EP2716779A1 - Alliage métallique avec particules quasi-cristallines, poudre, composant, procédé et système de couche - Google Patents

Alliage métallique avec particules quasi-cristallines, poudre, composant, procédé et système de couche Download PDF

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Publication number
EP2716779A1
EP2716779A1 EP12187151.1A EP12187151A EP2716779A1 EP 2716779 A1 EP2716779 A1 EP 2716779A1 EP 12187151 A EP12187151 A EP 12187151A EP 2716779 A1 EP2716779 A1 EP 2716779A1
Authority
EP
European Patent Office
Prior art keywords
component
quasi
metal
crystal particles
particles
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Withdrawn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
EP12187151.1A
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German (de)
English (en)
Inventor
Michael Clossen-Von Lanken Schulz
Kai Kadau
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.)
Siemens AG
Siemens Corp
Original Assignee
Siemens AG
Siemens Corp
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 Siemens AG, Siemens Corp filed Critical Siemens AG
Priority to EP12187151.1A priority Critical patent/EP2716779A1/fr
Priority to PCT/EP2013/070253 priority patent/WO2014053419A2/fr
Publication of EP2716779A1 publication Critical patent/EP2716779A1/fr
Withdrawn legal-status Critical Current

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    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/03—Alloys based on nickel or cobalt based on nickel
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C19/00—Alloys based on nickel or cobalt
    • C22C19/07—Alloys based on nickel or cobalt based on cobalt
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C21/00—Alloys based on aluminium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C30/00—Alloys containing less than 50% by weight of each constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C30/00—Alloys containing less than 50% by weight of each constituent
    • C22C30/02—Alloys containing less than 50% by weight of each constituent containing copper
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C45/00—Amorphous alloys
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C45/00—Amorphous alloys
    • C22C45/001—Amorphous alloys with Cu as the major constituent
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C45/00—Amorphous alloys
    • C22C45/04—Amorphous alloys with nickel or cobalt as the major constituent

Definitions

  • the invention relates to alloys and metallic components comprising particles of quasicrystals, to a method of production and to coating systems.
  • Particle reinforcement is a known mechanism for improving the mechanical properties of metals or metallic alloys.
  • the prior art is to achieve such particle reinforcement by ceramic particles, which can also achieve an increase in strength due to the different coefficients of thermal expansion and the stresses initiated thereby, but can also initiate cracks if the thermal stresses become too great, in particular if the component is used with such an alloy at high temperatures and is exposed to thermal temperature gradients.
  • the object is achieved by an alloy according to claim 1, a powder according to claim 5, a component according to claim 6 and a method according to claim 10 or 13 and a layer system according to claim 14, 15.
  • QKP quasi-crystal particles
  • Quasicrystals have properties that are adjustable between those of metals and ceramics.
  • the thermal expansion coefficient may be close to metals, which minimizes thermal stresses between metal matrix and QKP during operation.
  • the QCPs stabilize the metallic microstructure and help the material to reach higher failure voltages. Abrasive properties also improve with the introduction of QKP. Since quasicrystals have poor heat conduction, near-surface QCPs can also be used for thermal insulation, although this does not have to be understood as a layer with its problem of spalling, but rather as a gradual concentration gradient of the QCP.
  • FIG. 1 schematically a component 1, 120, 130 is shown, which was made of a metallic alloy or metal.
  • the component 1, 120, 130 can also be made of a powder comprising a metal alloy with quasi-crystals.
  • the quasi-crystal particles are present only in the near-surface region 7 of the component 1 ', 120, 130, when the greatest stresses or strains occur there.
  • the quasi-crystal particle (QKP) has. These may be mechanically more heavily loaded areas of the component. For turbine blades 120, 130 this is eg the leading edge.
  • the elements can replace Ni with Pd or Ru or / and Co with Fe or Mn.
  • the listed QC types offer good flexibility to realize the proposed particle-based quasicrystalline layer systems and to adapt them to the individual requirements of the component.
  • FIG. 4 shows a perspective view of a blade 120 or guide vane 130 of a turbomachine, which extends along a longitudinal axis 121.
  • the turbomachine may be a gas turbine of an aircraft or a power plant for power generation, a steam turbine or a compressor.
  • the blade 120, 130 has along the longitudinal axis 121 consecutively a fastening region 400, a blade platform 403 adjacent thereto and an airfoil 406 and a blade tip 415.
  • the blade 130 may have at its blade tip 415 another platform (not shown).
  • a blade root 183 is formed, which serves for attachment of the blades 120, 130 to a shaft or a disc (not shown).
  • the blade root 183 is designed, for example, as a hammer head. Other designs as Christmas tree or Schwalbenschwanzfuß are possible.
  • the blade 120, 130 has a leading edge 409 and a trailing edge 412 for a medium flowing past the airfoil 406.
  • blades 120, 130 for example, solid metallic materials, in particular superalloys, are used in all regions 400, 403, 406 of the blade 120, 130.
  • Such superalloys are for example from EP 1 204 776 B1 .
  • EP 1 306 454 .
  • the blade 120, 130 can be made by a casting process, also by directional solidification, by a forging process, by a milling process or combinations thereof.
  • the blades 120, 130 may have coatings against corrosion or oxidation, e.g. M is at least one element of the group iron (Fe), cobalt (Co), nickel (Ni), X is an active element and stands for yttrium (Y) and / or silicon and / or at least one element of the rare ones Earth, or hafnium (Hf)).
  • M is at least one element of the group iron (Fe), cobalt (Co), nickel (Ni)
  • X is an active element and stands for yttrium (Y) and / or silicon and / or at least one element of the rare ones Earth, or hafnium (Hf)).
  • Such alloys are known from the EP 0 486 489 B1 .
  • EP 0 412 397 B1 or EP 1 306 454 A1 The density is preferably 95% of the theoretical density.
  • the layer composition comprises Co-30Ni-28Cr-8Al-0.6Y-0.7Si or Co-28Ni-24Cr-10Al-0.6Y.
  • nickel-based protective layers such as Ni-10Cr-12Al-0.6Y-3Re or Ni-12Co-21Cr-11Al-0.4Y-2Re or Ni-25Co-17Cr-10Al-0.4Y-1 are also preferably used , 5RE.
  • thermal barrier coating which is preferably the outermost layer, and consists for example of ZrO 2 , Y 2 O 3 -ZrO 2 , ie it is not, partially or completely stabilized by yttria and / or calcium oxide and / or magnesium oxide.
  • the thermal barrier coating covers the entire MCrAlX layer.
  • suitable coating processes such as electron beam evaporation (EB-PVD)
  • stalk-shaped grains are produced in the thermal barrier coating.
  • Other coating methods are conceivable, for example atmospheric plasma spraying (APS), LPPS, VPS or CVD.
  • the thermal barrier coating may have porous, micro- or macro-cracked grains for better thermal shock resistance.
  • the thermal barrier coating is therefore preferably more porous than the MCrAlX layer.
  • Refurbishment means that components 120, 130 may have to be freed of protective layers after use (eg by sandblasting). This is followed by removal of the corrosion and / or oxidation layers or products. Optionally, even cracks in the component 120, 130 are repaired. Thereafter, a recoating occurs of the component 120, 130 and a renewed use of the component 120, 130.
  • the blade 120, 130 may be hollow or solid. If the blade 120, 130 is to be cooled, it is hollow and may still film cooling holes 418 (indicated by dashed lines) on.

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  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Powder Metallurgy (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Other Surface Treatments For Metallic Materials (AREA)
EP12187151.1A 2012-10-04 2012-10-04 Alliage métallique avec particules quasi-cristallines, poudre, composant, procédé et système de couche Withdrawn EP2716779A1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
EP12187151.1A EP2716779A1 (fr) 2012-10-04 2012-10-04 Alliage métallique avec particules quasi-cristallines, poudre, composant, procédé et système de couche
PCT/EP2013/070253 WO2014053419A2 (fr) 2012-10-04 2013-09-27 Alliage métalique à particules de quasi-cristaux, poudre, élément structural, procédé et système multicouche

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP12187151.1A EP2716779A1 (fr) 2012-10-04 2012-10-04 Alliage métallique avec particules quasi-cristallines, poudre, composant, procédé et système de couche

Publications (1)

Publication Number Publication Date
EP2716779A1 true EP2716779A1 (fr) 2014-04-09

Family

ID=47010321

Family Applications (1)

Application Number Title Priority Date Filing Date
EP12187151.1A Withdrawn EP2716779A1 (fr) 2012-10-04 2012-10-04 Alliage métallique avec particules quasi-cristallines, poudre, composant, procédé et système de couche

Country Status (2)

Country Link
EP (1) EP2716779A1 (fr)
WO (1) WO2014053419A2 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014067855A3 (fr) * 2012-10-30 2014-09-04 Siemens Aktiengesellschaft Ailette de turbine et procede de fabrication d'une ailette de turbine présentant une dureté de surface élevée
CN104167234A (zh) * 2014-08-29 2014-11-26 孙金福 一种铜包铝镁合金线

Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0486489B1 (fr) 1989-08-10 1994-11-02 Siemens Aktiengesellschaft Revetement anticorrosion resistant aux temperatures elevees, notamment pour elements de turbines a gaz
EP0412397B1 (fr) 1989-08-10 1998-03-25 Siemens Aktiengesellschaft Revêtement protecteur contenant du rhénium possédant une résistance plus grande à la corrosion et l'oxydation
EP0892090A1 (fr) 1997-02-24 1999-01-20 Sulzer Innotec Ag Procédé de fabrication de structure smonocristallines
EP0786017B1 (fr) 1994-10-14 1999-03-24 Siemens Aktiengesellschaft Couche de protection de pieces contre la corrosion, l'oxydation et les contraintes thermiques excessives, et son procede de production
WO1999067435A1 (fr) 1998-06-23 1999-12-29 Siemens Aktiengesellschaft Alliage a solidification directionnelle a resistance transversale a la rupture amelioree
US6024792A (en) 1997-02-24 2000-02-15 Sulzer Innotec Ag Method for producing monocrystalline structures
WO2000044949A1 (fr) 1999-01-28 2000-08-03 Siemens Aktiengesellschaft Superalliage a base de nickel presentant une bonne usinabilite
EP1306454A1 (fr) 2001-10-24 2003-05-02 Siemens Aktiengesellschaft Revêtement protecteur contenant du rhénium pour la protection d'un élément contre l'oxydation et la corrosion aux températures élevées
EP1319729A1 (fr) 2001-12-13 2003-06-18 Siemens Aktiengesellschaft Pièce résistante à des températures élevées réalisé en superalliage polycristallin ou monocristallin à base de nickel
EP1204776B1 (fr) 1999-07-29 2004-06-02 Siemens Aktiengesellschaft Piece resistant a des temperatures elevees et son procede de production

Patent Citations (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP0486489B1 (fr) 1989-08-10 1994-11-02 Siemens Aktiengesellschaft Revetement anticorrosion resistant aux temperatures elevees, notamment pour elements de turbines a gaz
EP0412397B1 (fr) 1989-08-10 1998-03-25 Siemens Aktiengesellschaft Revêtement protecteur contenant du rhénium possédant une résistance plus grande à la corrosion et l'oxydation
EP0786017B1 (fr) 1994-10-14 1999-03-24 Siemens Aktiengesellschaft Couche de protection de pieces contre la corrosion, l'oxydation et les contraintes thermiques excessives, et son procede de production
EP0892090A1 (fr) 1997-02-24 1999-01-20 Sulzer Innotec Ag Procédé de fabrication de structure smonocristallines
US6024792A (en) 1997-02-24 2000-02-15 Sulzer Innotec Ag Method for producing monocrystalline structures
WO1999067435A1 (fr) 1998-06-23 1999-12-29 Siemens Aktiengesellschaft Alliage a solidification directionnelle a resistance transversale a la rupture amelioree
WO2000044949A1 (fr) 1999-01-28 2000-08-03 Siemens Aktiengesellschaft Superalliage a base de nickel presentant une bonne usinabilite
EP1204776B1 (fr) 1999-07-29 2004-06-02 Siemens Aktiengesellschaft Piece resistant a des temperatures elevees et son procede de production
EP1306454A1 (fr) 2001-10-24 2003-05-02 Siemens Aktiengesellschaft Revêtement protecteur contenant du rhénium pour la protection d'un élément contre l'oxydation et la corrosion aux températures élevées
EP1319729A1 (fr) 2001-12-13 2003-06-18 Siemens Aktiengesellschaft Pièce résistante à des températures élevées réalisé en superalliage polycristallin ou monocristallin à base de nickel

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
D. SHECHTMAN ET AL: "Metallic Phase with Long-Range Orientational Order and No Translational Symmetry", PHYSICAL REVIEW LETTERS, vol. 53, no. 20, 1 November 1984 (1984-11-01), pages 1951 - 1953, XP055059884, ISSN: 0031-9007, DOI: 10.1103/PhysRevLett.53.1951 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2014067855A3 (fr) * 2012-10-30 2014-09-04 Siemens Aktiengesellschaft Ailette de turbine et procede de fabrication d'une ailette de turbine présentant une dureté de surface élevée
CN104167234A (zh) * 2014-08-29 2014-11-26 孙金福 一种铜包铝镁合金线

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Publication number Publication date
WO2014053419A2 (fr) 2014-04-10
WO2014053419A3 (fr) 2014-08-07

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