EP2396128A1 - Pièce coulée à base de nickel comprenant un corps de compensation et procédé pour la production d'une pièce de coulée à base de nickel - Google Patents

Pièce coulée à base de nickel comprenant un corps de compensation et procédé pour la production d'une pièce de coulée à base de nickel

Info

Publication number
EP2396128A1
EP2396128A1 EP10702642A EP10702642A EP2396128A1 EP 2396128 A1 EP2396128 A1 EP 2396128A1 EP 10702642 A EP10702642 A EP 10702642A EP 10702642 A EP10702642 A EP 10702642A EP 2396128 A1 EP2396128 A1 EP 2396128A1
Authority
EP
European Patent Office
Prior art keywords
nickel
cast component
base
compensating
base cast
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Withdrawn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
EP10702642A
Other languages
German (de)
English (en)
Inventor
Heinz Dallinger
Torsten-Ulf Kern
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
Original Assignee
Siemens AG
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 filed Critical Siemens AG
Priority to EP10702642A priority Critical patent/EP2396128A1/fr
Publication of EP2396128A1 publication Critical patent/EP2396128A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D29/00—Removing castings from moulds, not restricted to casting processes covered by a single main group; Removing cores; Handling ingots
    • B22D29/001—Removing cores
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22C—FOUNDRY MOULDING
    • B22C9/00—Moulds or cores; Moulding processes
    • B22C9/10—Cores; Manufacture or installation of cores
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
    • F01D25/00—Component parts, details, or accessories, not provided for in, or of interest apart from, other groups
    • F01D25/24—Casings; Casing parts, e.g. diaphragms, casing fastenings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05C—INDEXING SCHEME RELATING TO MATERIALS, MATERIAL PROPERTIES OR MATERIAL CHARACTERISTICS FOR MACHINES, ENGINES OR PUMPS OTHER THAN NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES
    • F05C2201/00—Metals
    • F05C2201/04—Heavy metals
    • F05C2201/0433—Iron group; Ferrous alloys, e.g. steel
    • F05C2201/0466—Nickel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00—Application
    • F05D2220/30—Application in turbines
    • F05D2220/31—Application in turbines in steam turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00—Manufacture
    • F05D2230/20—Manufacture essentially without removing material
    • F05D2230/21—Manufacture essentially without removing material by casting

Definitions

  • the invention relates to a nickel-base cast component and to a method for producing a nickel-based cast component, wherein the nickel-based cast component is in particular a steam turbine housing.
  • Steam turbines are used for example in steam power plants at live steam temperatures up to 620 0 C and up to a shaft power of 1000 MW. It is desirable to select the steam temperature as high as possible to increase the efficiency of the steam power plant, the steam temperature is sought up to 720 0 C.
  • areas of the housing of the steam turbine are in direct contact with the live steam, so that the use of nickel-based materials for reasons of strength is necessary for this purpose. Affected by this are in particular the high-pressure inner housing, the inner-pressure inner housing and valves of the steam turbine.
  • the components of the steam turbine up to a power range of 1000 MW such a high weight that the limits of manufacturability and manageability can be at least partially exceeded.
  • the use of the nickel-base alloys for the components of the steam turbine leads to high production costs, with the production times of these components being long.
  • the machining of the components, such as milling, broaching or drilling, due to the material of the nickel-base alloys is complicated and expensive.
  • the object of the invention is to provide a nickel-base cast component which is easier to produce by a corresponding method for producing this nickel-base cast component.
  • the nickel-based cast component according to the invention has a compensation body which is cast into the cast component and thereby covers a cavity formed in the nickel-based material, the compensation body being compressed in such a way by the nickel-based material surrounding it that after cooling of the cast component during its production by casting, the compensation body has yielded to a shrinkage of the surrounding nickel-based material, whereby the formation of cracks in the nickel-based material caused by the shrinkage is prevented.
  • the compensation body is formed such that it is a hollow body before shrinking, which collapsed after shrinking in itself and is thereby destroyed. Further, it is preferred that the compensation body is formed as a solid body, the material of which prior to casting has at least such a high porosity that the pores in the material of the solid body are compressed by the shrinkage. It is preferred that the material of the compensating body is ceramic.
  • the compensating body is formed as a hollow body, which is slotted by a parting line, on which the hollow body overlaps after shrinking.
  • the compensating body is formed as a hollow body composed of at least two shell elements, the shell elements, after shrinking at their edges, overlapping each other.
  • the compensation body is formed with a lattice structure defining the outer surface of the compensation body which is closed. Preferred dimensions of the material of the compensating body is steel.
  • the compensating body is furthermore preferably coated with a separating layer with which it is prevented that the compensating body is connected to the nickel-based material surrounding it. is bound.
  • the nickel-based material preferably comprises a solid solution hardening alloy.
  • the nickel-based cast component is preferably a steam turbine housing.
  • the cavity is a channel provided in the nickel-base cast component and / or an undercut provided in the nickel-base cast component.
  • the method according to the invention for producing a nickel-base cast component has the steps according to claims 13 or 14.
  • the compensating body is removed during post-processing of the nickel-base cast component.
  • the compensation body is cast, whereby a cavity is defined by the compensation body.
  • the balancing body is deformed or destroyed by the shrinkage process during solidification of the nickel-based material and can be easily removed thereby.
  • cracking in the nickel-base cast component is prevented during the shrinking process.
  • the compensating body is provided with a greater deformability than the nickel-based material in that the compensating body is provided with a targeted weakening of its structure.
  • the solid solution hardening alloy has the advantage that, in the event of subsequent heat treatment of the nickel-based cast component, there are no formation-related or exacerbation-related stresses at critical radii, cavities or transitions. As a result, cracking in the nickel-based cast component is prevented.
  • the inventively defined generation of the cavity in the nickel-based cast component by pouring the compensation body, taking into account the shrinkage behavior of the nickel-based material cracking in the nickel-base cast component can be prevented. If the compensating body is provided with the separating layer, then a connection of the compensating body to the nickel-based material is prevented, wherein the compensating body can be removed within the framework of a post-processing of the nickel-based cast component.
  • the nickel-based cast component according to the invention can advantageously have a complicated geometric shape, wherein the strength of the nickel-based cast component is not impaired thereby.
  • the machining time of the nickel-based cast component is reduced and its weight reduced by the provision of the cavity. As a result, larger nickel-based cast components tend to be produced with the same material use as without cavity formation.
  • FIG. 1 shows a cross section through a section of a
  • Fig. 2 to 5 cross sections of compensation bodies.
  • a steam turbine casing 1 has a cavity 2.
  • the cavity 2 is filled by a compensating body 3.
  • the compensating body 3 is a ceramic body 4, which is designed as a solid body whose material has at least such a high porosity prior to the casting of the steam turbine casing 1 that the shrinkage of the ceramic body 4 in the cavity 2 causes the pores of the body to become hollow Ceramic body 4 are compressed.
  • the balancing body 3 is shown as a steel body 5, which is formed as a hollow body 6.
  • the outer surface of the hollow body 6 is provided with a separating layer 7, with which it is prevented that the hollow body 6 is connected in the cavity 2.
  • a first embodiment of the hollow body 6 is shown, wherein the hollow body 6 is formed as a cylinder.
  • the hollow body 6 is provided with a slot which extends in the longitudinal direction of the hollow body 6, wherein at the slot 8, the hollow body 6 has a first tab 9 and a second tab 10, wherein, when the hollow body 6 is compressed in the radial direction, the first Tab 9 and the second tab 10 are arranged overlapping each other.
  • a second embodiment of the hollow body 6 is shown, which is formed from two semi-cylindrical shell elements 11, 12.
  • the shell elements 11, 12 each have an edge 13, wherein the edges 13 of the shell elements 11, 12 are radially offset from each other so that the edges 13 of the second shell member 12 radially disposed within the edges 13 of the first shell member 11 are.
  • the edges 13 of the first shell element 11 slide against each other at the edges 13 of the second shell element 12 in the circumferential direction of the hollow body 6, whereby the radial extent of the hollow body 6 is reduced.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Molds, Cores, And Manufacturing Methods Thereof (AREA)

Abstract

L'invention concerne une pièce coulée à base de nickel présentant un corps de compensation (3, 4, 5) qui est coulé dans la pièce coulée (1) et qui remplit ainsi une cavité (2) formée dans le matériau à base de nickel (1). Selon l'invention, le corps de compensation (3, 4, 5) est comprimé par le matériau à base de nickel l'entourant de telle manière que, après refroidissement de la pièce coulée (1) lors de sa fabrication par coulée, le corps de compensation (3, 4, 5) a cédé à un retrait du matériau à base de nickel l'entourant, ce qui empêche la formation de fissures dues au retrait dans le matériau à base de nickel.
EP10702642A 2009-02-10 2010-01-22 Pièce coulée à base de nickel comprenant un corps de compensation et procédé pour la production d'une pièce de coulée à base de nickel Withdrawn EP2396128A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP10702642A EP2396128A1 (fr) 2009-02-10 2010-01-22 Pièce coulée à base de nickel comprenant un corps de compensation et procédé pour la production d'une pièce de coulée à base de nickel

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
EP09001830A EP2216112A1 (fr) 2009-02-10 2009-02-10 Pièce coulée à base de nickel doté d'un corps de compensation et procédé de fabrication d'une pièce coulée à base de nickel
PCT/EP2010/050726 WO2010091931A1 (fr) 2009-02-10 2010-01-22 Pièce coulée à base de nickel comprenant un corps de compensation et procédé pour la production d'une pièce de coulée à base de nickel
EP10702642A EP2396128A1 (fr) 2009-02-10 2010-01-22 Pièce coulée à base de nickel comprenant un corps de compensation et procédé pour la production d'une pièce de coulée à base de nickel

Publications (1)

Publication Number Publication Date
EP2396128A1 true EP2396128A1 (fr) 2011-12-21

Family

ID=40792881

Family Applications (2)

Application Number Title Priority Date Filing Date
EP09001830A Withdrawn EP2216112A1 (fr) 2009-02-10 2009-02-10 Pièce coulée à base de nickel doté d'un corps de compensation et procédé de fabrication d'une pièce coulée à base de nickel
EP10702642A Withdrawn EP2396128A1 (fr) 2009-02-10 2010-01-22 Pièce coulée à base de nickel comprenant un corps de compensation et procédé pour la production d'une pièce de coulée à base de nickel

Family Applications Before (1)

Application Number Title Priority Date Filing Date
EP09001830A Withdrawn EP2216112A1 (fr) 2009-02-10 2009-02-10 Pièce coulée à base de nickel doté d'un corps de compensation et procédé de fabrication d'une pièce coulée à base de nickel

Country Status (4)

Country Link
EP (2) EP2216112A1 (fr)
JP (1) JP2012517351A (fr)
CN (1) CN102317008B (fr)
WO (1) WO2010091931A1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110842147B (zh) * 2019-11-29 2021-03-05 西安航天发动机有限公司 一种闭式叶轮熔模精密铸件流道尺寸的控制方法

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE625524C (de) * 1932-12-06 1936-02-11 Foerderanlagen Ernst Heckel M Mehrteiliger, nachgiebiger Metallkern, insbesondere fuer Stahlformgussstuecke
DE669825C (de) * 1936-02-02 1939-01-05 Press Und Walzwerk Akt Ges Kern zur Herstellung von gegossenen Hohlkoerpern
JPS6310041A (ja) * 1986-07-01 1988-01-16 Kawasaki Steel Corp 中空鋳片の鋳造方法
JPH07290188A (ja) * 1994-04-25 1995-11-07 Aisin Seiki Co Ltd ピストンの製造方法
JPH08206779A (ja) * 1995-02-08 1996-08-13 Furukawa Electric Co Ltd:The 中空部材の鋳造方法
JP3759656B2 (ja) * 1996-10-25 2006-03-29 富士重工業株式会社 複合材積層用石膏捨て型およびその製造方法
JP3295683B2 (ja) * 1997-05-02 2002-06-24 三菱自動車テクノメタル株式会社 中空軸鋳造方法
US20040261969A1 (en) * 2001-09-14 2004-12-30 Bernhard Stauder Method for producing castings, molding sand and its use for carrying out said method
US6637500B2 (en) * 2001-10-24 2003-10-28 United Technologies Corporation Cores for use in precision investment casting
US7055574B2 (en) * 2004-07-27 2006-06-06 Honeywell International Inc. Method of producing metal article having internal passage coated with a ceramic coating
JP5109115B2 (ja) * 2005-04-07 2012-12-26 国立大学法人 長崎大学 ニッケル基超合金及びその製造方法
EP1721688A1 (fr) * 2005-05-13 2006-11-15 Processi Innovativi Tecnologici, S.r.L Noyaux de fonderie et procédé pour leur fabrication
JP2007307596A (ja) * 2006-05-19 2007-11-29 Toyota Motor Corp 成形用中子およびその製造方法
US7610945B2 (en) * 2006-09-29 2009-11-03 General Electric Company Rare earth-based core constructions for casting refractory metal composites, and related processes
US7779892B2 (en) * 2007-05-09 2010-08-24 United Technologies Corporation Investment casting cores and methods
CN101229975A (zh) * 2008-01-04 2008-07-30 西北工业大学 氧化铝陶瓷型芯的制作方法以及脱芯方法

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
See references of WO2010091931A1 *

Also Published As

Publication number Publication date
JP2012517351A (ja) 2012-08-02
CN102317008B (zh) 2013-11-20
WO2010091931A1 (fr) 2010-08-19
EP2216112A1 (fr) 2010-08-11
CN102317008A (zh) 2012-01-11

Similar Documents

Publication Publication Date Title
EP2536924B1 (fr) Unité stator-couvercle frittée et déphaseur d'arbre à cames
EP2040354B1 (fr) Gaine d'un moteur de commande pour un agrégat de pompe
DE102011108957B4 (de) Verfahren zum Herstellen, Reparieren und/oder Austauschen eines Gehäuses, insbesondere eines Triebwerkgehäuses, sowie ein entsprechendes Gehäuse
EP1977102B1 (fr) Piston pour moteur a combustion interne et procede pour le produire
WO2016058900A1 (fr) Aube de turbine munie d'un module interne et procédé de fabrication d'une aube de turbine
DE102007023152A1 (de) Verfahren zur Herstellung eines Gussteils, Gussform und damit hergestelltes Gussteil
DE102007050142A1 (de) Verfahren zur Herstellung einer Blisk oder eines Blings, damit hergestelltes Bauteil und Turbinenschaufel
DE102009048665A1 (de) Turbinenschaufel und Verfahren zu deren Herstellung
DE102013219774A1 (de) Schaufel für eine Gasturbine
EP3085888A1 (fr) Carter de turbine et turbosoufflante de gaz d'echappement associee
WO2012072384A1 (fr) Turbomachine comportant une structure d'étanchéité entre des pièces tournantes et des pièces fixes ainsi que procédé de fabrication de ladite structure d'étanchéité
EP1029154B1 (fr) Carter de turbine et son procede de production
EP1815145A1 (fr) Roue de pompe a vide
DE102018209315A1 (de) Verfahren zur Herstellung eines Bauteils aus Gamma - TiAl und entsprechend hergestelltes Bauteil
AT519135B1 (de) Verfahren zur Herstellung eines Stators für einen Nockenwellenversteller
DE69110777T2 (de) Statorschaufeln für Turbinen, hergestellt aus einem thermostrukturellen Verbundmaterial.
EP1790865B1 (fr) Vilebrequin creux coulé
DE102008018875A1 (de) Auslassventil an einem Hubkolbenmotor
EP2396128A1 (fr) Pièce coulée à base de nickel comprenant un corps de compensation et procédé pour la production d'une pièce de coulée à base de nickel
EP3061561B1 (fr) Procédé de fabrication d'un composant et composant correspondant
EP2022944A1 (fr) Fixation d'aube dans une rainure circonférentielle au moyen d'une masse céramique durcissable
EP1876336A2 (fr) Composant de turbine à gaz pour groupes volatiles tout comme procédé destiné à la fabrication de composants de turbines à gaz pour groupes volatiles
DE102012201871A1 (de) Verfahren zur Herstellung eines Abgasturbolader-Turbinengehäuses mit Trennwand
DE112011100606B4 (de) Turbinenrad und Verfahren zu seiner Herstellung
EP2414129B1 (fr) Procédé de fabrication par soudage d'un composant de grande taille en fonte nodulaire en utilisant des matériaux apportés par rechargement laser et soudage par faisceau d'electron

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: 20110701

AK Designated contracting states

Kind code of ref document: A1

Designated state(s): 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

DAX Request for extension of the european patent (deleted)
RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SIEMENS AKTIENGESELLSCHAFT

17Q First examination report despatched

Effective date: 20160517

RAP1 Party data changed (applicant data changed or rights of an application transferred)

Owner name: SIEMENS AKTIENGESELLSCHAFT

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: 20170801