DE1303517B - - Google Patents
Info
- Publication number
- DE1303517B DE1303517B DE19641303517D DE1303517DA DE1303517B DE 1303517 B DE1303517 B DE 1303517B DE 19641303517 D DE19641303517 D DE 19641303517D DE 1303517D A DE1303517D A DE 1303517DA DE 1303517 B DE1303517 B DE 1303517B
- Authority
- DE
- Germany
- Prior art keywords
- alloys
- oxidizing
- cobalt
- alloy
- tungsten
- 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
Links
- 239000000956 alloy Substances 0.000 claims description 20
- 229910045601 alloy Inorganic materials 0.000 claims description 20
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 claims description 13
- 230000001590 oxidative effect Effects 0.000 claims description 10
- 229910052748 manganese Inorganic materials 0.000 claims description 9
- 229910052710 silicon Inorganic materials 0.000 claims description 9
- 229910052715 tantalum Inorganic materials 0.000 claims description 9
- 229910052802 copper Inorganic materials 0.000 claims description 8
- 229910052750 molybdenum Inorganic materials 0.000 claims description 8
- 229910052759 nickel Inorganic materials 0.000 claims description 8
- 229910052758 niobium Inorganic materials 0.000 claims description 8
- 229910052720 vanadium Inorganic materials 0.000 claims description 8
- 229910052742 iron Inorganic materials 0.000 claims description 6
- 239000012535 impurity Substances 0.000 claims description 4
- 239000007788 liquid Substances 0.000 claims description 4
- 229910000713 I alloy Inorganic materials 0.000 claims 1
- PXHVJJICTQNCMI-UHFFFAOYSA-N nickel Substances [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 13
- 239000010949 copper Substances 0.000 description 9
- 230000004580 weight loss Effects 0.000 description 9
- 229910052804 chromium Inorganic materials 0.000 description 7
- 239000010955 niobium Substances 0.000 description 7
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 4
- GRYLNZFGIOXLOG-UHFFFAOYSA-N Nitric acid Chemical compound O[N+]([O-])=O GRYLNZFGIOXLOG-UHFFFAOYSA-N 0.000 description 4
- 239000002253 acid Substances 0.000 description 4
- 150000007513 acids Chemical class 0.000 description 4
- 238000009835 boiling Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 238000005260 corrosion Methods 0.000 description 4
- 239000011733 molybdenum Substances 0.000 description 4
- 229910017604 nitric acid Inorganic materials 0.000 description 4
- 229910052721 tungsten Inorganic materials 0.000 description 4
- GUCVJGMIXFAOAE-UHFFFAOYSA-N niobium atom Chemical compound [Nb] GUCVJGMIXFAOAE-UHFFFAOYSA-N 0.000 description 3
- GUVRBAGPIYLISA-UHFFFAOYSA-N tantalum atom Chemical compound [Ta] GUVRBAGPIYLISA-UHFFFAOYSA-N 0.000 description 3
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 3
- 239000010937 tungsten Substances 0.000 description 3
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 3
- NKRHXEKCTWWDLS-UHFFFAOYSA-N [W].[Cr].[Co] Chemical compound [W].[Cr].[Co] NKRHXEKCTWWDLS-UHFFFAOYSA-N 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 150000001247 metal acetylides Chemical class 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 238000003466 welding Methods 0.000 description 2
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 1
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 1
- TZVJRPRFJIXRGV-UHFFFAOYSA-N [Cr].[Co].[Ta] Chemical compound [Cr].[Co].[Ta] TZVJRPRFJIXRGV-UHFFFAOYSA-N 0.000 description 1
- HUESMFSDXNMSKD-UHFFFAOYSA-N [Nb].[Cr].[Co] Chemical compound [Nb].[Cr].[Co] HUESMFSDXNMSKD-UHFFFAOYSA-N 0.000 description 1
- YLMFVESASPUUTM-UHFFFAOYSA-N [V].[Cr].[Co] Chemical compound [V].[Cr].[Co] YLMFVESASPUUTM-UHFFFAOYSA-N 0.000 description 1
- 239000000654 additive Substances 0.000 description 1
- 239000003638 chemical reducing agent Substances 0.000 description 1
- 239000000788 chromium alloy Substances 0.000 description 1
- 238000005336 cracking Methods 0.000 description 1
- 150000002334 glycols Chemical class 0.000 description 1
- 238000011835 investigation Methods 0.000 description 1
- NFFIWVVINABMKP-UHFFFAOYSA-N methylidynetantalum Chemical compound [Ta]#C NFFIWVVINABMKP-UHFFFAOYSA-N 0.000 description 1
- ABLLXXOPOBEPIU-UHFFFAOYSA-N niobium vanadium Chemical compound [V].[Nb] ABLLXXOPOBEPIU-UHFFFAOYSA-N 0.000 description 1
- 239000007800 oxidant agent Substances 0.000 description 1
- 239000010703 silicon Substances 0.000 description 1
- 239000000126 substance Substances 0.000 description 1
- 229910003468 tantalcarbide Inorganic materials 0.000 description 1
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
- C22C38/30—Ferrous alloys, e.g. steel alloys containing chromium with cobalt
-
- 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
- C22C19/07—Alloys based on nickel or cobalt based on cobalt
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C27/00—Alloys based on rhenium or a refractory metal not mentioned in groups C22C14/00 or C22C16/00
- C22C27/06—Alloys based on chromium
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Soft Magnetic Materials (AREA)
Description
Mart legierungen auf Kobalt-Chrom-Wolfram-Basis haben nur eine geringe Beständigkeit gegenüber ausgesprochen oxydierend wirkenden Angriffsmedien. Wie Versuche /eigen, ist die I laiipiursache dieser haliene Wolfram. Tabelle I zeigt eine Legierung mit etwa 2"„ C und etua 30",, Cr. etwa 0.2",, Si Ivw. Mn. Rest Iiisen. in welcher das liisen nach und nach durch Co, W. Co ι W + Mo. Co + W + Mo -t- Cu undMart alloys based on cobalt-chromium-tungsten have only a low resistance to pronounced oxidizing attack media. Like attempts / own, the I laiipi cause is this haliene tungsten. Table I shows an alloy of about 2 "" C and about 30 "" Cr. about 0.2 ",, Si Ivw. Mn. Rest Iiisen. in which the liisen gradually through Co, W. Co ι W + Mo. Co + W + Mo -t- Cu and
geringen Beständigkeit das in den Legierungen ent- 5 Co -t- W ι Cu + Ni ersetzt wurde.low resistance that was replaced in the alloys ent- 5 Co -t- W ι Cu + Ni.
Chemische Zusammensetzung und Gewichtsverluste in g irrh in siedender 3()%iger Salpetersäure von Legierungen, die zur Ermittlung des Einflusses der einzelnen Legierungsbestandteile auf das KorrosionsverhaltenChemical composition and weight loss in g irrh in boiling 3 ()% nitric acid of alloys, to determine the influence of the individual alloy components on the corrosion behavior
von llartlegierungen erstellt werdenmade of alloys
1 j 2,251 j 2.25
2 j 2,182 j 2.18
3 2,153 2.15
4 2,184 2.18
5 2,185 2.18
6 2.186 2.18
7 2,307 2.30
8 2.268 2.26
Ί \K R1-.1 hercchnei.Ί \ K R1-.1 hercchnei.
Aus den gleichzeitig mit angegebenen Gewichtsverlusten bei Raum- und Siedetemperatur in 30%iger Salpetersäure geht die starke Steigerung der Gewichtsverlustzunahmc durch Wolfram hervor (Schmelze 3). Der gleichzeitige Zusatz von Kobalt in Schmelze 4 verringert zwar den Gewichtsverlust wieder, doch werden die -liedrigen Gewichtsverluste der wolframfreien Legierungen I und 2 nicht mehr erreicht. Die höchste Beständigkeit weisen somit Chrom-Kobalt-Legicrungcn auf, die sonst keine weiteren Zusatzelemente enthalten.From the weight losses specified at the same time as the room and boiling temperature in 30% Nitric acid is the major increase in weight loss gain through tungsten (melt 3). The simultaneous addition of cobalt in the melt 4 it reduces the weight loss again, but the -little weight losses become the tungsten-free Alloys I and 2 no longer achieved. Chromium-cobalt alloys therefore have the highest resistance which otherwise contain no additional elements.
Aus Untersuchungen über das Korrosionsverhalten von Karbiden ergab sich, daß Niob-Vanadin- und Tantalkarbid gegenüber oxydierender Beanspruchung sehr widerstandsfähig sind. Daraus ergibt sich die Möglichkeit, durch Zusatz dieser Elemente, die m der Martlegierung als Karbide vorliegen, deren Verschleißfestigkeit zu erhöhen, ohne dabei die Beständigkeit gegenüber oxydierenden Medien zu beeinträchtigen.Investigations into the corrosion behavior of carbides showed that niobium-vanadium and Tantalum carbide are very resistant to oxidizing stress. This results in the Possibility of adding these elements that m the Martalloy present as carbides, increasing their wear resistance without reducing the durability to impair against oxidizing media.
Versuche an llartlegierungen. welche Niob. Vanadin oder Tantal an Stelle von Wolfram enthalten, ergaben, daß die Gewichtsverluste in siedender 30%iger Salpetersäure sämtlich unter I g m2h und im Durchschnitt bei 0.5 g m2h liegen. Märtewcrle wurden zwischen 53 und 61 Rc gemessen.Tests on alloys. which niobium. Containing vanadium or tantalum instead of tungsten showed that the weight losses in boiling 30% nitric acid are all below 1 gm 2 h and on average 0.5 gm 2 h. Martial circles were measured between 53 and 61 Rc.
Der Legicrungsbereich der oben beschriebenen Martlegierungcn. die auch in oxydierend wirkenden Medien beständig sind, liegt innerhalb folgender Grenzen: 0.3 bis 4.0% C. 15 bis 40% Cr. 0 bis }.y,, Si. 0 bis 2.0% Mn. 38 bis 80% Co. 2.5 bis 18",, Nb. Ta oder V. einzeln oder zu mehreren. Rest Eisen, insbesondere 0,7 bis 2,5% C. 28 bis 30% Cr. 0.15 bisThe alloy range of the martial alloys described above. which are also resistant to oxidizing media, lies within the following limits: 0.3 to 4.0% C. 15 to 40% Cr. 0 to } .y ,, Si. 0 to 2.0% Mn. 38 to 80% Co. 2.5 to 18 ",, Nb. Ta or V. individually or in groups. The remainder is iron, in particular 0.7 to 2.5% C. 28 to 30% Cr. 0.15 to
tudo
NiNi
Il-Il-
ii.· in jj nr'liii. · in jj nr'li
0.45% Si, 0,06 bis 0,32% Mn, 45 bis 60% Co. 2,5 bis 18% Nb. Ta oder V, Rest Eisen. Bei Siliziumgehalten über 1% werden die Fließeigenschaften des Schmelzbades beim Sehweißen günstig beeinflußt.0.45% Si, 0.06 to 0.32% Mn, 45 to 60% Co. 2.5 to 18% Nb. Ta or V, remainder iron. With silicon contents The flow properties of the melt pool are above 1% favorably influenced in vision welding.
Weiter wurde gefunden, daß man auch bei den Hartlegierungen auf der Kobalt-Chrom-Niob- bzw. Kobalt-Chrom-Tantal- und Kobalt-Chrom-Vanadin-Basis durch Zusatz von Kupfer, Molybdän und Nickel in reduzierenden Säuren eine ebenso hohe Korrosionsbeständigkeit erlangen kann wie bei den Martlegierungcn auf Kobalt-Chrom-Wolfram-Basis, sofern Kupfer. Molybdän und Nickel gemeinsam zugesetzt werden, wobei Kupfcrgchalte von 0.2 bis 6%. Molybdängehaitc von 0,3 bis 6% und Nickeluehalte von 0.5 bis 10% bei entsprechender Erniedrigung des Kobaltgehaltcs wirksam und von technischem Interesse sind. Die niob-, tantal- und vanadinhaltigen Hartlcgierungen mit entsprechenden Zusätzen weisen somit eine hohe Korrosionsbeständigkeit sowohl in reduzierend wirkenden als auch in oxydierend wirkenden Säuren auf.It was also found that hard alloys based on cobalt-chromium-niobium or Cobalt-chromium-tantalum and cobalt-chromium-vanadium base through the addition of copper, molybdenum and nickel Corrosion resistance can be as high in reducing acids as in martial alloys on a cobalt-chromium-tungsten basis, provided copper. Molybdenum and nickel added together with copper content of 0.2 to 6%. Molybdenum content c from 0.3 to 6% and nickel content from 0.5 to 10% with a corresponding reduction in the Cobalt contents are effective and of technical interest. Hard alloys containing niobium, tantalum and vanadium with appropriate additives thus have a high level of corrosion resistance in both reducing as well as oxidizing acids.
Zur Bestätigung dieser Aussage sind die Gewichtsverluste in Schwefel- und Salpetersäure für eine Versuchslegierung mit folgender Zusammensetzung wiedergegeben:The weight losses in sulfuric and nitric acid for a test alloy are used to confirm this statement reproduced with the following composition:
1. 1.84% C. 1.24% Si. 0.2% Mn. 28.6% Cr. 5.0% Nb. 6.2% Ni. 3.55% Mo. 1.5% Cu. 2.6",. Fe. Rest Co.1. 1.84% C. 1.24% Si. 0.2% Mn. 28.6% Cr. 5.0% Nb. 6.2% Ni. 3.55% Mo.1.5% Cu. 2.6 ",. Fe. Rest Co.
2. 1.87% C. 1.10% Si. 0.32% Mn. 29.5% Cr. 4.72%, Ta. 7.5% Ni. 3.74% Mo. 1.48% Cu. 3.5% Fc. Rest Co.2.187% C. 1.10% Si. 0.32% Mn. 29.5% Cr. 4.72%, Ta. 7.5% Ni. 3.74% Mo. 1.48% Cu. 3.5% Fc. Rest Co.
3. I.98%C. 1.17% Si. 0.17% Mn. 28.4% Cr. 5.24",, V. 7.8% Ni, 3.46% Mo. 1.65% Cu, 3.12% Fc. Rest Co.3. I. 98% C. 1.17% Si. 0.17% Mn. 28.4% Cr. 5.24 ",, V. 7.8% Ni, 3.46% Mo. 1.65% Cu, 3.12% Fc. Balance Co.
Vcrsiichstempcriitiir RaumtemperaturVeristempriitiir Room temperature
10%10%
0.008 0.012 0,0090.008 0.012 0.009
0.72 0.84 0.940.72 0.84 0.94
20%20%
0.011 0.014 0,0130.011 0.014 0.013
1.13 1.14 1.251.13 1.14 1.25
10%10%
0,003 0,007 0.0070.003 0.007 0.007
0.09 0,11 0.130.09 0.11 0.13
0.003
0.008
0.0080.003
0.008
0.008
0.20.2
0.270.27
0,240.24
0.003
0.005
0.0080.003
0.005
0.008
0.6
0.8
0.650.6
0.8
0.65
40%40%
0,003 0.003 0,0060.003 0.003 0.006
1.11.1
1.251.25
1.351.35
Die angerührten Gewichtsverluste /eigen, duIi diese l.egierungslypen sowohl in reduzierend wirkenden ;iis auch in oxydierend wirkenden Säuren beständig sind. Auch im Verschleißverhallen sind diese Eegieningstypen den vergleichbaren woliranihaltigen Legierungstypen üherlegen. Weiler sind sie beim AuI-sehweißen weniger rißanfällig als die entsprechenden wolframhiilligen Legierungen.The touched weight losses / own, youIi this 1. Alloy glycols are resistant to reducing acids as well as oxidizing acids are. These types of energy are also subject to wear and tear the comparable types of alloy containing wolirani overlay. Hamlet they are at the outside welding less susceptible to cracking than the corresponding tungsten-enveloping alloys.
Gegenstand der Erfindung ist somit die Verwendung von llartlegierungen mit 0.3 bis 4.0% C, 15 bis 40% Cr, 0 bis 3,5% Si, 0 bis 2% Mn. 3« bis M)'!··„ Co. 2.5 bis 18% Nb, Ta, V einzeln oder zu mehreren. Rest Iiisen und unvermeidbare Verunreinigungen für den Einsatz in oxydierend wirkenden flüssigen AngrilTsmedien und die Verwendung von Hartlegierungen mit 0.3 bis 4,0% C, 15 bis 40% Cr, 0 bis 3,5% Si.0 bis 2.0% Mn. 38 bis 80% Co. 2,5 bis 18% Niob, Tantal, Vanadin einzeln oder zu inehreren, 0,2 bis 6% Kupfer, 0,3 bis 6% Molybdän und 0,5 bis 10% Nickel, Rest Eisen und unvermeidbare Verunreinigungen für den Einsatz in oxydierend und oder reduzierend wirkenden flüssigen Angriffsmedien.The subject of the invention is therefore the use of llart alloys with 0.3 to 4.0% C, 15 to 40% Cr, 0 to 3.5% Si, 0 to 2% Mn. 3 "to M)"! ·· "Co. 2.5 to 18% Nb, Ta, V individually or in groups. Residual iron and unavoidable impurities for use in oxidizing liquid attack media and the use of hard alloys with 0.3 up to 4.0% C, 15 to 40% Cr, 0 to 3.5% Si, 0 to 2.0% Mn. 38 to 80% Co. 2.5 to 18% niobium, tantalum, vanadium individually or in several, 0.2 to 6% copper, 0.3 to 6% molybdenum and 0.5 to 10% nickel, the remainder iron and unavoidable impurities for use in oxidizing and / or reducing agents liquid attack media.
Claims (2)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DEB0079109 | 1964-10-28 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE1303517B true DE1303517B (en) | 1971-12-23 |
Family
ID=6980170
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19641303517D Pending DE1303517B (en) | 1964-10-28 | 1964-10-28 |
Country Status (2)
| Country | Link |
|---|---|
| AT (1) | AT259880B (en) |
| DE (1) | DE1303517B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1995025826A1 (en) * | 1994-03-18 | 1995-09-28 | Ksb Aktiengesellschaft | Corrosion and wear-resistant chill casting |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| AT383030B (en) * | 1984-04-06 | 1987-05-11 | Ver Edelstahlwerke Ag | DENTAL ALLOY |
-
1964
- 1964-10-28 DE DE19641303517D patent/DE1303517B/de active Pending
-
1965
- 1965-09-07 AT AT815565A patent/AT259880B/en active
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO1995025826A1 (en) * | 1994-03-18 | 1995-09-28 | Ksb Aktiengesellschaft | Corrosion and wear-resistant chill casting |
Also Published As
| Publication number | Publication date |
|---|---|
| AT259880B (en) | 1968-02-12 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| E77 | Valid patent as to the heymanns-index 1977 |