US20150231690A1 - Method for producing a turbine rotor - Google Patents

Method for producing a turbine rotor Download PDF

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Publication number
US20150231690A1
US20150231690A1 US14/181,878 US201414181878A US2015231690A1 US 20150231690 A1 US20150231690 A1 US 20150231690A1 US 201414181878 A US201414181878 A US 201414181878A US 2015231690 A1 US2015231690 A1 US 2015231690A1
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US
United States
Prior art keywords
rotor
existing
intended
steam turbine
machined
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.)
Abandoned
Application number
US14/181,878
Inventor
Ralf Bell
Gary Griffin
Jeremy Marshall
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 US14/181,878 priority Critical patent/US20150231690A1/en
Assigned to SIEMENS AKTIENGESELLSCHAFT reassignment SIEMENS AKTIENGESELLSCHAFT ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BELL, RALF
Assigned to SIEMENS ENERGY, INC. reassignment SIEMENS ENERGY, INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: GRIFFIN, GARY, MARSHALL, JEREMY
Assigned to SIEMENS AKTIENGESELLSCHAFT reassignment SIEMENS AKTIENGESELLSCHAFT ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: SIEMENS ENERGY, INC.
Priority to EP15700388.0A priority patent/EP3071365A1/en
Priority to PCT/EP2015/050624 priority patent/WO2015121016A1/en
Priority to RU2016133502A priority patent/RU2016133502A/en
Publication of US20150231690A1 publication Critical patent/US20150231690A1/en
Priority to US15/358,101 priority patent/US20170074105A1/en
Abandoned legal-status Critical Current

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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B21MECHANICAL METAL-WORKING WITHOUT ESSENTIALLY REMOVING MATERIAL; PUNCHING METAL
    • B21KMAKING FORGED OR PRESSED METAL PRODUCTS, e.g. HORSE-SHOES, RIVETS, BOLTS OR WHEELS
    • B21K3/00Making engine or like machine parts not covered by sub-groups of B21K1/00; Making propellers or the like
    • 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
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/06Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections
    • F01D5/063Welded rotors
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K31/00Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups
    • B23K31/02Processes relevant to this subclass, specially adapted for particular articles or purposes, but not covered by only one of the preceding main groups relating to soldering or welding
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P15/00Making specific metal objects by operations not covered by a single other subclass or a group in this subclass
    • B23P15/006Making specific metal objects by operations not covered by a single other subclass or a group in this subclass turbine wheels
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23PMETAL-WORKING NOT OTHERWISE PROVIDED FOR; COMBINED OPERATIONS; UNIVERSAL MACHINE TOOLS
    • B23P6/00Restoring or reconditioning objects
    • B23P6/002Repairing turbine components, e.g. moving or stationary blades, rotors
    • 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
    • F01D5/005Repairing methods or devices
    • 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
    • F01D5/02Blade-carrying members, e.g. rotors
    • F01D5/026Shaft to shaft connections
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K2101/00Articles made by soldering, welding or cutting
    • B23K2101/001Turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2220/00Application
    • F05D2220/30Application in turbines
    • F05D2220/31Application in turbines in steam turbines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/10Manufacture by removing material
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/20Manufacture essentially without removing material
    • F05D2230/23Manufacture essentially without removing material by permanently joining parts together
    • F05D2230/232Manufacture essentially without removing material by permanently joining parts together by welding
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05DINDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2230/00Manufacture
    • F05D2230/30Manufacture with deposition of material
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49316Impeller making
    • Y10T29/4932Turbomachine making
    • Y10T29/49321Assembling individual fluid flow interacting members, e.g., blades, vanes, buckets, on rotary support member

Definitions

  • the claimed invention refers to a method for producing a turbine rotor, in particular a steam turbine rotor.
  • Steam turbine rotors are large components manufactured from forged steel ingots.
  • the size and mechanical properties required of the forging for satisfactory operation require specialized processing that only a few vendors in the world can provide.
  • In order to obtain a new forging from one of the suppliers often takes in excess of a year or more. Accordingly the production of a new turbine rotor is very costly not only in financial terms but also in terms of time.
  • the damaged rotor may be replaced by a spare rotor. Due to the fact, that the waiting period for a forging necessary to produce a new rotor is very long, as already mentioned above, customers often store a spare rotor in order to ensure that they can resume power generation as quickly as possible in case of an unrepairable rotor. However, the stocking of a new replacement rotor is accompanied by large expense.
  • a method for producing a turbine rotor, in particular a steam turbine rotor comprising the steps of:
  • a new rotor is produced on the basis of at least one existing rotor, which may be provided in form of a salvaged or spare rotor having predominantly larger dimensions as the dimensions of the intended rotor to be produced.
  • the intended rotor is fitted in the at least one existing rotor by means of a comparison of the form of the at least one existing rotor with the form of the intended rotor in order to choose a favorable position of the intended rotor within said at least one existing rotor, wherein the fitting may be supported by a corresponding computer program.
  • the choice of the position of the intended rotor within said at least one existing rotor in step b) is made taking into consideration production-orientated aspects, in particular the amount of material to be applied in step c) and/or the amount of material to be machined in step d).
  • the machining in step d) is performed by means of turning and/or milling and/or grinding.
  • At least two forged and machined existing steam turbine rotors are provided and joined to each other in step a), in particular by means of welding. Accordingly, the new rotor is produced on the basis of two existing rotors, which may be provided in the form of salvaged or spare rotors.
  • one or both of said at least two forged and machined existing steam turbine rotors are shortened prior to their joining in order to create a favorable basis for the production of the new rotor.
  • the drawing schematically shows a steam turbine rotor 1 , which is intended to be produced by the claimed method, and an existing steam turbine rotor 2 having predominantly larger dimensions as the dimensions of the intended rotor 1 .
  • the existing steam turbine rotor 2 is provided.
  • the existing rotor 2 may be a salvaged or a spare rotor being in stock.
  • the existing rotor 2 may also be assembled of two or more existing steam turbine rotors, which are joined to each other in order to form the existing rotor 2 , e.g. by means of welding, wherein the existing steam turbine rotors may be shortened prior to their joining
  • a second step b) the form of the existing rotor 2 is compared with the form of the intended rotor 1 and a position of the intended rotor 1 is chosen within the existing rotor 2 taking into consideration production-oriented aspects, in particular the amount of material to be applied in step c) and/or the amount of material to be machined in step d).
  • the comparison of the forms of the existing rotor 2 and the intended rotor 1 as well as the choice of the position of the intended rotor 1 within the existing rotor 2 may be supported by a suitable computer program, by means of which the intended rotor 1 can be fitted in the existing rotor 2 as indicated in the figure.
  • the intended rotor 1 is produced at the chosen position by machining the existing rotor 2 , in particular by means of turning and/or milling and/or grinding.
  • One main advantage of the method is that it is superior to purchasing a new forging from both a cost and schedule perspective. It is also preferable to performing large-scale weld repairs where a significant percentage of the forging would have to be restored.

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Butt Welding And Welding Of Specific Article (AREA)
  • Forging (AREA)

Abstract

A method of producing a turbine rotor, in particular a steam turbine rotor, is provided. A forged and machined existing steam turbine rotor having partially larger dimensions as dimensions of an intended rotor is provided. The form of the existing rotor is compared with the form of the intended rotor and a position of the intended rotor within the existing rotor is chosen. Material is applied by build-up welding on portions of the existing rotor where not enough material is present for machining the intended rotor at the chosen position. The intended rotor is produced at the chosen position by machining the existing rotor.

Description

    FIELD OF INVENTION
  • The claimed invention refers to a method for producing a turbine rotor, in particular a steam turbine rotor.
  • BACKGROUND OF INVENTION
  • Steam turbine rotors are large components manufactured from forged steel ingots. The size and mechanical properties required of the forging for satisfactory operation require specialized processing that only a few vendors in the world can provide. In order to obtain a new forging from one of the suppliers often takes in excess of a year or more. Accordingly the production of a new turbine rotor is very costly not only in financial terms but also in terms of time.
  • Steam turbine rotors wear out during their operation. Accordingly, it is necessary to repair worn steam turbine rotors and to return them to service. Rotors can be repaired mechanically. Such mechanical repairs include machining away damaged areas, modifying integral rotors to include separate components, or stress relieving to remove excessive hardness or distortion. In addition, rotors can be repaired by means of build-up welding and subsequent machining Build-up welding introduces the ability to restore a rotor to its original configuration with little to no detriment to performance or reliability. However, rotor welding can be a slow and expensive process, which can make large repairs difficult financially.
  • If a repair of a steam turbine rotor is not profitable due to excessive damages, the damaged rotor may be replaced by a spare rotor. Due to the fact, that the waiting period for a forging necessary to produce a new rotor is very long, as already mentioned above, customers often store a spare rotor in order to ensure that they can resume power generation as quickly as possible in case of an unrepairable rotor. However, the stocking of a new replacement rotor is accompanied by large expense.
  • SUMMARY OF INVENTION
  • It is an object to provide an alternative method for producing a turbine rotor of the above-mentioned kind, which is favorable in terms of time and expense.
  • In order to solve this object, a method for producing a turbine rotor, in particular a steam turbine rotor is provided, said method comprising the steps of:
    • a) Providing at least one forged and machined existing steam turbine rotor having partially larger dimensions as the dimensions of the intended rotor to be produced;
    • b) Comparing the form of said at least one existing rotor with the form of the intended rotor and choosing a position of the intended rotor within said at least one existing rotor;
    • c) Applying material by means of build-up welding on portions of said at least one existing rotor, where not enough material is present for machining the intended rotor at the chosen position; and
    • d) Producing the intended rotor at the chosen position by machining the existing rotor.
  • Thus, according to the method of the claimed invention a new rotor is produced on the basis of at least one existing rotor, which may be provided in form of a salvaged or spare rotor having predominantly larger dimensions as the dimensions of the intended rotor to be produced. The intended rotor is fitted in the at least one existing rotor by means of a comparison of the form of the at least one existing rotor with the form of the intended rotor in order to choose a favorable position of the intended rotor within said at least one existing rotor, wherein the fitting may be supported by a corresponding computer program. At positions, where not enough material is present for producing the intended rotor at the chosen position by means of machining, additional material is applied by means of build-up welding on the respective portions of the at least one existing rotor. Subsequently, the intended rotor is produced at the chosen position by machining the existing rotor.
  • Preferably, the choice of the position of the intended rotor within said at least one existing rotor in step b) is made taking into consideration production-orientated aspects, in particular the amount of material to be applied in step c) and/or the amount of material to be machined in step d).
  • For example, the machining in step d) is performed by means of turning and/or milling and/or grinding.
  • According to one embodiment, at least two forged and machined existing steam turbine rotors are provided and joined to each other in step a), in particular by means of welding. Accordingly, the new rotor is produced on the basis of two existing rotors, which may be provided in the form of salvaged or spare rotors.
  • According to another embodiment, one or both of said at least two forged and machined existing steam turbine rotors are shortened prior to their joining in order to create a favorable basis for the production of the new rotor.
  • BRIEF DESCRIPTION OF THE DRAWINGS
  • Further features and aspects of the claimed invention become apparent by means of the following description of a method for producing a turbine rotor with reference to the accompanying drawing.
  • DETAILED DESCRIPTION OF INVENTION
  • The drawing schematically shows a steam turbine rotor 1, which is intended to be produced by the claimed method, and an existing steam turbine rotor 2 having predominantly larger dimensions as the dimensions of the intended rotor 1.
  • In a first step a) of the method, the existing steam turbine rotor 2 is provided. The existing rotor 2 may be a salvaged or a spare rotor being in stock. According to an alternative embodiment of the method, the existing rotor 2 may also be assembled of two or more existing steam turbine rotors, which are joined to each other in order to form the existing rotor 2, e.g. by means of welding, wherein the existing steam turbine rotors may be shortened prior to their joining
  • In a second step b) the form of the existing rotor 2 is compared with the form of the intended rotor 1 and a position of the intended rotor 1 is chosen within the existing rotor 2 taking into consideration production-oriented aspects, in particular the amount of material to be applied in step c) and/or the amount of material to be machined in step d). The comparison of the forms of the existing rotor 2 and the intended rotor 1 as well as the choice of the position of the intended rotor 1 within the existing rotor 2 may be supported by a suitable computer program, by means of which the intended rotor 1 can be fitted in the existing rotor 2 as indicated in the figure.
  • At portions A and B, where not enough material is present for machining the intended rotor 1 at the chosen position, it is necessary to augment the dimensions of the existing rotor 2 with a corresponding amount of weld material in an additional step c) by means of a build-up welding.
  • In a further step d) the intended rotor 1 is produced at the chosen position by machining the existing rotor 2, in particular by means of turning and/or milling and/or grinding.
  • One main advantage of the method is that it is superior to purchasing a new forging from both a cost and schedule perspective. It is also preferable to performing large-scale weld repairs where a significant percentage of the forging would have to be restored.
  • While specific embodiments have been described in detail, those with ordinary skill in the art will appreciate that various modifications and alternative to those details could be developed in light of the overall teachings of the disclosure. For example, elements described in association with different embodiments may be combined. Accordingly, the particular arrangements disclosed are meant to be illustrative only and should not be construed as limiting the scope of the claims or disclosure, which are to be given the full breadth of the appended claims, and any and all equivalents thereof It should be noted that the term “comprising” does not exclude other elements or steps and the use of articles “a” or “an” does not exclude a plurality.

Claims (7)

1. Method for producing a turbine rotor comprising:
a) providing at least one forged and machined existing steam turbine rotor having partially larger dimensions as dimensions of an intended rotor to be produced;
b) comparing the form of said at least one existing rotor with the form of the intended rotor and choosing a position of the intended rotor within said at least one existing rotor;
c) applying material by build-up welding on portions of said at least one existing rotor, where not enough material is present for machining the intended rotor at the chosen position; and
d) producing the intended rotor at the chosen position by machining the existing rotor.
2. Method according to claim 1, wherein a choice of the position of the intended rotor within said at least one existing rotor in step b) is made taking into consideration production-orientated aspects, in particular the amount of material to be applied in step c) and/or the amount of material to be machined in step d).
3. Method according to claim 1, wherein the machining in step d) is performed by means of turning and/or milling and/or grinding.
4. Method according to claim 1, wherein at least two forged and machined existing steam turbine rotors are provided and joined to each other in step a).
5. Method according to claim 4, wherein said at least two existing rotors are joined to each other by welding.
6. Method according to claim 4, wherein one or both of said at least two forged and machined existing steam turbine rotors are shortened prior to their joining.
7. Method according to claim 5, wherein one or both of said at least two forged and machined existing steam turbine rotors are shortened prior to their joining.
US14/181,878 2014-02-17 2014-02-17 Method for producing a turbine rotor Abandoned US20150231690A1 (en)

Priority Applications (5)

Application Number Priority Date Filing Date Title
US14/181,878 US20150231690A1 (en) 2014-02-17 2014-02-17 Method for producing a turbine rotor
EP15700388.0A EP3071365A1 (en) 2014-02-17 2015-01-15 Method for producing a turbine rotor
PCT/EP2015/050624 WO2015121016A1 (en) 2014-02-17 2015-01-15 Method for producing a turbine rotor
RU2016133502A RU2016133502A (en) 2014-02-17 2015-01-15 METHOD FOR PRODUCING A TURBINE ROTOR
US15/358,101 US20170074105A1 (en) 2014-02-17 2016-11-21 Method for producing a turbine rotor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/181,878 US20150231690A1 (en) 2014-02-17 2014-02-17 Method for producing a turbine rotor

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US15/358,101 Continuation US20170074105A1 (en) 2014-02-17 2016-11-21 Method for producing a turbine rotor

Publications (1)

Publication Number Publication Date
US20150231690A1 true US20150231690A1 (en) 2015-08-20

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US14/181,878 Abandoned US20150231690A1 (en) 2014-02-17 2014-02-17 Method for producing a turbine rotor
US15/358,101 Abandoned US20170074105A1 (en) 2014-02-17 2016-11-21 Method for producing a turbine rotor

Family Applications After (1)

Application Number Title Priority Date Filing Date
US15/358,101 Abandoned US20170074105A1 (en) 2014-02-17 2016-11-21 Method for producing a turbine rotor

Country Status (4)

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US (2) US20150231690A1 (en)
EP (1) EP3071365A1 (en)
RU (1) RU2016133502A (en)
WO (1) WO2015121016A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019154957A1 (en) * 2018-02-09 2019-08-15 Otto Fuchs - Kommanditgesellschaft Method for producing a structural component from a high-strength alloy material

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3521664A1 (en) * 1985-06-18 1986-12-18 BBC Aktiengesellschaft Brown, Boveri & Cie., Baden, Aargau METHOD FOR FASTENING BLADES ON THE CIRCUMFERENCE OF THE ROTOR BODY OF A STEAM TURBINE
US4893388A (en) * 1988-12-08 1990-01-16 Westinghouse Electric Corp. Method of modifying turbine rotor discs
US5172475A (en) * 1991-12-02 1992-12-22 Westinghouse Electric Corp. Method for repairing a rotor
US6749518B2 (en) * 2002-04-08 2004-06-15 General Electric Company Inertia welded shaft and method therefor
US20080011812A1 (en) * 2005-11-04 2008-01-17 General Electric Company Integral backing ring for stub shaft weld repairs of rotating equipment and related method
US7507933B2 (en) * 2005-11-23 2009-03-24 General Electric Company Method for fabricating a rotor shaft
US8961144B2 (en) * 2011-06-30 2015-02-24 General Electric Company Turbine disk preform, welded turbine rotor made therewith and methods of making the same

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2019154957A1 (en) * 2018-02-09 2019-08-15 Otto Fuchs - Kommanditgesellschaft Method for producing a structural component from a high-strength alloy material
EP3658328B1 (en) 2018-02-09 2020-12-30 Otto Fuchs - Kommanditgesellschaft - Method for producing a structural component from a high-strength alloy material

Also Published As

Publication number Publication date
RU2016133502A (en) 2018-03-22
EP3071365A1 (en) 2016-09-28
US20170074105A1 (en) 2017-03-16
RU2016133502A3 (en) 2018-03-22
WO2015121016A1 (en) 2015-08-20

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Owner name: SIEMENS AKTIENGESELLSCHAFT, GERMANY

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Effective date: 20140708

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Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNORS:GRIFFIN, GARY;MARSHALL, JEREMY;SIGNING DATES FROM 20140326 TO 20140707;REEL/FRAME:033988/0979

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