EP2283952A2 - Moule de métal pulvérulent - Google Patents

Moule de métal pulvérulent Download PDF

Info

Publication number
EP2283952A2
EP2283952A2 EP10172220A EP10172220A EP2283952A2 EP 2283952 A2 EP2283952 A2 EP 2283952A2 EP 10172220 A EP10172220 A EP 10172220A EP 10172220 A EP10172220 A EP 10172220A EP 2283952 A2 EP2283952 A2 EP 2283952A2
Authority
EP
European Patent Office
Prior art keywords
nickel
maximum
process according
molybdenum
chromium
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.)
Withdrawn
Application number
EP10172220A
Other languages
German (de)
English (en)
Other versions
EP2283952A3 (fr
Inventor
Timothy Eden Channel
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of EP2283952A2 publication Critical patent/EP2283952A2/fr
Publication of EP2283952A3 publication Critical patent/EP2283952A3/fr
Withdrawn legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C1/00Making non-ferrous alloys
    • C22C1/04Making non-ferrous alloys by powder metallurgy
    • C22C1/0433Nickel- or cobalt-based alloys
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/055Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C19/00Alloys based on nickel or cobalt
    • C22C19/03Alloys based on nickel or cobalt based on nickel
    • C22C19/05Alloys based on nickel or cobalt based on nickel with chromium
    • C22C19/051Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
    • C22C19/056Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
    • 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
    • C22F1/10Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of nickel or cobalt or alloys based thereon
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22FWORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10Processes characterised by the sequence of their steps

Definitions

  • the billet is then forged using known techniques, such as those currently utilized to produce Alloy 706 and Alloy 718 rotor forgings for large industrial turbines, but modified to take advantage of fine grain billet techniques.
  • Forging is performed at temperatures and loading conditions that allow complete filling of the finish forging die cavity, avoid fracture, and produce or retain a fine uniform grain size within the material of not larger than ASTM 8.
  • ASTM 8 ASTM 8
  • An illustrative example of an appropriate heat treatment process for the Alloy 725 entails a solution heat treatment at a temperature of about 900 °C (about 1650 °F) for approximately four hours, followed by two step aging at a temperature of about 760 °C (about 1400 °F) for approximately eight hours, then cooling at a rate of 56 °C (about 100 °F) per minute to about 620 °C (about 1150 °F) and holding for approximately eight hours, followed by air cooling.

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)
  • Forging (AREA)
  • Powder Metallurgy (AREA)
EP10172220.5A 2009-08-14 2010-08-06 Moule de métal pulvérulent Withdrawn EP2283952A3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/541,200 US20110038748A1 (en) 2009-08-14 2009-08-14 Powder metal mold

Publications (2)

Publication Number Publication Date
EP2283952A2 true EP2283952A2 (fr) 2011-02-16
EP2283952A3 EP2283952A3 (fr) 2014-03-12

Family

ID=43067051

Family Applications (1)

Application Number Title Priority Date Filing Date
EP10172220.5A Withdrawn EP2283952A3 (fr) 2009-08-14 2010-08-06 Moule de métal pulvérulent

Country Status (3)

Country Link
US (1) US20110038748A1 (fr)
EP (1) EP2283952A3 (fr)
RU (1) RU2010133879A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3327159A1 (fr) * 2016-11-29 2018-05-30 Sulzer Management AG Alliage de moulage à base de nickel, coulage et procédé de fabrication d'un rotor d'une machine tournante

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB201317757D0 (en) 2013-10-08 2013-11-20 Rolls Royce Plc A method of manufacturing an article by hot pressing and ultrasonically inspecting the article
US9902641B2 (en) * 2015-03-20 2018-02-27 Corning Incorporated Molds for shaping glass-based materials and methods for making the same
GB2545004B (en) * 2015-12-03 2019-04-03 Rolls Royce Plc Method and apparatus for machining objects

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6315846B1 (en) 1998-07-09 2001-11-13 Inco Alloys International, Inc. Heat treatment for nickel-base alloys
US6531002B1 (en) 2001-04-24 2003-03-11 General Electric Company Nickel-base superalloys and articles formed therefrom
US20070020135A1 (en) 2005-07-22 2007-01-25 General Electric Company Powder metal rotating components for turbine engines and process therefor

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4077109A (en) * 1976-05-10 1978-03-07 The International Nickel Company, Inc. Hot working of metal powders
US5640667A (en) * 1995-11-27 1997-06-17 Board Of Regents, The University Of Texas System Laser-directed fabrication of full-density metal articles using hot isostatic processing
US7985304B2 (en) * 2007-04-19 2011-07-26 Ati Properties, Inc. Nickel-base alloys and articles made therefrom
US20090142221A1 (en) * 2007-11-30 2009-06-04 Honeywell International, Inc. Engine components and methods of forming engine components

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6315846B1 (en) 1998-07-09 2001-11-13 Inco Alloys International, Inc. Heat treatment for nickel-base alloys
US6531002B1 (en) 2001-04-24 2003-03-11 General Electric Company Nickel-base superalloys and articles formed therefrom
US20070020135A1 (en) 2005-07-22 2007-01-25 General Electric Company Powder metal rotating components for turbine engines and process therefor

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP3327159A1 (fr) * 2016-11-29 2018-05-30 Sulzer Management AG Alliage de moulage à base de nickel, coulage et procédé de fabrication d'un rotor d'une machine tournante
US10787723B2 (en) 2016-11-29 2020-09-29 Sulzer Management Ag Nickel base casting alloy, casting, and method for manufacturing an impeller of a rotary machine

Also Published As

Publication number Publication date
EP2283952A3 (fr) 2014-03-12
RU2010133879A (ru) 2012-02-20
US20110038748A1 (en) 2011-02-17

Similar Documents

Publication Publication Date Title
US9322090B2 (en) Components formed by controlling grain size in forged precipitation-strengthened alloys
US20070020135A1 (en) Powder metal rotating components for turbine engines and process therefor
Clemens et al. Processing and applications of intermetallic γ‐TiAl‐based alloys
US4482398A (en) Method for refining microstructures of cast titanium articles
EP2407565B1 (fr) Procédé pour améliorer les propriétés mécaniques d'un composant
EP1649954A2 (fr) Composant à basse porosité formée par métallurgie de poudres
CN104759830B (zh) 生产性能增强的金属材料的方法
US5571345A (en) Thermomechanical processing method for achieving coarse grains in a superalloy article
KR20160046770A (ko) 단조용 Ni기 합금, 그 제조 방법 및 터빈 부품
WO2014203714A1 (fr) Alliage à base de ti-al forgé à chaud et son procédé de production
EP2283952A2 (fr) Moule de métal pulvérulent
JP2008229680A (ja) TiAl基合金成形体の製造方法
EP1779946B1 (fr) Pressage isostatique à chaud supersolvus et laminage circulaire de formes creueses de poudres
US20150167123A1 (en) Nickel-based superalloy, process therefor, and components formed therefrom
CN112359302B (zh) 一种镍基高温合金扁钢组织均匀化的方法
US7138020B2 (en) Method for reducing heat treatment residual stresses in super-solvus solutioned nickel-base superalloy articles
Rao et al. Hot Isostatic Pressing Technology for Defence and Space Applications.
RU2610658C2 (ru) Способ изготовления составных заготовок типа "диск-диск" и "диск-вал" из жаропрочных титановых и никелевых сплавов
Mashl Powder metallurgy processing by hot isostatic pressing
WO2010023210A1 (fr) Procédé de fabrication d'une pièce en superalliage à base de nickel et pièce ainsi fabriquée
Xu et al. Microstructure and properties of friction welding joint of Ti–45Al-8.5 Nb-0. 2W-0. 2B-0. 02Y alloy
US6063212A (en) Heat treated, spray formed superalloy articles and method of making the same
JP6185347B2 (ja) Ni基超耐熱合金の分塊用中間素材及びその製造方法、Ni基超耐熱合金の製造方法
Valitov et al. The effect of thermomechanical treatment conditions on the structure and properties of the granulated EP741NP nickel alloy
Bin et al. Low cycle fatigue improvement of powder metallurgy titanium alloy through thermomechanical treatment

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

AK Designated contracting states

Kind code of ref document: A2

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME RS

PUAL Search report despatched

Free format text: ORIGINAL CODE: 0009013

AK Designated contracting states

Kind code of ref document: A3

Designated state(s): AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO SE SI SK SM TR

AX Request for extension of the european patent

Extension state: BA ME RS

RIC1 Information provided on ipc code assigned before grant

Ipc: B22F 3/12 20060101AFI20140205BHEP

Ipc: B22F 3/17 20060101ALI20140205BHEP

Ipc: B22F 3/15 20060101ALI20140205BHEP

Ipc: C22C 1/04 20060101ALI20140205BHEP

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

Free format text: STATUS: THE APPLICATION IS DEEMED TO BE WITHDRAWN

18D Application deemed to be withdrawn

Effective date: 20140301