EP0956371A1 - Austenitic nickel-chromium-molybdenum-silicon alloy with high corrosion resistance to hot chloride-containing gases and chloride - Google Patents
Austenitic nickel-chromium-molybdenum-silicon alloy with high corrosion resistance to hot chloride-containing gases and chlorideInfo
- Publication number
- EP0956371A1 EP0956371A1 EP97951980A EP97951980A EP0956371A1 EP 0956371 A1 EP0956371 A1 EP 0956371A1 EP 97951980 A EP97951980 A EP 97951980A EP 97951980 A EP97951980 A EP 97951980A EP 0956371 A1 EP0956371 A1 EP 0956371A1
- Authority
- EP
- European Patent Office
- Prior art keywords
- max
- alloy
- chloride
- molybdenum
- chromium
- 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.)
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Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/056—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 10% but less than 20%
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B23—MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
- B23K—SOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
- B23K35/00—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting
- B23K35/22—Rods, electrodes, materials, or media, for use in soldering, welding, or cutting characterised by the composition or nature of the material
- B23K35/24—Selection of soldering or welding materials proper
- B23K35/30—Selection of soldering or welding materials proper with the principal constituent melting at less than 1550 degrees C
- B23K35/3033—Ni as the principal constituent
- B23K35/304—Ni as the principal constituent with Cr as the next major constituent
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- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C19/00—Alloys based on nickel or cobalt
- C22C19/03—Alloys based on nickel or cobalt based on nickel
- C22C19/05—Alloys based on nickel or cobalt based on nickel with chromium
- C22C19/051—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W
- C22C19/055—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being at least 20% but less than 30%
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02B—INTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
- F02B3/00—Engines characterised by air compression and subsequent fuel addition
- F02B3/06—Engines characterised by air compression and subsequent fuel addition with compression ignition
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02F—CYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
- F02F7/00—Casings, e.g. crankcases or frames
- F02F2007/0097—Casings, e.g. crankcases or frames for large diesel engines
Definitions
- the invention relates to an enitic nickel-chromium-molybdenum alloy with additions of silicon.
- the alloy with the material number 2.4856 is difficult to process.
- this alloy suffers a considerable loss of ductility at temperatures above 500 ° C., which can lead to crack formation in components that are pressurized and / or subject to high mechanical stress.
- the start of excretion of the ductility-reducing excretions can be delayed by lowering the iron content.
- the new alloy described in this document also has disadvantages.
- the ductility-increasing measures listed reduce the corrosion resistance against gases containing high chlorine and chloride-containing deposits compared to the alloy with material number 2.4856. Even with this alloy, high corrosion rates occur due to the constantly increasing process and exhaust gas temperatures due to the increase in efficiency. Alloys of the type 2.4856 are also susceptible to hot corrosion due to sulphate-containing deposits, so that there is a considerable need for a different type of alloy with improved resistance to high-temperature corrosion.
- the invention has for its object to develop an alloy with a significantly improved resistance to chlorine gas corrosion and chloride-containing deposits compared to the prior art with simultaneous increased resistance to sulphate corrosion and with high ductility in the entire temperature range up to 1000 ° C.
- the task is solved by a silicon-containing nickel-chromium-molybdenum alloy, which (in mass%) consists of the following components:
- the alloy according to the invention is distinguished by a significantly increased high-temperature corrosion resistance against chlorine-containing gases, chloride-containing ashes, deposits and salt compounds with simultaneous corrosion resistance against sulphate corrosion and wet corrosion as well as high ductility.
- a preferred alloy is characterized by the following alloy components (in% by mass):
- the alloy is advantageously suitable, on the one hand, for the production of pipes, in particular composite tubes, sheets, strip material, foils, wires and objects made from these semi-finished products, and on the other hand, corrosion protection applied as cladding or plating.
- Table 1 shows, by way of example, analyzes of batches from the alloy (AF) according to the invention and the comparison alloys (G, H) lying outside the composition according to the invention. Alloy 2.4856 was used for comparison. All alloy variants were made from cast blocks by hot rolling followed by cold rolling at room temperature. The resistance of the alloy according to the invention to chloride corrosion can be seen from Figures 1 and 2.
- FIG. 3 shows the metallographically determined corrosion attack of samples which are in a complex medium (chlorine-containing synthetic waste combustion gas (2.5 g / m 3 HC1, 1.3 g / m 3 S0 2 / 9% 0 2 , remainder N 2 ) with simultaneous exposure to boiler ash containing chloride) were stored at 600 ° C for 1000 hours.
- chlorine-containing synthetic waste combustion gas 2.5 g / m 3 HC1, 1.3 g / m 3 S0 2 / 9% 0 2 , remainder N 2
- the silicon-containing alloy according to the invention shows a significantly reduced corrosion attack.
- Figure 4 shows corrosion attack after 1008 hours of cyclical aging of samples which were coated with a coating of Na 2 S0 4 / KCl before being aged at 750 ° C in an atmosphere containing chlorine and sulfur dioxide. This test is used to test the resistance to sulphate corrosion. How as can be seen from the figure, the alloy according to the invention also shows significantly lower corrosion rates than the alloy 2.4856 currently used under such corrosion conditions with this corrosion stress.
- the excellent properties of the alloy according to the invention can be attributed to the silicon additives and the coordination of the alloy elements molybdenum, chromium and iron.
- the silicon content of the alloy according to the invention should be between 0.6% and 1.7%, since at lower silicon contents the corrosion-inhibiting effect of the silicon no longer occurs and at higher silicon contents with the appearance of embrittling suicides and significant loss of ductility, particularly in the case of medium-sized ones Temperatures (500-800 ° C), can be expected. With silicon contents between 0.5 and 1.7%, the notched impact strength, measured on ISO V notched impact samples, does not drop below 100 J / cm, even after aging for 100 hours at 600 ° C, as shown in Figure 5.
- the molybdenum content of the alloy according to the invention is limited to 10%, since, as can be seen from FIG. 4, the susceptibility to sulphate corrosion increases with higher molybdenum contents. A minimum molybdenum content is required to avoid wet corrosion in the event of a drop below the dew point.
- the chromium content of the alloy according to the invention should be between 18% and 22% in order to ensure adequate corrosion resistance. Higher chromium contents make it difficult to process nickel-chromium-molybdenum alloys.
- the alloy should also contain hafnium and / or rare earths and / or zirconium and / or yttrium, if an improved adhesion of protective oxide layers is required for specific applications, for example in automotive exhaust systems at high temperatures and / or with rapid temperature changes. However, the sum of these reactive elements should not exceed 0.5%.
- the iron content of the alloy according to the invention is limited to a maximum of 5%, since at higher iron contents in chloride-containing media there is a risk of the formation of volatile iron chlorides. However, a minimum iron content of 1% is required to ensure the processability of the alloy.
- the carbon content of the alloy according to the invention is limited to a maximum of 0.05% since there is a risk of intergranular corrosion at higher carbon contents.
- the titanium and aluminum contents are each reduced to a maximum of 0.5%, the actually undesirable niobium content to a maximum of. 0.5% is limited, since these elements can lead to a loss of ductility due to the formation of intermetallic phases at medium temperatures.
- the total addition of niobium, aluminum and titanium should not exceed 1%.
- a minimum content of the oxygen-affine elements aluminum, titanium, magnesium and calcium is required to ensure good oxidation resistance.
- the manganese content should be at least 0.05%, but not exceed 0.5%, since higher manganese contents have an unfavorable effect on the resistance to oxidation.
- 0.001-0.01% boron is also added to improve processability.
- the levels of phosphorus and sulfur should be kept as low as possible since these surface-active elements reduce both the high-temperature corrosion resistance and the ductility of the alloy.
- the alloy according to the invention can be used for strips, foils, sheets, tubes (seamless or welded), wires, as cladding, as cladding or as a composite tube.
- the alloy according to the invention can be produced either by block casting or by continuous casting after melting in a vacuum induction furnace or after open melting.
- the alloy can be remelted, but is not absolutely necessary.
- the hot shaping is carried out by forging, hot rolling or extrusion, the cold shaping by cold rolling, wire drawing or pilgrims.
- the production of composite materials, for example plating on carbon steels can be carried out by one of the customary build-up welding processes, by cold or hot rolling of sheets and strips, by explosive plating or by one of the customary processes for producing bimetallic tubes.
- the alloy is particularly suitable as a strip and sheet, pipe or cladding material for use in hot chlorine-containing gases or in the presence of chloride-containing deposits, such as in plants in the chemical industry, in plants for the thermal treatment of chlorine-containing chemical waste and contaminated soils as well as in automotive exhaust systems (bellows for decoupling the catalytic converter and engine).
- the excellent resistance of the alloy to complex corrosive salt deposits makes the alloy also suitable for use as a cladding and construction material in plants for thermal waste disposal, in large diesel engines, in plants for energy generation from biomass and in plants of the pulp industry.
Abstract
The invention relates to an austenitic nickel-chromium-molybdenum-silicon alloy with a markedly improved resistance to the type of hot chlorine-containing gases and chlorides found, for example, in chemical plants, thermal waste-disposal facilities, the exhaust systems of cars and in diesel engines, consisting of: Cr 18-22 %; Mo 6-10 %; Si 0.6-1.7 %; C 0.002-0.05 %; Fe 1-5 %; Mn 0.05-0.5 %; Al 0.1-0.5 %; Ti 0.1-0.5 %; Mg 0.005-0.05 %; Ca 0.001-0.01 %; V max. 0.5; P max. 0.02 %; S max. 0.01 %; B 0.001-0.01; Cu max. 0.5; Co max. 1 %; Hf, Y, Zr and/or rare earth elements 0.02-0.5 %; and the remainder nickel and impurities caused by the melting process.
Description
Austenitische Nickel-Chrom-Molybdän-Silizium-Legierung mit hoher Korrosionsbeständigkeit gegen heiße chlorhaltige Gase und ChlorideAustenitic nickel-chromium-molybdenum-silicon alloy with high corrosion resistance against hot chlorine-containing gases and chlorides
Gegenstand der Erfindung ist eine aus enitische Nickel-Chrom- Molybdän-Legierung mit Zusätzen von Silizium.The invention relates to an enitic nickel-chromium-molybdenum alloy with additions of silicon.
In Anlagen und Aggregaten, bei denen heiße chlorhaltige Gase und chloridhaltige Ablagerungen auftreten (Anlagen der chemischen Industrie, Anlagen zur thermischen Müllentsorgung, insbesondere bei der Verwertung von Sondermüll, Anlagen zur Verwertung von Biomasse, Großdieselmotoren, AuspuffSysteme von Automobilen) werden bei Temperaturen von bis zu 400 °C ferritische Kesselbau- stähle eingesetzt. Bei höheren Temperaturen werden vielfach Nikkei-Chrom-Molybdän-Legierungen mit 21,5 % Chrom, 9 % Molybdän, 3,7 % Niob, 2,5 % Eisen, Rest Nickel und unvermeidbare Verunreinigungen (Deutsche Werkstoffnummer 2.4856) verwendet (Stahlschlüssel 1995) .In plants and units in which hot chlorine-containing gases and chloride-containing deposits occur (plants in the chemical industry, plants for thermal waste disposal, in particular when recycling special waste, plants for recycling biomass, large diesel engines, exhaust systems of automobiles), temperatures of up to 400 ° C ferritic boiler steels are used. At higher temperatures, Nikkei-chromium-molybdenum alloys with 21.5% chromium, 9% molybdenum, 3.7% niobium, 2.5% iron, the rest nickel and inevitable impurities (German material number 2.4856) are used (steel key 1995) .
Die Legierung mit der Werkstoffnummer 2.4856 ist jedoch schwierig zu verarbeiten. Darüber hinaus erleidet diese Legierung bei Temperaturen oberhalb von 500 °C einen erheblichen Duktilitäts- verlust, der bei druckführenden und/oder mechanisch stark beanspruchten Bauteilen zur Rißbildung führen kann. In einem gewissen Umfang kann der Ausscheidungsbeginn der duktilitätsmindern- den Ausscheidungen verzögert werden durch ein Absenken des Eisengehaltes .However, the alloy with the material number 2.4856 is difficult to process. In addition, this alloy suffers a considerable loss of ductility at temperatures above 500 ° C., which can lead to crack formation in components that are pressurized and / or subject to high mechanical stress. To a certain extent, the start of excretion of the ductility-reducing excretions can be delayed by lowering the iron content.
Maßnahmen, die zu einer deutlichen Anhebung der Duktilität führen, werden in der internationalen Patentanmeldung WO 95/31579
angeführt, in welcher eine neue Legierung auf der Basis der Legierung gemäß Werkstoffnummer 2.4856 beschrieben wird, die sich durch eine erhöhte Kalt- und Warmverformbarkeit und eine höhere Duktilität auszeichnet.Measures which lead to a significant increase in ductility are described in international patent application WO 95/31579 in which a new alloy is described based on the alloy according to material number 2.4856, which is characterized by increased cold and hot formability and higher ductility.
Auch die neue, in dieser Druckschrift beschriebene Legierung weist noch Nachteile auf. So wird durch die angeführten duktili- tätssteigernden Maßnahmen die Korrosionsbeständigkeit gegen hochchlorhaltige Gase und chloridhaltige Beläge gegenüber der Legierung mit der Werkstoffnummer 2.4856 reduziert. Bereits bei dieser Legierung treten bei den aus Gründen der Wirkungsgradsteigerung ständig ansteigenden Prozeß- und Abgastemperaturen hohe Korrosionsraten auf. Legierungen vom Typ 2.4856 sind darüber hinaus anfällig gegen Heißkorrosion durch sulphathaltige Ablagerungen, so daß ein erheblicher Bedarf nach einer andersartigen Legierung mit verbesserter Beständigkeit gegen Hochtemperaturkorrosion besteht.The new alloy described in this document also has disadvantages. The ductility-increasing measures listed reduce the corrosion resistance against gases containing high chlorine and chloride-containing deposits compared to the alloy with material number 2.4856. Even with this alloy, high corrosion rates occur due to the constantly increasing process and exhaust gas temperatures due to the increase in efficiency. Alloys of the type 2.4856 are also susceptible to hot corrosion due to sulphate-containing deposits, so that there is a considerable need for a different type of alloy with improved resistance to high-temperature corrosion.
Der Erfindung liegt die Aufgabe zugrunde, eine Legierung mit einer gegenüber dem Stand der Technik deutlich verbesserten Beständigkeit gegen Chlorgaskorrosion und chloridhaltige Beläge bei gleichzeitiger erhöhter Beständigkeit gegen Sulphatkorrosion und bei hoher Duktilität im gesamten Temperaturbereich bis 1 000 °C zu entwickeln.
Die Aufgabe wird gelöst durch eine siliziumhaltige Nickel-Chrom- Molybdän-Legierung, die (in Masse-%) aus folgenden Bestandteilen besteht :The invention has for its object to develop an alloy with a significantly improved resistance to chlorine gas corrosion and chloride-containing deposits compared to the prior art with simultaneous increased resistance to sulphate corrosion and with high ductility in the entire temperature range up to 1000 ° C. The task is solved by a silicon-containing nickel-chromium-molybdenum alloy, which (in mass%) consists of the following components:
Cr 18 - 22Cr 18-22
Mo 6 - 10Mon 6-10
Si 0, 6 1,7Si 0.6 1.7
C 0, 002 - 0,05C 0.002 - 0.05
Fe 1 - 5Fe 1-5
Mn o, 05 - 0,5Mn 0.05-0.5
AI o, 1 0,5AI o, 1 0.5
Ti o, 1 0,5Ti o, 1 0.5
Mg o, 005 - 0,05Mg 005-0.05
Ca o, 001 - 0, 01Ca 001-0.01
V max. 0,5V max. 0.5
P max. 0,02P max. 0.02
S max. 0,01
S max. 0.01
Cu max. 0,5Cu max. 0.5
Co max. 1Co max. 1
Hf und/oder Y und/oder Zr und/oder Seltene ErdenHf and / or Y and / or Zr and / or rare earths
0,02 - 0,5 % Rest Nickel und erschmelzungsbedingte Verunreinigungen.0.02 - 0.5% rest of nickel and melting-related impurities.
Die erfindungsgemäße Legierung zeichnet sich mit einer gegenüber dem Stand der Technik deutlich erhöhten Hochtemperaturkorro- sionsbeständigkeit gegen chlorhaltige Gase, chloridhaltige Aschen, Ablagerungen und Salzverbindungen bei gleichzeitiger Korrosionsbeständigkeit gegen Sulphatkorrosion und Naßkorrosion sowie hoher Duktilität aus.The alloy according to the invention is distinguished by a significantly increased high-temperature corrosion resistance against chlorine-containing gases, chloride-containing ashes, deposits and salt compounds with simultaneous corrosion resistance against sulphate corrosion and wet corrosion as well as high ductility.
Vorteilhafte Weiterbildungen des Erfindungsgegenstandes sind den Unteransprüchen zu entnehmen .
Eine bevorzugte Legierung zeichnet sich durch folgende Legierungsbestandteile (in Masse-%) aus:Advantageous further developments of the subject matter of the invention can be found in the subclaims. A preferred alloy is characterized by the following alloy components (in% by mass):
Cr 18 - 20 %Cr 18 - 20%
Mo 8 - 9,0 oMon 8 - 9.0 o
Si 0, 7 - 1,1 oSi 0.7 - 1.1 o
C 0,02 - 0, 015 o,C 0.02 - 0.015 o,
OO
Fe 2,5 - 3,5Fe 2.5 - 3.5
Mn 0,05 - 0,1 oMn 0.05 - 0.1 o
AI 0,1 - 0,3 %AI 0.1 - 0.3%
Ti 0, 1 - 0,4 oTi 0.1-1.4 o
Mg 0,005 - 0, 015 oMg 0.005-0.015 o
Ca 0,001 - 0, 005 Q, oCa 0.001-0.005 Q, o
V max. 0,01 oV max. 0.01 o
P max. 0,002 g, oP max. 0.002 g, o
S max. . 0,001 oS max. . 0.001 o
B 0,001 - 0, 001 g, oB 0.001-0.001 g, o
Cu max . , 0,5 %Cu max. , 0.5%
Hf und/oder Y und/oder Zr und/oder Seltene ErdenHf and / or Y and / or Zr and / or rare earths
0, 03 - 0,06 o0.03 - 0.06 o
Rest Nickel und erschmelzungsbedingte Verunreinigungen.Remainder nickel and melting impurities.
Die Legierung eignet sich in vorteilhafter Weise einerseits zur Herstellung von Rohren, insbesondere Kompositröhren, Blechen, Bandmaterial, Folien, Drähten sowie aus diesen Halbzeugen hergestellte Gegenstände und andererseits als Auftragsschweißung oder Plattierung aufgebrachter Korrosionsschutz .The alloy is advantageously suitable, on the one hand, for the production of pipes, in particular composite tubes, sheets, strip material, foils, wires and objects made from these semi-finished products, and on the other hand, corrosion protection applied as cladding or plating.
Die vorteilhaften Eigenschaf en der erfindungsgemäßen Legierung gehen aus den folgenden Ausführungsbeispielen hervor. Tabelle 1 zeigt beispielhaft Analysen von Chargen aus der erfindungsgemäßen Legierung (A-F) sowie die von außerhalb der erfindungsgemäßen Zusammensetzung liegenden Vergleichslegierungen (G,H). Zum Vergleich wurde die Legierung 2.4856 herangezogen. Alle Legierungsvarianten wurden aus gegossenen Blöcken durch Warmwalzen mit anschließendem Kaltwalzen bei Raumtemperatur hergestellt.
Die Beständigkeit der erfindungsgemäßen Legierung gegen Chloridkorrosion geht aus den Abbildungen 1 und 2 hervor. Für die Versuche wurden geschliffene und gereinigte Testcoupons verschiedener Versuchslegierungen in eine wäßrige Lösung aus 1 mol/1 NaCl , 0,1 mol/1 CaCl2 und 0,25 mol/1 NaHC03 getaucht, bei 60 °C getrocknet und anschließend bei 750 °C an Luft über 240 Stunden ausgelagert. Dieser Test simuliert die Beanspruchungen, wie sie beispielsweise in Abgassystemen von Automobilmotoren (an Faltenbälgen zur Entkopplung von Katalysator und Motor) auftreten. Abbildung 1 zeigt den Metallabtrag, Abbildung 2 zeigt den metallo- graphisch ermittelten Korrosionsangriff bei Versuchsende . Bei den Untersuchungen hat es sich überraschend gezeigt, daß die Beständigkeit gegen Chloridkorrosion z.B. gegenüber der Legierung 2.4856 erheblich verbessert werden konnte durch die Zugabe von Silizium in Mengen zwischen 0,6 und 1,7 %.The advantageous properties of the alloy according to the invention are evident from the following exemplary embodiments. Table 1 shows, by way of example, analyzes of batches from the alloy (AF) according to the invention and the comparison alloys (G, H) lying outside the composition according to the invention. Alloy 2.4856 was used for comparison. All alloy variants were made from cast blocks by hot rolling followed by cold rolling at room temperature. The resistance of the alloy according to the invention to chloride corrosion can be seen from Figures 1 and 2. For the experiments, ground and cleaned test coupons of various test alloys were immersed in an aqueous solution of 1 mol / 1 NaCl, 0.1 mol / 1 CaCl 2 and 0.25 mol / 1 NaHC0 3 , dried at 60 ° C and then at 750 ° C exposed to air over 240 hours. This test simulates the stresses that occur, for example, in exhaust systems of automotive engines (on bellows for decoupling the catalytic converter and engine). Figure 1 shows the metal removal, Figure 2 shows the metallographically determined corrosion attack at the end of the test. In the course of the investigations, it has surprisingly been found that the resistance to chloride corrosion, for example in relation to the alloy 2.4856, could be considerably improved by adding silicon in amounts between 0.6 and 1.7%.
Der vorteilhafte Einfluß des Siliziums geht auch aus Abbildung 3 hervor, welche den metallographisch ermittelten Korrosionsangriff von Proben zeigt, welche in einem komplexen Medium (chlorhaltiges synthetisches Müllverbrennungsgas (2,5 g/m3 HC1, 1,3 g/m3 S02/ 9 % 02 , Rest N2) bei gleichzeitiger Beaufschlagung mit chloridhaltiger Kesselasche) über 1000 Stunden bei 600 °C ausgelagert wurden. Gegenüber der siliziumarmen Charge (Beispiel G) zeigt die erfindungsgemäße siliziu haltige Legierung einen deutlich verringerten Korrosionsangriff.The advantageous influence of silicon can also be seen in Figure 3, which shows the metallographically determined corrosion attack of samples which are in a complex medium (chlorine-containing synthetic waste combustion gas (2.5 g / m 3 HC1, 1.3 g / m 3 S0 2 / 9% 0 2 , remainder N 2 ) with simultaneous exposure to boiler ash containing chloride) were stored at 600 ° C for 1000 hours. Compared to the low-silicon batch (Example G), the silicon-containing alloy according to the invention shows a significantly reduced corrosion attack.
Abbildung 4 zeigt Korrosionsangriff nach 1008stündiger zyklischer Auslagerung von Proben, welche vor der Auslagerung bei 750 °C in einer chlor- und schwefeldioxidhaltigen Atmosphäre mit einem Belag aus Na2S04/KCl beschichtet wurden. Dieser Versuch dient der Prüfung der Beständigkeit gegen Sulphatkorrosion. Wie
der Abbildung zu entnehmen ist, zeigt auch bei dieser Korro- sionsbeanspruchung die erfindungsgemäße Legierung deutlich geringere Korrosionsraten auf, als die zur Zeit unter solchen Korrosionsbedingungen verwendete Legierung 2.4856.Figure 4 shows corrosion attack after 1008 hours of cyclical aging of samples which were coated with a coating of Na 2 S0 4 / KCl before being aged at 750 ° C in an atmosphere containing chlorine and sulfur dioxide. This test is used to test the resistance to sulphate corrosion. How as can be seen from the figure, the alloy according to the invention also shows significantly lower corrosion rates than the alloy 2.4856 currently used under such corrosion conditions with this corrosion stress.
Die hervorragenden Eigenschaften der erfindungsgemäßen Legierung sind auf die Siliziumzusätze und auf die Abstimmung der Legie- rungselemente Molybdän, Chrom und Eisen zurückzuführen. Der Siliziumgehalt der erfindungsgemäßen Legierung soll zwischen 0,6 % und 1,7 % liegen, da bei geringeren Siliziumgehalten die korro- sionshemmende Wirkung des Siliziums nicht mehr auftritt und bei höheren Siliziumgehalten verstärkt mit dem Auftreten versprodend wirkender Suizide und deutlichem Duktilitätsverlust , insbesondere bei mittleren Temperaturen (500-800 °C) , zu rechnen ist. Bei Siliziumgehalten zwischen 0,5 und 1,7 % sinkt die Kerbschlagzähigkeit, gemessen an ISO-V-Kerbschlagproben, selbst nach lOOOstündiger Auslagerung bei 600 °C nicht unter 100 J/cm, wie Abbildung 5 zeigt .The excellent properties of the alloy according to the invention can be attributed to the silicon additives and the coordination of the alloy elements molybdenum, chromium and iron. The silicon content of the alloy according to the invention should be between 0.6% and 1.7%, since at lower silicon contents the corrosion-inhibiting effect of the silicon no longer occurs and at higher silicon contents with the appearance of embrittling suicides and significant loss of ductility, particularly in the case of medium-sized ones Temperatures (500-800 ° C), can be expected. With silicon contents between 0.5 and 1.7%, the notched impact strength, measured on ISO V notched impact samples, does not drop below 100 J / cm, even after aging for 100 hours at 600 ° C, as shown in Figure 5.
Der Molybdängehalt der erfindungsgemäßen Legierung wird auf 10 % begrenzt, da, wie aus Abbildung 4 hervorgeht, bei höheren Molybdängehalten die Anfälligkeit gegen Sulphatkorrosion zunimmt. Ein Mindestmolybdängehalt ist erforderlich um Naßkorrosion im Falle von Taupunktunterschreitungen zu vermeiden.The molybdenum content of the alloy according to the invention is limited to 10%, since, as can be seen from FIG. 4, the susceptibility to sulphate corrosion increases with higher molybdenum contents. A minimum molybdenum content is required to avoid wet corrosion in the event of a drop below the dew point.
Der Chromgehalt der erfindungsgemäßen Legierung soll zwischen 18 % und 22 % betragen, um eine ausreichende Korrosionsbeständigkeit zu gewährleisten. Höhere Chromgehalte erschweren deutlich die Verarbeitbarkeit von Nickel-Chrom-Molybdän-Legierungen.
Die Legierung sollte darüber hinaus Hafnium und/oder Seltene Erden und/oder Zirkonium und/oder Yttrium enthalten, wenn für spezifische Anwendungen zum Beispiel in Automobilabgassystemen bei hohen Temperaturen und/oder bei schnellen Temperaturwechseln eine verbesserte Haftung schützender Oxidschichten gefordert wird. Die Summe an diesen reaktiven Elementen sollte jedoch 0,5 % nicht überschreiten.The chromium content of the alloy according to the invention should be between 18% and 22% in order to ensure adequate corrosion resistance. Higher chromium contents make it difficult to process nickel-chromium-molybdenum alloys. The alloy should also contain hafnium and / or rare earths and / or zirconium and / or yttrium, if an improved adhesion of protective oxide layers is required for specific applications, for example in automotive exhaust systems at high temperatures and / or with rapid temperature changes. However, the sum of these reactive elements should not exceed 0.5%.
Der Eisengehalt der erfindungsgemäßen Legierung wird auf maximal auf 5 % beschränkt, da bei höheren Eisengehalten in chloridhal- tigen Medien die Gefahr der Bildung leicht flüchtiger Eisenchloride besteht. Ein Mindesteisengehalt von 1 % ist jedoch erforderlich, um die Verarbeitbarkeit der Legierung zu gewährleisten.The iron content of the alloy according to the invention is limited to a maximum of 5%, since at higher iron contents in chloride-containing media there is a risk of the formation of volatile iron chlorides. However, a minimum iron content of 1% is required to ensure the processability of the alloy.
Der Kohlenstoffgehalt der erfindungsgemäßen Legierung wird auf maximal 0,05 % beschränkt, da bei höheren Kohlenstoffgehalten die Gefahr der interkristallinen Korrosion besteht.The carbon content of the alloy according to the invention is limited to a maximum of 0.05% since there is a risk of intergranular corrosion at higher carbon contents.
Die Gehalte an Titan und Aluminium werden jeweils auf maximal 0,5 %,- der eigentlich unerwünschte Niobgehalt auf max. 0,5 % beschränkt, da diese Elemente bei mittleren Temperaturen zu einem Duktilitätsverlust wegen der Bildung intermetallischer Phasen führen können. Die Gesamtsumme der Zusätze an Niob, Aluminium und Titan soll 1 % nicht überschreiten. Ein Mindestgehalt an den Sauerstoffäffinen Elementen Aluminium, Titan, Magnesium und Calcium ist jedoch erforderlich, um eine gute Oxidationsbestän- digkeit zu gewährleisten. Der Mangangehalt soll aus Verarbeitungsgründen mindestens 0,05 % betragen, jedoch nicht über 0,5 % hinausgehen, da sich höhere Mangangehalte ungünstig auf die Oxi- dationsbeständigkeit auswirken. Zur Verbesserung der Verarbeitbarkeit werden auch 0,001-0,01 % Bor zulegiert.
Die Gehalte an Phosphor und Schwefel sollten so gering wie möglich gehalten werden, da diese grenzflächenaktiven Elemente sowohl die Hochtemperaturkorrosionsbeständigkeit, als auch die Duktilität der Legierung verringern.The titanium and aluminum contents are each reduced to a maximum of 0.5%, the actually undesirable niobium content to a maximum of. 0.5% is limited, since these elements can lead to a loss of ductility due to the formation of intermetallic phases at medium temperatures. The total addition of niobium, aluminum and titanium should not exceed 1%. However, a minimum content of the oxygen-affine elements aluminum, titanium, magnesium and calcium is required to ensure good oxidation resistance. For processing reasons, the manganese content should be at least 0.05%, but not exceed 0.5%, since higher manganese contents have an unfavorable effect on the resistance to oxidation. 0.001-0.01% boron is also added to improve processability. The levels of phosphorus and sulfur should be kept as low as possible since these surface-active elements reduce both the high-temperature corrosion resistance and the ductility of the alloy.
Die erfindungsgemäße Legierung kann für Bänder, Folien, Bleche, Rohre (nahtlos oder geschweißt) , Drähte, als Auftragsschweißung, als Auftragsplattierung oder als Kompositrohr verwendet werden.The alloy according to the invention can be used for strips, foils, sheets, tubes (seamless or welded), wires, as cladding, as cladding or as a composite tube.
Die Herstellung der erfindungsgemäßen Legierung kann sowohl durch Blockguß als auch durch Strangguß nach Erschmelzung im Vakuuminduktionsofen oder nach offener Erschmelzung erfolgen. Ein Umschmelzen der Legierung kann erfolgen, ist aber nicht zwingend erforderlich. Die Warmformgebung erfolgt durch Schmieden, Warmwalzen oder Strangpressen, die Kaltformgebung durch Kaltwalzen, Drahtziehen oder Pilgern. Die Herstellung von Verbundwerkstoffen, beispielsweise das Plattieren auf Kohlenstoffstähle kann durch eines der üblichen Auftragsschweißverfahren, durch Kaltoder Warmwalzen von Blechen und Bändern, durch Sprengplattieren oder durch eines der üblichen Verfahren zur Herstellung von Bimetallrohren erfolgen.The alloy according to the invention can be produced either by block casting or by continuous casting after melting in a vacuum induction furnace or after open melting. The alloy can be remelted, but is not absolutely necessary. The hot shaping is carried out by forging, hot rolling or extrusion, the cold shaping by cold rolling, wire drawing or pilgrims. The production of composite materials, for example plating on carbon steels, can be carried out by one of the customary build-up welding processes, by cold or hot rolling of sheets and strips, by explosive plating or by one of the customary processes for producing bimetallic tubes.
Wegen ihrer ausgezeichneten Chlorierungsbeständigkeit kommt die Legierung insbesondere als Band und Blech, Rohr oder Plattiermaterial für den Einsatz in heißen chlorhaltigen Gasen oder in Anwesenheit chloridhaltiger Beläge in Frage, wie diese in Anlagen der chemischen Industrie, in Anlagen zur thermischen Behandlung von chlorhaltigen Chemieabfällen und kontaminierten Böden sowie in Automobilabgassystemen (Faltenbälge zur Entkopplung von Abgaskatalysator und Motor) auftreten. Die ausgezeichnete Beständigkeit der Legierung gegen komplexe korrosive Salzablagerungen
(Kesselasche) macht die Legierung auch geeignet für die Verwendung als Plattier- und Konstruktionswerkstoff in Anlagen zur thermischen Abfallentsorgung, in Großdieselmotoren, in Anlagen zur Energiegewinnung aus Biomasse und in Anlagen der Zellstoff- industrie.
Because of its excellent resistance to chlorination, the alloy is particularly suitable as a strip and sheet, pipe or cladding material for use in hot chlorine-containing gases or in the presence of chloride-containing deposits, such as in plants in the chemical industry, in plants for the thermal treatment of chlorine-containing chemical waste and contaminated soils as well as in automotive exhaust systems (bellows for decoupling the catalytic converter and engine). The excellent resistance of the alloy to complex corrosive salt deposits (Boiler ash) makes the alloy also suitable for use as a cladding and construction material in plants for thermal waste disposal, in large diesel engines, in plants for energy generation from biomass and in plants of the pulp industry.
Claims
1. Austenitische Nickel-Chrom-Molybdän-Legierung mit Zusätzen von Silizium gekennzeichnet durch die Legierungsbestandteile (in Masse-%)1. Austenitic nickel-chromium-molybdenum alloy with addition of silicon characterized by the alloy components (in mass%)
Cr 18 22 oCr 18 22 o
Mo 6 10 g,Mo 6 10 g,
00
Si 0,6 1,7 g, oSi 0.6 1.7 g, o
C 0,002 - 0,05 g,C 0.002 - 0.05 g,
00
Fe 1 5 g, "SFe 1 5 g, "S
Mn 0,05 - 0,5 %Mn 0.05 - 0.5%
AI 0,1 0,5 g,AI 0.1 0.5 g,
00
Ti 0,1 0,5 %Ti 0.1 0.5%
Mg 0,005 - 0,05 g, oMg 0.005-0.05 g, o
Ca 0,001 - 0,01 g. oCa 0.001-0.01 g. O
V max. , 0,5 oV max. , 0.5 o
P max. 0,02 g,P max. 0.02 g,
00
S max. . 0,01 g, oS max. . 0.01 g, o
B 0,001 - 0,01 g, oB 0.001 - 0.01 g, o
Cu max. , 0,5 g,Cu max. 0.5 g
00
Co max. . 1 g, oCo max. . 1 g, o
Hf und/oder Y und/oder Zr und/oder Seltene ErdenHf and / or Y and / or Zr and / or rare earths
0,02 - 0,5 g, o0.02 - 0.5 g, o
Rest Nickel und erschmelzungsbedingte Verunreinigungen,
Remainder nickel and melting-related impurities,
2. Legierung nach Anspruch 1, gekennzeichnet durch die Legierungsbestandteile (in Masse-%)2. Alloy according to claim 1, characterized by the alloy components (in% by mass)
Cr 18 - 20 g, oCr 18 - 20 g, o
Mo 8 - 9,0 %Mo 8 - 9.0%
Si 0, 7 - 1,1 g,Si 0.7 - 1.1 g,
00
C 0,02 - 0,015 %C 0.02 - 0.015%
Fe 2,5 - 3,5 g, oFe 2.5 - 3.5 g, o
Mn 0,05 - 0,1 g, oMn 0.05-0.1 g, o
AI 0,1 - 0,3 g. *oAI 0.1 - 0.3 g. * o
Ti 0,1 - 0,4 oTi 0.1 - 0.4 o
Mg 0,005 - 0,015 g„ oMg 0.005 - 0.015 g "o
Ca 0,001 - 0,005Approx. 0.001 - 0.005
V max. 0, 01 g, oV max. 0.01 g, o
P max. 0,002 g. oP max. 0.002 g. O
S max. 0,001 %S max. 0.001%
B 0,001 - 0, 001 g, oB 0.001-0.001 g, o
Cu ma . 0,5 g, oCu ma. 0.5 g, o
Hf und/oder Y und/oder Zr und/oder Seltene ErdenHf and / or Y and / or Zr and / or rare earths
0,03 - 0,06 %0.03 - 0.06%
Rest Nickel und erschmelzungsbedingte VerunreinigungenRemainder nickel and melting impurities
3. Legierung nach Anspruch 1, gekennzeichnet durch einen Molybdängehalt zwischen 6,5 und 9,5 %.3. Alloy according to claim 1, characterized by a molybdenum content between 6.5 and 9.5%.
4. Legierung nach Anspruch 1, gekennzeichnet durch einen Siliziumgehalt zwischen 0,6 und 1,3 %.4. Alloy according to claim 1, characterized by a silicon content between 0.6 and 1.3%.
5. Verwendung der Legierungen nach einem der Ansprüche 1 bis 4 zur Herstellung von Rohren, Blechen, Bandmaterial, Folien, Drähten sowie aus diesen Halbzeugen hergestellte Gegenstände.5. Use of the alloys according to one of claims 1 to 4 for the production of tubes, sheets, strip material, foils, wires and objects made from these semi-finished products.
6. Verwendung der Legierung nach einem der Ansprüche 1 bis 4 zur Herstellung von Kompositrohren.
6. Use of the alloy according to one of claims 1 to 4 for the production of composite pipes.
7. Verwendung der Legierung nach einem der Ansprüche 1 bis 4 als durch Auftragsschweißung oder Plattierung aufgebrachter Korrosionsschutz .
7. Use of the alloy according to one of claims 1 to 4 as corrosion protection applied by cladding or plating.
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19703035 | 1997-01-29 | ||
DE1997103035 DE19703035C2 (en) | 1997-01-29 | 1997-01-29 | Use of an austenitic nickel-chromium-molybdenum-silicon alloy with high corrosion resistance against hot chlorine-containing gases and chlorides |
PCT/EP1997/006592 WO1998032887A1 (en) | 1997-01-29 | 1997-11-26 | Austenitic nickel-chromium-molybdenum-silicon alloy with high corrosion resistance to hot chloride-containing gases and chloride |
Publications (1)
Publication Number | Publication Date |
---|---|
EP0956371A1 true EP0956371A1 (en) | 1999-11-17 |
Family
ID=7818575
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP97951980A Withdrawn EP0956371A1 (en) | 1997-01-29 | 1997-11-26 | Austenitic nickel-chromium-molybdenum-silicon alloy with high corrosion resistance to hot chloride-containing gases and chloride |
Country Status (5)
Country | Link |
---|---|
EP (1) | EP0956371A1 (en) |
JP (1) | JP2001509210A (en) |
CA (1) | CA2279294A1 (en) |
DE (1) | DE19703035C2 (en) |
WO (1) | WO1998032887A1 (en) |
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CN101899593B (en) * | 2010-04-06 | 2012-06-13 | 江苏立新合金实业总公司 | Nickel-chromium high-resistance electrothermal alloy |
CN102191409B (en) * | 2011-04-22 | 2012-07-04 | 江苏新华合金电器有限公司 | New high-resistance electrical heating alloy material and preparation method thereof |
CN104087769B (en) * | 2014-06-25 | 2017-02-15 | 盐城市鑫洋电热材料有限公司 | Method for improving properties of nickel-base electrothermal alloy |
CN104087768B (en) * | 2014-06-25 | 2017-02-15 | 盐城市鑫洋电热材料有限公司 | Method for improving performance of nickel-chromium-iron electrothermal alloy |
CN109722554B (en) * | 2018-12-22 | 2020-12-01 | 北京航空航天大学青岛研究院 | Method for reducing wettability between high-temperature alloy melt and oxide ceramic crucible |
JP7009666B1 (en) * | 2021-07-13 | 2022-02-15 | 日本冶金工業株式会社 | Ni—Cr—Mo alloy for welded pipes with excellent workability and corrosion resistance |
CN117535559A (en) * | 2024-01-10 | 2024-02-09 | 北京北冶功能材料有限公司 | Low-density nickel-based high-temperature alloy foil and preparation method and application thereof |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3272666A (en) * | 1963-12-09 | 1966-09-13 | Du Pont | Method of heat treating nickel base alloy articles up to 20 mils in thickness |
JPS5631345B2 (en) * | 1972-01-27 | 1981-07-21 | ||
US3785877A (en) * | 1972-09-25 | 1974-01-15 | Special Metals Corp | Treating nickel base alloys |
EP0092397A1 (en) * | 1982-04-20 | 1983-10-26 | Huntington Alloys, Inc. | Nickel-chromium-molybdenum alloy |
JPS6199649A (en) * | 1984-10-22 | 1986-05-17 | Kubota Ltd | Alloy for electrically conductive roll |
US4853183A (en) * | 1987-08-28 | 1989-08-01 | Chas S. Lewis & Co., Inc. | Air meltable castable corrosion resistant alloy and its process thereof |
SE513552C2 (en) * | 1994-05-18 | 2000-10-02 | Sandvik Ab | Use of a Cr-Ni-Mo alloy with good workability and structural stability as a component in waste incineration plants |
-
1997
- 1997-01-29 DE DE1997103035 patent/DE19703035C2/en not_active Expired - Fee Related
- 1997-11-26 EP EP97951980A patent/EP0956371A1/en not_active Withdrawn
- 1997-11-26 WO PCT/EP1997/006592 patent/WO1998032887A1/en not_active Application Discontinuation
- 1997-11-26 JP JP53151598A patent/JP2001509210A/en active Pending
- 1997-11-26 CA CA002279294A patent/CA2279294A1/en not_active Abandoned
Non-Patent Citations (1)
Title |
---|
See references of WO9832887A1 * |
Also Published As
Publication number | Publication date |
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DE19703035A1 (en) | 1998-07-30 |
WO1998032887A1 (en) | 1998-07-30 |
JP2001509210A (en) | 2001-07-10 |
CA2279294A1 (en) | 1998-07-30 |
DE19703035C2 (en) | 2000-12-07 |
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