EP4204595A1 - Martensitic steel with retarded z phase formation, powder and blank or component - Google Patents

Martensitic steel with retarded z phase formation, powder and blank or component

Info

Publication number
EP4204595A1
EP4204595A1 EP21773009.2A EP21773009A EP4204595A1 EP 4204595 A1 EP4204595 A1 EP 4204595A1 EP 21773009 A EP21773009 A EP 21773009A EP 4204595 A1 EP4204595 A1 EP 4204595A1
Authority
EP
European Patent Office
Prior art keywords
weight
powder
alloy
blank
component according
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.)
Pending
Application number
EP21773009.2A
Other languages
German (de)
French (fr)
Inventor
Torsten Neddemeyer
Axel Bublitz
Torsten-Ulf Kern
Karsten Kolk
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 Energy Global GmbH and Co KG
Original Assignee
Siemens Energy Global GmbH and Co KG
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 Energy Global GmbH and Co KG filed Critical Siemens Energy Global GmbH and Co KG
Publication of EP4204595A1 publication Critical patent/EP4204595A1/en
Pending legal-status Critical Current

Links

Classifications

    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/12—Metallic powder containing non-metallic particles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F3/00—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces
    • B22F3/17—Manufacture of workpieces or articles from metallic powder characterised by the manner of compacting or sintering; Apparatus specially adapted therefor ; Presses and furnaces by forging
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B33—ADDITIVE MANUFACTURING TECHNOLOGY
    • B33Y—ADDITIVE MANUFACTURING, i.e. MANUFACTURING OF THREE-DIMENSIONAL [3-D] OBJECTS BY ADDITIVE DEPOSITION, ADDITIVE AGGLOMERATION OR ADDITIVE LAYERING, e.g. BY 3-D PRINTING, STEREOLITHOGRAPHY OR SELECTIVE LASER SINTERING
    • B33Y10/00—Processes of additive manufacturing
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C33/00—Making ferrous alloys
    • C22C33/02—Making ferrous alloys by powder metallurgy
    • C22C33/0257—Making ferrous alloys by powder metallurgy characterised by the range of the alloying elements
    • C22C33/0278—Making 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%
    • C22C33/0285—Making 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%
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/001—Ferrous alloys, e.g. steel alloys containing N
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/02—Ferrous alloys, e.g. steel alloys containing silicon
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/04—Ferrous alloys, e.g. steel alloys containing manganese
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/06—Ferrous alloys, e.g. steel alloys containing aluminium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/42—Ferrous alloys, e.g. steel alloys containing chromium with nickel with copper
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/44—Ferrous alloys, e.g. steel alloys containing chromium with nickel with molybdenum or tungsten
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/46—Ferrous alloys, e.g. steel alloys containing chromium with nickel with vanadium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/48—Ferrous alloys, e.g. steel alloys containing chromium with nickel with niobium or tantalum
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/50—Ferrous alloys, e.g. steel alloys containing chromium with nickel with titanium or zirconium
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/52—Ferrous alloys, e.g. steel alloys containing chromium with nickel with cobalt
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C38/00—Ferrous alloys, e.g. steel alloys
    • C22C38/18—Ferrous alloys, e.g. steel alloys containing chromium
    • C22C38/40—Ferrous alloys, e.g. steel alloys containing chromium with nickel
    • C22C38/54—Ferrous alloys, e.g. steel alloys containing chromium with nickel with boron
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F1/00—Metallic powder; Treatment of metallic powder, e.g. to facilitate working or to improve properties
    • B22F1/10—Metallic powder containing lubricating or binding agents; Metallic powder containing organic material
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F5/00—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product
    • B22F5/009—Manufacture of workpieces or articles from metallic powder characterised by the special shape of the product of turbine components other than turbine blades
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C1/00—Making non-ferrous alloys
    • C22C1/04—Making non-ferrous alloys by powder metallurgy
    • C22C1/05—Mixtures of metal powder with non-metallic powder

Definitions

  • the invention relates to a martensitic steel with delayed Z-phase formation, powder and a blank or a component from it.
  • forged rotor disks of turbines in particular gas turbines, have hitherto been made from various forged steels.
  • a steel based on NiCrMoV is used for compressor disks and a steel based on CrMoWVNbN for turbine disks.
  • the application conditions and design requirements are decisive for the choice of forging material.
  • the material with the highest application temperature is currently a CrMoWVNbN-based steel and a CrMoCoVB-based steel.
  • Nickel materials are currently being discussed for higher operating temperatures.
  • the object is achieved by an alloy according to claim 1, a powder according to claim 2 and a blank or component according to claim 3.
  • the alloy according to the invention has at least (in % by weight): carbon (C): 0.16% - 0.24%, preferably 0.19% - 0.21%, silicon (Si): 0.0% - 0.08%, preferably 0.0% - 0.06%, more preferably 0.02% - 0.06%, Manganese (Mn): 0.04% - 0.16%, preferably 0.07% - 0 1.13%, chromium (Cr): 10.6% - 11.5%, preferably 11.2% - 11.5%, more preferably 11.2%, molybdenum (Mo) : 0.5% - 0.9% %, preferably 0.7%, tungsten (W) : 2.2% - 2.6%, preferably 2.3% - 2.5%, more preferably 2.45%, cobalt (Co) : 3.0% - 3.6%, preferably 3.25% - 3.40%, nickel (Ni): 0.09% - 0.19%, preferably 0.13% - 0.17%, Boron (B) :
  • Remainder iron consisting in particular of these elements.
  • silicon (Si) has the positive effect of making the melt more fluid and also serves as a deoxidizing agent. Another positive influence of silicon (Si) is that it increases tensile strength, yield point and resistance to scaling.
  • chromium (Cr) and cobalt (Co) also play an important role. They increase oxidation resistance and increase heat resistance.
  • a titanium (Ti)/nitrogen (N) ratio of 1.5 to 2 has proven advantageous.
  • An advantageous embodiment is (in % by weight): carbon (C): 0.20%, silicon (Si): ⁇ 0.08%, manganese (Mn): 0.10%, chromium (Cr): 11, 2%, molybdenum (Mo) : 0.7%, tungsten (W) : 2.4%, cobalt (Co) : 3.3%, nickel (Ni) : 0.15%, boron (B) : 0, 0.05%, nitrogen (N) : 0.013%, titanium (Ti) : 0.02%, vanadium (V) : 0.20%, niobium (Nb) : 0.05%, copper (Cu) : 1.75% , aluminum (Al): 0.02%, balance iron (Fe) .

Landscapes

  • Chemical & Material Sciences (AREA)
  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Materials Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacturing & Machinery (AREA)
  • Powder Metallurgy (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Heat Treatment Of Articles (AREA)

Abstract

Martensitic steel with Z phase, powder, and blank or component - alloy, at least comprising (in % by weight): carbon (C): 0.16% - 0.24%, silicon (Si): 0.0% – 0.08%, manganese (Mn): 0.04% – 0.16%, chromium (Cr): 10.6% – 11.5%, molybdenum (Mo): 0.5% – 0.9%, tungsten (W): 2.2% – 2.6%, cobalt (Co): 3.0% – 3.6%, nickel (Ni): 0.09% – 0.19%, boron (B): 0.0035% – 0.01%, nitrogen (N): 0.001% – 0.025%, titanium (Ti): 0.01% – 0.04%, copper (Cu): 1.20% - 2.30%, optionally vanadium (V): 0.10% – 0.30%, niobium (Nb): 0.02% – 0.08%, aluminium (Al): 0.003% - 0.06%, balance: iron (Fe), especially consisting of these elements.

Description

Beschreibung description
MARTENSITISCHER STAHL MIT VERZÖGERTER Z-PHASENBILDUNG, PULVER SOWIE ROHTEIL ODER BAUTEIL DELAYED Z-PHASE MARTENSITIC STEEL, POWDER AND BLANK OR COMPONENT
Die Erfindung betri f ft einen martensitischen Stahl mit verzögerter Z-Phasenbildung, Pulver sowie ein Rohteil bzw . ein Bauteil daraus . The invention relates to a martensitic steel with delayed Z-phase formation, powder and a blank or a component from it.
In Korrelation zu Anwendungsbedingungen werden geschmiedete Rotorscheiben von Turbinen, insbesondere Gasturbinen, bisher aus verschiedenen Schmiedestählen hergestellt . So wird ein Stahl auf der Basis NiCrMoV für Verdichterscheiben sowie ein Stahl auf der Basis CrMoWVNbN für Turbinenscheiben verwendet . Ausschlaggebend für die Wahl des Schmiedematerials sind die Anwendungsbedingungen und die Designanforderungen . In correlation to application conditions, forged rotor disks of turbines, in particular gas turbines, have hitherto been made from various forged steels. A steel based on NiCrMoV is used for compressor disks and a steel based on CrMoWVNbN for turbine disks. The application conditions and design requirements are decisive for the choice of forging material.
Für die Auswahl eines Schmiedewerkstof fes gilt es immer ein Gleichgewicht aus Festigkeit und Zähigkeit zu gewährleiten, um die Designanforderungen einzuhalten . When selecting a forging material, there is always a balance of strength and toughness to meet design requirements.
Der Werkstof f mit der höchsten Einsat ztemperatur ist aktuell ein Stahl auf der Basis CrMoWVNbN sowie ein Stahl auf der Basis CrMoCoVB . The material with the highest application temperature is currently a CrMoWVNbN-based steel and a CrMoCoVB-based steel.
Beide Werkstof fe stoßen aber für einen Einsatz oberhalb 773K an ihre Grenzen . However, both materials reach their limits when used above 773K.
Nichtsdestotrotz deuten aktuelle Untersuchungen darauf hin, dass Eisenlegierungen bis 900K genutzt werden können . Nonetheless, recent research suggests that ferrous alloys up to 900K can be used.
Für höhere Einsat ztemperaturen sind aktuell Nickelwerkstof fe in Diskussion . Nickel materials are currently being discussed for higher operating temperatures.
Leider haben die nichtbasierten Bauteile folgende Nachteile , weshalb der Einsatz abzuwägen ist : Unfortunately, the non-based components have the following disadvantages, which is why their use should be considered:
- höhere Kosten im Vergleich zur Scheibe aus Stahl , - higher cost compared to steel disc,
- neue Bruchmechanikkonzepte müssen entwickelt werden, - new fracture mechanics concepts have to be developed,
- längere Bearbeitungs zeiten in der Fertigung . Es ist daher Aufgabe der Erfindung oben genanntes Problem zu lösen, insbesondere die Warmfestigkeit zu steigern, so dass noch größere Einsat ztemperaturen, also eine Steigerung um mindestens 20K bis 30K, möglich sind. - Longer processing times in production. It is therefore the object of the invention to solve the above-mentioned problem, in particular to increase the heat resistance, so that even higher application temperatures, ie an increase by at least 20K to 30K, are possible.
Die Aufgabe wird gelöst durch eine Legierung gemäß Anspruch 1, ein Pulver gemäß Anspruch 2 sowie ein Rohteil oder Bauteil gemäß Anspruch 3. The object is achieved by an alloy according to claim 1, a powder according to claim 2 and a blank or component according to claim 3.
In den Unteransprüchen sind weitere vorteilhafte Maßnahmen aufgelistet, die beliebig miteinander kombiniert werden können, um weitere Vorteile zu erzielen. Further advantageous measures are listed in the dependent claims, which can be combined with one another as desired in order to achieve further advantages.
Durch die Bildung der Z-Phase innerhalb des Nutzungszeitraums des Bauteils wurde die Legierungszusammensetzung martensi- tischer Stähle bisher begrenzt. Until now, the alloy composition of martensitic steels has been limited by the formation of the Z-phase within the service life of the component.
Die erfindungsgemäße Legierung weist zumindest auf ( in Gew . -% ) : Kohlenstoff (C) : 0,16% - 0,24%, vorzugsweise 0,19% - 0,21%, Silizium (Si) : 0,0% - 0,08%, vorzugsweise 0,0% - 0,06%, besonders vorzugsweise 0,02% - 0,06%, Mangan (Mn) : 0,04% - 0,16%, vorzugsweise 0,07% - 0,13%, Chrom (Cr) : 10, 6% - 11,5%, vorzugsweise 11,2% - 11,5%, ganz vorzugsweise 11,2%, Molybdän (Mo) : 0,5% - 0,9%, vorzugsweise 0,7%, Wolfram (W) : 2,2% - 2, 6%, vorzugsweise 2,3% - 2,5%, ganz vorzugsweise 2,45%, Kobalt (Co) : 3,0% - 3, 6%, vorzugsweise 3,25% - 3,40%, Nickel (Ni) : 0,09% - 0,19%, vorzugsweise 0,13% - 0,17%, Bor (B) : 0, 0035% - 0, 01%, vorzugsweise 0,004% - 0,006%, Stickstoff (N) : 0,001% - 0,025%, vorzugsweise 0,011% - 0,015%, Titan (Ti) : 0,01% - 0,04%, vorzugsweise 0,018% - 0,028%, Kupfer (Cu) : 1,20% - 2,30%, vorzugsweise 1, 65% - 1,85%, optional Vanadium (V) : 0,10% - 0,30%, vorzugsweise 0,15% - 0,25%, Niob (Nb) : 0,02% - 0,08%, vorzugsweise 0,04% - 0,06%, Aluminium (Al) : 0,003% - 0,06%, insbesondere 0,005% - 0,04%, The alloy according to the invention has at least (in % by weight): carbon (C): 0.16% - 0.24%, preferably 0.19% - 0.21%, silicon (Si): 0.0% - 0.08%, preferably 0.0% - 0.06%, more preferably 0.02% - 0.06%, Manganese (Mn): 0.04% - 0.16%, preferably 0.07% - 0 1.13%, chromium (Cr): 10.6% - 11.5%, preferably 11.2% - 11.5%, more preferably 11.2%, molybdenum (Mo) : 0.5% - 0.9% %, preferably 0.7%, tungsten (W) : 2.2% - 2.6%, preferably 2.3% - 2.5%, more preferably 2.45%, cobalt (Co) : 3.0% - 3.6%, preferably 3.25% - 3.40%, nickel (Ni): 0.09% - 0.19%, preferably 0.13% - 0.17%, Boron (B) : 0.0035% - 0.01%, preferably 0.004% - 0.006%, Nitrogen (N) : 0.001% - 0.025%, preferably 0.011% - 0.015%, Titanium (Ti) : 0.01% - 0.04%, preferably 0.018% - 0.028%, copper (Cu): 1.20% - 2.30%, preferably 1.65% - 1.85%, optionally vanadium (V): 0.10% - 0 .30%, preferably 0.15% - 0.25%, niobium (Nb) : 0.02% - 0.08%, preferably 0.04% - 0.06%, aluminum (Al) : 0.003% - 0 .06%, especially 0.005% - 0.04%,
Rest Eisen ( Fe ) , insbesondere bestehend aus diesen Elementen. Remainder iron (Fe), consisting in particular of these elements.
Bei der Stahlherstellung hat Silizium (Si) die positive Wirkung die Schmelze dünnflüssiger zu gestalten und dient auch als Desoxidationsmittel. Ein weiterer positiver Einfluss von Silizium (Si) ist es, dass es die Zugfestigkeit, Streckgrenze und Zunderbeständigkeit erhöht. In steel production, silicon (Si) has the positive effect of making the melt more fluid and also serves as a deoxidizing agent. Another positive influence of silicon (Si) is that it increases tensile strength, yield point and resistance to scaling.
Außerdem spielen die Anteile von Chrom (Cr) und Kobalt (Co) eine wichtige Rolle. Sie erhöhen die Oxidationsbeständigkeit und steigern die Warmfestigkeit. The proportions of chromium (Cr) and cobalt (Co) also play an important role. They increase oxidation resistance and increase heat resistance.
Als vorteilhaft hat sich ein Titan (Ti) /Stickstoff (N) Verhältnis von 1.5 bis 2 erwiesen. A titanium (Ti)/nitrogen (N) ratio of 1.5 to 2 has proven advantageous.
Durch das neue Konzept kann die Bildung der Z-Phase in Richtung 200.000h verschoben werden. Ein vorteilhaftes Ausführungsbeispiel lautet (in Gew.-%) : Kohlenstoff (C) : 0,20%, Silizium (Si) : < 0,08%, Mangan (Mn) : 0,10%, Chrom (Cr) : 11,2%, Molybdän (Mo) : 0,7%, Wolfram (W) : 2,4%, Kobalt (Co) : 3,3%, Nickel (Ni) : 0,15%, Bor (B) : 0, 005%, Stickstoff (N) : 0,013%, Titan (Ti) : 0, 02%, Vanadium (V) : 0,20%, Niob (Nb) : 0, 05%, Kupfer (Cu) : 1,75%, Aluminium (Al) : 0,02%, Rest Eisen (Fe) . With the new concept, the formation of the Z phase can be shifted in the direction of 200,000 hours. An advantageous embodiment is (in % by weight): carbon (C): 0.20%, silicon (Si): <0.08%, manganese (Mn): 0.10%, chromium (Cr): 11, 2%, molybdenum (Mo) : 0.7%, tungsten (W) : 2.4%, cobalt (Co) : 3.3%, nickel (Ni) : 0.15%, boron (B) : 0, 0.05%, nitrogen (N) : 0.013%, titanium (Ti) : 0.02%, vanadium (V) : 0.20%, niobium (Nb) : 0.05%, copper (Cu) : 1.75% , aluminum (Al): 0.02%, balance iron (Fe) .
Neben der Anwendung als Schmiedescheibe in der Gasturbine sind weitere Anwendungen denkbar, wie z.B. Gasturbinenverdichterschaufeln, Dampfturbinenschaufel oder als Dampfturbinenschmiedeteil . In addition to being used as a forged disk in the gas turbine, other applications are conceivable, such as gas turbine compressor blades, steam turbine blades or as a steam turbine forged part.
Die Vorteile sind: The advantages are:
Erweiterung des Einsatzbereiches „preiswerter" Eisenbasislegierungen im Vergleich zu „teuren Nickelbasiswerkstoffen" , schnellere Bearbeitbarkeit der Rotorbauteile auf Eisenbasis (10, 6% - 11,5% Chrom (Cr) ) im Vergleich zu Nickelbasiswerkstoff en, Extension of the area of application of "cheap" iron-based alloys compared to "expensive nickel-based materials", faster machinability of the rotor components based on iron (10.6% - 11.5% chromium (Cr)) compared to nickel-based materials,
Erfahrungen aus der Konstruktion, Fertigung und Herstellung der hochlegierten Eisenbasislegierungen können größtenteils übernommen werden; das hilft z.B. bei allen probabilistischen Ansätzen wie Bruchmechanik zur Minimierung des Risikos, Anwendungstemperatur kann erhöht werden und ermöglicht daher Leistungs- und Perf ormancesteigerung der Maschine , ohne dass externe Kühlung notwendig ist . Experiences from the design, manufacture and manufacture of high-alloy iron-based alloys can largely be adopted; this helps, for example, with all probabilistic approaches such as fracture mechanics to minimize the risk, Application temperature can be increased and therefore increases the power and performance of the machine without the need for external cooling.

Claims

6 6
Patentansprüche patent claims
1. Legierung, zumindest aufweisend (in Gew.-%) : Kohlenstoff (C) : 0,16% - 0,24%, vorzugsweise 0,19% - 0,21%, Silizium (Si) : 0,0% - 0,08%, vorzugsweise 0,0% - 0,06%, ganz vorzugsweise 0,02% - 0,06%, Mangan (Mn) : 0,04% - 0,16%, vorzugsweise 0,07% - 0,13%, Chrom (Cr) : 10, 6% - 11,5%, vorzugsweise 11,2% - 11,5%, ganz vorzugsweise 11,2%, Molybdän (Mo) : 0,5% - 0,9%, vorzugsweise 0,7%, Wolfram (W) : 2,2% - 2, 6%, vorzugsweise 2,3% - 2,5%, ganz vorzugsweise 2,45%, Kobalt (Co) : 3,0% - 3, 6%, vorzugsweise 3,25% - 3,40%, Nickel (Ni) : 0,09% - 0,19%, vorzugsweise 0,13% - 0,17%, Bor (B) : 0, 0035% - 0, 01%, vorzugsweise 0,004% - 0,006%, Stickstoff (N) : 0,001% - 0,025%, vorzugsweise 0,011% - 0,015%, Titan (Ti) : 0,015% - 0,035%, vorzugsweise 0,018% - 0,028%, Kupfer (Cu) : 1,30% - 2,00%, vorzugsweise 1, 65% - 1,85%, optional Vanadium (V) : 0,10% - 0,30%, vorzugsweise 0,15% - 0,25%, Niob (Nb) : 0,02% - 0,08%, vorzugsweise 0,04% - 0,06%, Aluminium (Al) : 0,003% - 0,06%, insbesondere 0,005% - 0,04%, 7 1. Alloy at least comprising (in % by weight): carbon (C): 0.16% - 0.24%, preferably 0.19% - 0.21%, silicon (Si): 0.0% - 0.08%, preferably 0.0% - 0.06%, more preferably 0.02% - 0.06%, Manganese (Mn): 0.04% - 0.16%, preferably 0.07% - 0 1.13%, chromium (Cr): 10.6% - 11.5%, preferably 11.2% - 11.5%, more preferably 11.2%, molybdenum (Mo) : 0.5% - 0.9% %, preferably 0.7%, tungsten (W) : 2.2% - 2.6%, preferably 2.3% - 2.5%, more preferably 2.45%, cobalt (Co) : 3.0% - 3.6%, preferably 3.25% - 3.40%, nickel (Ni) : 0.09% - 0.19%, preferably 0.13% - 0.17%, boron (B) : 0, 0.035% - 0.01%, preferably 0.004% - 0.006%, Nitrogen (N) : 0.001% - 0.025%, preferably 0.011% - 0.015%, Titanium (Ti) : 0.015% - 0.035%, preferably 0.018% - 0.028% , Copper (Cu) : 1.30% - 2.00%, preferably 1.65% - 1.85%, optionally Vanadium (V) : 0.10% - 0.30%, preferably 0.15% - 0 .25%, niobium (Nb) : 0.02% - 0.08%, preferably 0.04% - 0.06%, aluminum (Al) : 0.003% - 0.06%, preferably 0.005% - 0.0 4%, 7
Rest Eisen ( Fe ) , insbesondere bestehend aus diesen Elementen. Pulver, aufweisend eine Legierung nach Anspruch 1, optional aufweisend Binder oder Keramikpartikel, insbesondere bestehend aus dieser Legierung. Rohteil oder Bauteil, zumindest aufweisend eine Legierung nach Anspruch 1 oder hergestellt aus einem Pulver gemäß Anspruch 2, insbesondere bestehend aus einer Legierung nach Anspruch 1, welches gegossen und/oder geschmiedet und/oder wärmebehandelt und/oder bearbeitet ist. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der Ansprüche 1, 2 oder 3, enthaltend 0,2 Gew.-% Kohlenstoff (C) . Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,02 Gew.-% - 0,06 Gew.-% Silizium (Si) . Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,10 Gew.-% Mangan (Mn) . Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 10, 6 Gew.-% - 11,0 Gew.-% Chrom (Gr) , insbesondere 10,7 Gew.-% - 10,8 Gew.-% Chrom (Cr) . Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche 1 bis 6, enthaltend 11,0 Gew.-% - 11,4 Gew.-% Chrom (Cr) , insbesondere 11,2 Gew.-% Chrom (Cr) . 8 Remainder iron (Fe), consisting in particular of these elements. Powder containing an alloy according to Claim 1, optionally containing binder or ceramic particles, in particular consisting of this alloy. Blank or component at least comprising an alloy according to claim 1 or made from a powder according to claim 2, in particular consisting of an alloy according to claim 1, which is cast and/or forged and/or heat treated and/or machined. Alloy, powder, blank or component according to one or more of Claims 1, 2 or 3, containing 0.2% by weight of carbon (C). Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.02% by weight - 0.06% by weight of silicon (Si). Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.10% by weight of manganese (Mn). Alloy, powder, blank or component according to one or more of the preceding claims, containing 10.6% by weight - 11.0% by weight of chromium (Gr), in particular 10.7% by weight - 10.8% by weight. -% Chromium (Cr) . Alloy, powder, blank or component according to one or more of the preceding claims 1 to 6, containing 11.0% by weight - 11.4% by weight chromium (Cr), in particular 11.2% by weight chromium (Cr ) . 8th
9. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,70 Gew.-% Molybdän (Mo) . 9. Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.70 wt .-% molybdenum (Mo).
10. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 2,40 Gew.-% Wolfram (W) . 10. Alloy, powder, blank or component according to one or more of the preceding claims, containing 2.40% by weight of tungsten (W).
11. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 3,3 Gew.-% Kobalt (Co) . 11. Alloy, powder, blank or component according to one or more of the preceding claims, containing 3.3% by weight of cobalt (Co).
12. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,15 Gew.-% Nickel (Ni) . 12. Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.15% by weight of nickel (Ni).
13. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,005 Gew.-% Bor (B) . 13. Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.005% by weight of boron (B).
14. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,013 Gew.-% Stickstoff (N) , bis auf Verunreinigungslevel . 14. Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.013% by weight of nitrogen (N), down to the impurity level.
15. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,020 Gew.-% - 0,026 Gew.-% Titan (Ti) , insbesondere enthaltend 0,020 Gew.-% Titan (Ti) . 15. Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.020% by weight - 0.026% by weight of titanium (Ti), in particular containing 0.020% by weight of titanium (Ti).
16. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,20 Gew.-% Vanadium (V) . 16. Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.20% by weight of vanadium (V).
17. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,05 Gew.-% Niob (Nb) . 9 17. Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.05% by weight of niobium (Nb). 9
18. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 1,75 Gew.-% Kupfer (Cu) . 19. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, enthaltend 0,02 Gew.-% Aluminium (Al) . 18. Alloy, powder, blank or component according to one or more of the preceding claims, containing 1.75% by weight of copper (Cu). 19. Alloy, powder, blank or component according to one or more of the preceding claims, containing 0.02% by weight of aluminum (Al).
20. Legierung, Pulver, Rohteil oder Bauteil nach einem oder mehreren der vorherigen Ansprüche, aufweisend ein Titan (Ti) /Stickstoff (N) Verhältnis von 1.5 bis 2. 20. Alloy, powder, blank or component according to one or more of the preceding claims, having a titanium (Ti)/nitrogen (N) ratio of 1.5 to 2.
EP21773009.2A 2020-10-23 2021-09-01 Martensitic steel with retarded z phase formation, powder and blank or component Pending EP4204595A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102020213394.8A DE102020213394A1 (en) 2020-10-23 2020-10-23 Z-phase martensitic steel, powder and blank or part
PCT/EP2021/074098 WO2022083928A1 (en) 2020-10-23 2021-09-01 Martensitic steel with retarded z phase formation, powder and blank or component

Publications (1)

Publication Number Publication Date
EP4204595A1 true EP4204595A1 (en) 2023-07-05

Family

ID=77821723

Family Applications (1)

Application Number Title Priority Date Filing Date
EP21773009.2A Pending EP4204595A1 (en) 2020-10-23 2021-09-01 Martensitic steel with retarded z phase formation, powder and blank or component

Country Status (7)

Country Link
US (1) US20230392245A1 (en)
EP (1) EP4204595A1 (en)
JP (1) JP2023546198A (en)
KR (1) KR20230090346A (en)
CN (1) CN116419984A (en)
DE (1) DE102020213394A1 (en)
WO (1) WO2022083928A1 (en)

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE9002276D0 (en) * 1990-06-28 1990-06-28 Abb Powdermet Ab SAFETY MANUFACTURED FULLY THROTTLE CARMETS OF HEATHOLD SOLID MARTENSITIC CR STEEL
JP3315800B2 (en) * 1994-02-22 2002-08-19 株式会社日立製作所 Steam turbine power plant and steam turbine
JPH09296258A (en) * 1996-05-07 1997-11-18 Hitachi Ltd Heat resistant steel and rotor shaft for steam turbine
JP4212132B2 (en) * 1997-09-22 2009-01-21 独立行政法人物質・材料研究機構 Ferritic heat resistant steel having martensitic structure and method for producing the same
CN102517507B (en) * 2011-12-30 2013-08-07 山东理工大学 Steel for blades of turbine of ultra-supercritical fossil power plants and manufacturing method
EP2662462A1 (en) 2012-05-07 2013-11-13 Valls Besitz GmbH Low temperature hardenable steels with excellent machinability

Also Published As

Publication number Publication date
JP2023546198A (en) 2023-11-01
WO2022083928A1 (en) 2022-04-28
DE102020213394A1 (en) 2022-04-28
CN116419984A (en) 2023-07-11
US20230392245A1 (en) 2023-12-07
KR20230090346A (en) 2023-06-21

Similar Documents

Publication Publication Date Title
JP4162289B2 (en) Abrasion-resistant powder metallurgy cold work tool sintered steel with high impact toughness and method of manufacturing the same
US20060157171A1 (en) Heat resistant alloy for exhaust valves durable at 900°C and exhaust valves made of the alloy
KR101521071B1 (en) Precipitation hardening type martensitic steel and process for producing same
EP0083254A2 (en) Heat resisting steel
US5560788A (en) Heat resisting steels
US6162275A (en) Steel and a heat treated tool thereof manufactured by an integrated powder metalurgical process and use of the steel for tools
EP3175008A2 (en) Cobalt-based super alloy
CA2891863A1 (en) Method of manufacturing a ferrous alloy article using powder metallurgy processing
EP0073021B1 (en) Martensitic heat-resistant steel
WO2010133244A1 (en) Ferritic martensitic iron-based alloy, a component and a process
DE602004005910T2 (en) Heat-resistant steel and gas turbine and components made thereof
EP4204595A1 (en) Martensitic steel with retarded z phase formation, powder and blank or component
JP2014208869A (en) Precipitation-strengthened martensitic steel
EP3684957B1 (en) Martensitic steel with z-phase, powder and component made thereof
WO2017178555A1 (en) Martensitic steel with delayed z-phase formation, and component
JPH0414182B2 (en)
WO2017178188A1 (en) Martensitic steel having a z-phase, powder and component
EP4208579A1 (en) Alloy, raw workpiece, component consisting of austenite, and method for heat-treating an austenite
EP4377487A1 (en) Austenite alloy, blank and component, and method
EP0907758A1 (en) Martensitic-austentitic steel
WO2022053484A1 (en) Piston for an internal combustion engine, internal combustion engine having a piston, and use of an iron-based alloy
DE3333774C2 (en)
JPH0570902A (en) High cr alloy steel

Legal Events

Date Code Title Description
STAA Information on the status of an ep patent application or granted ep patent

Free format text: STATUS: UNKNOWN

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

Free format text: STATUS: THE INTERNATIONAL PUBLICATION HAS BEEN MADE

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

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

Free format text: STATUS: REQUEST FOR EXAMINATION WAS MADE

17P Request for examination filed

Effective date: 20230330

AK Designated contracting states

Kind code of ref document: A1

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 RS SE SI SK SM TR

DAV Request for validation of the european patent (deleted)
DAX Request for extension of the european patent (deleted)