM ALLOY
DE2049546A1 (en)
DE2527425A1 (en) DIRECTED CONSOLIDATED NICKEL-BASED EUTECTIC ALLOYS
DE69218109T2 (en) Compacted and solidified active ingredients made of aluminum alloy
DE4037959A1 (en) TITANAL ALUMINID ALLOY WITH HIGH NIOBES
DE4011129A1 (en) TANTALOUS SUPER ALLOYS
EP1213365A1 (en) Alloy on the basis of titanium aluminides
DE3530067C2 (en) Remote alloys
DE69110139T2 (en) Process for producing an article from pre-alloyed powders and article produced by this process.
CH676125A5 (en)
DE1132735B (en) Process for the production of a heat-resistant material

Legal Events

Date Code Title Description
PUAI Public reference made under article 153(3) epc to a published international application that has entered the european phase

Free format text: ORIGINAL CODE: 0009012

17P Request for examination filed

Effective date: 20000215

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): AT DE FR GB

17Q First examination report despatched

Effective date: 20000829

GRAP Despatch of communication of intention to grant a patent

Free format text: ORIGINAL CODE: EPIDOSNIGR1

GRAS Grant fee paid

Free format text: ORIGINAL CODE: EPIDOSNIGR3

GRAA (expected) grant

Free format text: ORIGINAL CODE: 0009210

AK Designated contracting states

Kind code of ref document: B1

Designated state(s): AT DE FR GB

REG Reference to a national code

Ref country code: GB

Ref legal event code: FG4D

Free format text: NOT ENGLISH

GBT Gb: translation of ep patent filed (gb section 77(6)(a)/1977)

Effective date: 20040107

REF Corresponds to:

Ref document number: 59810561

Country of ref document: DE

Date of ref document: 20040212

Kind code of ref document: P

ET Fr: translation filed
PLBE No opposition filed within time limit

Free format text: ORIGINAL CODE: 0009261

STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: NO OPPOSITION FILED WITHIN TIME LIMIT

26N No opposition filed

Effective date: 20041008

REG Reference to a national code

Ref country code: DE

Ref legal event code: R081

Ref document number: 59810561

Country of ref document: DE

Owner name: HELMHOLTZ-ZENTRUM GEESTHACHT ZENTRUM FUER MATE, DE

Free format text: FORMER OWNER: GKSS-FORSCHUNGSZENTRUM GEESTHACHT GMBH, 21502 GEESTHACHT, DE

Effective date: 20110418

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 19

REG Reference to a national code

Ref country code: FR

Ref legal event code: PLFP

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: GB

Payment date: 20170824

Year of fee payment: 20

Ref country code: DE

Payment date: 20170823

Year of fee payment: 20

Ref country code: FR

Payment date: 20170823

Year of fee payment: 20

PGFP Annual fee paid to national office [announced via postgrant information from national office to epo]

Ref country code: AT

Payment date: 20170821

Year of fee payment: 20

REG Reference to a national code

Ref country code: DE

Ref legal event code: R071

Ref document number: 59810561

Country of ref document: DE

REG Reference to a national code

Ref country code: GB

Ref legal event code: PE20

Expiry date: 20180811

REG Reference to a national code

Ref country code: AT

Ref legal event code: MK07

Ref document number: 257521

Country of ref document: AT

Kind code of ref document: T

Effective date: 20180812

PG25 Lapsed in a contracting state [announced via postgrant information from national office to epo]

Ref country code: GB

Free format text: LAPSE BECAUSE OF EXPIRATION OF PROTECTION

Effective date: 20180811