EP2227571A2 - Matériau pour composant de turbine à gaz, procédé de fabrication d'un composant de turbine à gaz et composant de turbine à gaz - Google Patents

Matériau pour composant de turbine à gaz, procédé de fabrication d'un composant de turbine à gaz et composant de turbine à gaz

Info

Publication number
EP2227571A2
EP2227571A2 EP08841961A EP08841961A EP2227571A2 EP 2227571 A2 EP2227571 A2 EP 2227571A2 EP 08841961 A EP08841961 A EP 08841961A EP 08841961 A EP08841961 A EP 08841961A EP 2227571 A2 EP2227571 A2 EP 2227571A2
Authority
EP
European Patent Office
Prior art keywords
phase
gas turbine
temperature
turbine component
material according
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
EP08841961A
Other languages
German (de)
English (en)
Other versions
EP2227571B1 (fr
Inventor
Wilfried Smarsly
Helmut Clemens
Volker Guether
Sascha Kremmer
Andreas Otto
Harald Chladil
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.)
Montanuniversitaet Leoben
Voestalpine Boehler Aerospace GmbH and Co KG
GfE Metalle und Materialien GmbH
MTU Aero Engines AG
Original Assignee
Montanuniversitaet Leoben
Voestalpine Boehler Aerospace GmbH and Co KG
GfE Metalle und Materialien GmbH
MTU Aero Engines 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 Montanuniversitaet Leoben, Voestalpine Boehler Aerospace GmbH and Co KG, GfE Metalle und Materialien GmbH, MTU Aero Engines GmbH filed Critical Montanuniversitaet Leoben
Priority to PL08841961T priority Critical patent/PL2227571T3/pl
Publication of EP2227571A2 publication Critical patent/EP2227571A2/fr
Application granted granted Critical
Publication of EP2227571B1 publication Critical patent/EP2227571B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C14/00Alloys based on titanium
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22FCHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
    • C22F1/00Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
    • C22F1/16Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of other metals or alloys based thereon
    • C22F1/18High-melting or refractory metals or alloys based thereon
    • C22F1/183High-melting or refractory metals or alloys based thereon of titanium or alloys based thereon

Definitions

  • the proportion of cubic body-centered ß / B2-Ti phase in the thermodynamic equilibrium of the material according to the invention is less than 5 vol .-% in the room temperature. In the area of the eutectoid temperature, the proportion of cubic body-centered ⁇ / B2-Ti phase is greater than 10% by volume.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Crystallography & Structural Chemistry (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Forging (AREA)

Abstract

L'invention concerne un matériau pour un composant de turbine à gaz, plus précisément un matériau d'alliage à base de titane et d'aluminium, contenant au moins du titane et de l'aluminium. Le matériau présente, a) aux alentours de la température ambiante, la phase B2-Ti, la phase a2-Ti3Al et la phase ?-TiAl, la phase B2-Ti représentant au maximum 5 % en vol., et b) aux alentours de la température eutectoïde, la phase ß-Ti, la phase a2-Ti3Al et la phase ?-TiAl, la phase ß-Ti représentant au minimum 10 % en vol.
EP08841961.9A 2007-10-27 2008-10-18 Matériau pour composant de turbine à gaz, procédé de fabrication d'un composant de turbine à gaz et composant de turbine à gaz Active EP2227571B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
PL08841961T PL2227571T3 (pl) 2007-10-27 2008-10-18 Materiał na podzespół turbiny gazowej, sposób produkcji podzespołu turbiny gazowej i podzespół turbiny gazowej

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102007051499A DE102007051499A1 (de) 2007-10-27 2007-10-27 Werkstoff für ein Gasturbinenbauteil, Verfahren zur Herstellung eines Gasturbinenbauteils sowie Gasturbinenbauteil
PCT/DE2008/001702 WO2009052792A2 (fr) 2007-10-27 2008-10-18 Matériau pour composant de turbine à gaz, procédé de fabrication d'un composant de turbine à gaz et composant de turbine à gaz

Publications (2)

Publication Number Publication Date
EP2227571A2 true EP2227571A2 (fr) 2010-09-15
EP2227571B1 EP2227571B1 (fr) 2015-09-02

Family

ID=40227637

Family Applications (1)

Application Number Title Priority Date Filing Date
EP08841961.9A Active EP2227571B1 (fr) 2007-10-27 2008-10-18 Matériau pour composant de turbine à gaz, procédé de fabrication d'un composant de turbine à gaz et composant de turbine à gaz

Country Status (8)

Country Link
US (1) US8888461B2 (fr)
EP (1) EP2227571B1 (fr)
JP (1) JP5926886B2 (fr)
CA (1) CA2703906C (fr)
DE (1) DE102007051499A1 (fr)
ES (1) ES2548243T3 (fr)
PL (1) PL2227571T3 (fr)
WO (1) WO2009052792A2 (fr)

Families Citing this family (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AT509768B1 (de) * 2010-05-12 2012-04-15 Boehler Schmiedetechnik Gmbh & Co Kg Verfahren zur herstellung eines bauteiles und bauteile aus einer titan-aluminium-basislegierung
US8876992B2 (en) * 2010-08-30 2014-11-04 United Technologies Corporation Process and system for fabricating gamma TiAl turbine engine components
WO2012041276A2 (fr) * 2010-09-22 2012-04-05 Mtu Aero Engines Gmbh Alliage tial résistant à la chaleur
EP2505780B1 (fr) * 2011-04-01 2016-05-11 MTU Aero Engines GmbH Agencement d'aubes pour une turbomachine
DE102011110740B4 (de) * 2011-08-11 2017-01-19 MTU Aero Engines AG Verfahren zur Herstellung geschmiedeter TiAl-Bauteile
US20130084190A1 (en) * 2011-09-30 2013-04-04 General Electric Company Titanium aluminide articles with improved surface finish and methods for their manufacture
EP2620517A1 (fr) * 2012-01-25 2013-07-31 MTU Aero Engines GmbH Alliage TiAl thermostable
ES2532582T3 (es) * 2012-08-09 2015-03-30 Mtu Aero Engines Gmbh Método para fabricar un segmento de corona de álabes de TiAl para una turbina de gas, así como un correspondiente segmento de corona de álabes
FR2997884B3 (fr) 2012-11-09 2015-06-26 Mecachrome France Procede et dispositif de fabrication d'aubes de turbines.
EP2762684B1 (fr) * 2013-01-30 2021-03-03 MTU Aero Engines AG Support d'étanchéité à base d'aluminure de titane pour une turbomachine
WO2014149122A2 (fr) * 2013-03-15 2014-09-25 United Technologies Corporation Procédé permettant de fabriquer un composant de turbine en aluminure de titane gamma
ES2747155T3 (es) 2013-09-20 2020-03-10 MTU Aero Engines AG Aleación de TiAl resistente a la fluencia
DE102013020460A1 (de) 2013-12-06 2015-06-11 Hanseatische Waren Handelsgesellschaft Mbh & Co. Kg Verfahren zur Herstellung von TiAl-Bauteilen
US10240608B2 (en) 2014-02-05 2019-03-26 Borgwarner Inc. TiAl alloy, in particular for turbocharger applications, turbocharger component, turbocharger and method for producing the TiAl alloy
US9963977B2 (en) 2014-09-29 2018-05-08 United Technologies Corporation Advanced gamma TiAl components
DE102015103422B3 (de) 2015-03-09 2016-07-14 LEISTRITZ Turbinentechnik GmbH Verfahren zur Herstellung eines hochbelastbaren Bauteils aus einer Alpha+Gamma-Titanaluminid-Legierung für Kolbenmaschinen und Gasturbinen, insbesondere Flugtriebwerke
DE102015115683A1 (de) * 2015-09-17 2017-03-23 LEISTRITZ Turbinentechnik GmbH Verfahren zur Herstellung einer Vorform aus einer Alpha+Gamma-Titanaluminid-Legierung zur Herstellung eines hochbelastbaren Bauteils für Kolbenmaschinen und Gasturbinen, insbesondere Flugtriebwerke
RU2614294C1 (ru) * 2016-04-04 2017-03-24 Федеральное государственное бюджетное образовательное учреждение высшего образования "Рыбинский государственный авиационный технический университет имени П.А. Соловьева" Способ изготовления штамповок лопаток из титановых сплавов
EP3249064A1 (fr) 2016-05-23 2017-11-29 MTU Aero Engines GmbH Fabrication additive de composants haute temperature en tial
EP3269838B1 (fr) 2016-07-12 2021-09-01 MTU Aero Engines AG Alliage tial thermostable, procédé de production d'un composant constitué d'un alliage tial correspondant, composant constitué d'un alliage tial correspondant
EP3326746A1 (fr) * 2016-11-25 2018-05-30 Helmholtz-Zentrum Geesthacht Zentrum für Material- und Küstenforschung GmbH Procédé pour assembler et/ou réparer des substrats d'alliages d'aluminure de titane
CN112410698B (zh) * 2020-11-03 2021-11-02 中国航发北京航空材料研究院 一种三相Ti2AlNb合金多层次组织均匀性控制方法
US20240043978A1 (en) 2021-04-16 2024-02-08 Kabushiki Kaisha Kobe Seiko Sho (Kobe Steel, Ltd.) Tial alloy for forging, tial alloy material, and method for producing tial alloy material

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2546551B2 (ja) * 1991-01-31 1996-10-23 新日本製鐵株式会社 γ及びβ二相TiAl基金属間化合物合金及びその製造方法
JPH06116692A (ja) * 1992-10-05 1994-04-26 Honda Motor Co Ltd 高温強度の優れたTiAl系金属間化合物およびその製造方法
WO1996012827A1 (fr) * 1994-10-25 1996-05-02 Mitsubishi Jukogyo Kabushiki Kaisha ALLIAGE A BASE DE COMPOSE INTERMETALLIQUE DE TiAl ET PROCEDE DE FABRICATION DUDIT ALLIAGE
USH1659H (en) * 1995-05-08 1997-07-01 The United States Of America As Represented By The Secretary Of The Air Force Method for heat treating titanium aluminide alloys
JP3388970B2 (ja) * 1995-12-26 2003-03-24 三菱重工業株式会社 TiAl系金属間化合物基合金
JP3492118B2 (ja) * 1996-10-28 2004-02-03 三菱重工業株式会社 TiAl金属間化合物基合金
US6174387B1 (en) * 1998-09-14 2001-01-16 Alliedsignal, Inc. Creep resistant gamma titanium aluminide alloy
DE102004056582B4 (de) * 2004-11-23 2008-06-26 Gkss-Forschungszentrum Geesthacht Gmbh Legierung auf der Basis von Titanaluminiden

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2009052792A2 *

Also Published As

Publication number Publication date
DE102007051499A1 (de) 2009-04-30
ES2548243T3 (es) 2015-10-15
PL2227571T3 (pl) 2016-02-29
WO2009052792A2 (fr) 2009-04-30
US20110189026A1 (en) 2011-08-04
CA2703906A1 (fr) 2009-04-30
WO2009052792A3 (fr) 2009-09-03
WO2009052792A9 (fr) 2009-11-05
CA2703906C (fr) 2016-07-19
JP5926886B2 (ja) 2016-05-25
US8888461B2 (en) 2014-11-18
EP2227571B1 (fr) 2015-09-02
JP2011502213A (ja) 2011-01-20
WO2009052792A8 (fr) 2009-07-30

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