EP1215366A2 - Aube pour turbomachine - Google Patents

Aube pour turbomachine Download PDF

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Publication number
EP1215366A2
EP1215366A2 EP01890337A EP01890337A EP1215366A2 EP 1215366 A2 EP1215366 A2 EP 1215366A2 EP 01890337 A EP01890337 A EP 01890337A EP 01890337 A EP01890337 A EP 01890337A EP 1215366 A2 EP1215366 A2 EP 1215366A2
Authority
EP
European Patent Office
Prior art keywords
turbine blade
blade according
martensitic
raw material
hip
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
EP01890337A
Other languages
German (de)
English (en)
Other versions
EP1215366B1 (fr
EP1215366A3 (fr
Inventor
Gerhard Hackl
Gabriele Saller
Raimund Huber
Rupert Winkelmeier
Günter Schirninger
Michael Dipl. Ing. Stromberger
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.)
Voestalpine Boehler Edelstahl GmbH and Co KG
Original Assignee
Boehler Edelstahl GmbH and Co KG
Boehler Edelstahl 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 Boehler Edelstahl GmbH and Co KG, Boehler Edelstahl GmbH filed Critical Boehler Edelstahl GmbH and Co KG
Priority to SI200130995T priority Critical patent/SI1215366T1/sl
Publication of EP1215366A2 publication Critical patent/EP1215366A2/fr
Publication of EP1215366A3 publication Critical patent/EP1215366A3/fr
Application granted granted Critical
Publication of EP1215366B1 publication Critical patent/EP1215366B1/fr
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01DNON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D5/00Blades; Blade-carrying members; Heating, heat-insulating, cooling or antivibration means on the blades or the members
    • F01D5/12Blades
    • F01D5/28Selecting particular materials; Particular measures relating thereto; Measures against erosion or corrosion
    • 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
    • B22F5/00Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/04Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine blades
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C33/00Making ferrous alloys
    • C22C33/02Making ferrous alloys by powder metallurgy
    • C22C33/0257Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
    • C22C33/0278Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5%
    • C22C33/0285Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements with at least one alloying element having a minimum content above 5% with Cr, Co, or Ni having a minimum content higher than 5%
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/001Ferrous alloys, e.g. steel alloys containing N
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/18Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/42Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • CCHEMISTRY; METALLURGY
    • C22METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22CALLOYS
    • C22C38/00Ferrous alloys, e.g. steel alloys
    • C22C38/60Ferrous alloys, e.g. steel alloys containing lead, selenium, tellurium, or antimony, or more than 0.04% by weight of sulfur
    • 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
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • B22F2003/247Removing material: carving, cleaning, grinding, hobbing, honing, lapping, polishing, milling, shaving, skiving, turning the surface
    • 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
    • B22F3/00Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/24After-treatment of workpieces or articles
    • B22F2003/248Thermal after-treatment
    • 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
    • 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
    • B22F2999/00Aspects linked to processes or compositions used in powder metallurgy

Definitions

  • the invention relates to a turbine blade for steam or gas turbines as well as compressors, which shovel made of primary material by cutting Machining is created and thermally treated or remunerated.
  • Turbine blades with one for the respective use in the turbines and Compressors required shape can be made according to the drop forging process by machining from a billet or by forging Raw form with a subsequent chip removal can be created. It will Pre-material from alloys solidified in forms by forging and / or Rolls produced and optionally heat-treated for further processing. It is known to use casting blocks, continuous casting booms or remelting blocks for the To use primary material production.
  • Turbines for two-phase generators have a number of revolutions of 3000 or 3600 min- 1 , which results in considerable stresses on the rotor blades when the same is high.
  • the high availability and safety of the Thermal engine turbine blades required the highest possible on the one hand Have material homogeneity and on the other hand a low tendency to creep Have material at operating temperature.
  • the aim of the invention is To create turbine blades that cut at the flow surfaces are processed and meet the above requirements.
  • PM powder metallurgy
  • HIP hot isostatic pressing
  • the advantages achieved with the invention are essentially that a, after the powder metallurgy (PM) process is essentially free of segregation and a high material homogeneity from it manufactured turbine blade ensures. Even with a high degree of deformation or a large longitudinal stretch of the material, the homogeneity remains, in particular obtained across the cross section, causing no tendency to a There is bending of the free blade ends.
  • PM powder metallurgy
  • the primary material after the hot isostatic presses (HIP-en), preferably in a near-final dimension Form, not deformed (as-HIP-ed) is machined can be a special one economic manufacture of the turbine blade can be achieved.
  • HIP-en preferably in a near-final dimension Form
  • AS-HIPED "condition, the desired mechanical material properties are not may have, it has been found that such a blade partially even has improved quality features.
  • the PM raw material is made of an iron-based alloy, which solidifies without ledeburit.
  • the PM process is especially for Alloys were developed which solidify primary precipitates, for example carbides, and form this process in case of ledeburit freezing Steel cannot be effective in terms of quality, it has surprisingly been found that thus a significant increase in the quality of the blade alloy material is achievable.
  • a turbine blade for high thermal and mechanical, in particular dynamic loads and a lack of tendency towards end bending in practical use can be created if the PM primary material is made of a martensitic chrome steel with a composition of in% by weight.
  • Manganese (Mn) to 2.0 Sulfur (S) to 0.49 (Mn / S) MIN 2.0 Tungsten (W) to 2.5 Nickel (Ni) MAX 3.0 Niobium (Nb) to 0.12 Boron (B) up to 0.01 Iron (Fe) rest as well as production-related impurities and accompanying elements.
  • the synergetic effect of the alloying elements of the PM material is beneficial for turbine blades in several ways.
  • the machinability of the material is significantly improved; on the other hand, if a certain Mn / S ratio is maintained, the mechanical properties remain unchanged at a high level even with frequent operating cycles.
  • the PM material is made of a soft martensitic or nickel martensitic steel with a composition of in% by weight.
  • a chromium content is metallurgical or manufacturing technology, which is at least 14% by weight to nitrogen, which has a beneficial effect on the Exercises material properties to bring in solution.
  • FIG. 3 A test is shown schematically in FIG. 3.
  • the sample fixture took place in a holder 3, with a clamping piece 22 of a sample 2 in this was fixed.
  • a respective one was carried out with different heating speeds Heating sample 2, which is then at temperatures between 300 ° C and 550 ° C were kept. The deviation of the was measured Clamping opposite sample end.
  • test specimens made from conventional primary material i.e. in blocks solidified steels and subsequent reshaping of the blocks Bends with higher rates of temperature change and increase larger ingot cross sections.

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • General Engineering & Computer Science (AREA)
  • Manufacturing & Machinery (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Powder Metallurgy (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
EP01890337A 2000-12-15 2001-12-12 Aube de turbine Expired - Lifetime EP1215366B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
SI200130995T SI1215366T1 (sl) 2000-12-15 2001-12-12 Turbinska lopatica

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
AT0209600A AT411028B (de) 2000-12-15 2000-12-15 Turbinenschaufel für dampf- oder gasturbinen sowie verdichter
AT209600 2000-12-15

Publications (3)

Publication Number Publication Date
EP1215366A2 true EP1215366A2 (fr) 2002-06-19
EP1215366A3 EP1215366A3 (fr) 2004-10-13
EP1215366B1 EP1215366B1 (fr) 2011-05-18

Family

ID=3689836

Family Applications (1)

Application Number Title Priority Date Filing Date
EP01890337A Expired - Lifetime EP1215366B1 (fr) 2000-12-15 2001-12-12 Aube de turbine

Country Status (6)

Country Link
EP (1) EP1215366B1 (fr)
AT (2) AT411028B (fr)
DK (1) DK1215366T3 (fr)
ES (1) ES2363928T3 (fr)
PT (1) PT1215366E (fr)
SI (1) SI1215366T1 (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2159295A3 (fr) * 2008-09-01 2011-04-20 MINEBEA Co., Ltd. Acier inoxydable martensitique et palier à roulement l'utilisant
WO2012104347A1 (fr) * 2011-02-04 2012-08-09 Siemens Aktiengesellschaft Roue à aubes de turbocompresseur et son procédé de fabrication

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102020131031A1 (de) 2020-11-24 2022-05-25 Otto-Von-Guericke-Universität Magdeburg Martensitische Stahllegierung mit optimierter Härte und Korrosionsbeständigkeit

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB718382A (en) * 1950-11-25 1954-11-10 Sintercast Corp America Powder metallurgical method of shaping articles from high melting metals
DE1238676B (de) * 1962-05-31 1967-04-13 Gen Electric Verwendung einer Chromstahllegierung fuer Schmiedestuecke
NO131944C (fr) * 1970-12-28 1975-08-27 Kobe Steel Ltd
GB1582651A (en) * 1977-04-01 1981-01-14 Rolls Royce Products formed by powder metallurgy and a method therefore
WO1982000158A1 (fr) * 1980-07-08 1982-01-21 Salk Inst For Biological Studi Systeme d'amplification des genes eucaryotiques
JPS58217664A (ja) * 1982-06-11 1983-12-17 Toshiba Corp 蒸気タ−ビン動翼
US5584948A (en) * 1994-09-19 1996-12-17 General Electric Company Method for reducing thermally induced porosity in a polycrystalline nickel-base superalloy article
GB2315441B (en) * 1996-07-20 2000-07-12 Special Melted Products Limite Production of metal billets

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2159295A3 (fr) * 2008-09-01 2011-04-20 MINEBEA Co., Ltd. Acier inoxydable martensitique et palier à roulement l'utilisant
US8591673B2 (en) 2008-09-01 2013-11-26 Minebea Co., Ltd. Martensitic stainless steel and antifriction bearing using the same
WO2012104347A1 (fr) * 2011-02-04 2012-08-09 Siemens Aktiengesellschaft Roue à aubes de turbocompresseur et son procédé de fabrication
EP2652268B1 (fr) 2011-02-04 2015-04-01 Siemens Aktiengesellschaft Rotor de turbocompresseur et procédé de fabrication associé

Also Published As

Publication number Publication date
SI1215366T1 (sl) 2011-08-31
DK1215366T3 (da) 2011-09-12
ATE510107T1 (de) 2011-06-15
EP1215366B1 (fr) 2011-05-18
AT411028B (de) 2003-09-25
ATA20962000A (de) 2003-02-15
ES2363928T3 (es) 2011-08-19
PT1215366E (pt) 2011-06-07
EP1215366A3 (fr) 2004-10-13

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