US2109285A - Alloy - Google Patents
Alloy Download PDFInfo
- Publication number
- US2109285A US2109285A US133267A US13326737A US2109285A US 2109285 A US2109285 A US 2109285A US 133267 A US133267 A US 133267A US 13326737 A US13326737 A US 13326737A US 2109285 A US2109285 A US 2109285A
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- United States
- Prior art keywords
- alloys
- silicon
- carbon
- alloy
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- Prior art date
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- 239000000956 alloy Substances 0.000 title description 28
- 229910045601 alloy Inorganic materials 0.000 title description 28
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 18
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 16
- 229910052799 carbon Inorganic materials 0.000 description 16
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 15
- 229910052710 silicon Inorganic materials 0.000 description 15
- 239000010703 silicon Substances 0.000 description 15
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 10
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 9
- 229910052804 chromium Inorganic materials 0.000 description 9
- 239000011651 chromium Substances 0.000 description 9
- 230000007797 corrosion Effects 0.000 description 9
- 238000005260 corrosion Methods 0.000 description 9
- 229910052759 nickel Inorganic materials 0.000 description 9
- VEXZGXHMUGYJMC-UHFFFAOYSA-N Hydrochloric acid Chemical compound Cl VEXZGXHMUGYJMC-UHFFFAOYSA-N 0.000 description 8
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 8
- 229910052750 molybdenum Inorganic materials 0.000 description 8
- 239000011733 molybdenum Substances 0.000 description 8
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 6
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 6
- 229910052802 copper Inorganic materials 0.000 description 6
- 239000010949 copper Substances 0.000 description 6
- 229910052748 manganese Inorganic materials 0.000 description 6
- 239000011572 manganese Substances 0.000 description 6
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 6
- 229910052721 tungsten Inorganic materials 0.000 description 6
- 239000010937 tungsten Substances 0.000 description 6
- 229910052742 iron Inorganic materials 0.000 description 5
- 239000003518 caustics Substances 0.000 description 4
- 239000012535 impurity Substances 0.000 description 3
- WPBNNNQJVZRUHP-UHFFFAOYSA-L manganese(2+);methyl n-[[2-(methoxycarbonylcarbamothioylamino)phenyl]carbamothioyl]carbamate;n-[2-(sulfidocarbothioylamino)ethyl]carbamodithioate Chemical compound [Mn+2].[S-]C(=S)NCCNC([S-])=S.COC(=O)NC(=S)NC1=CC=CC=C1NC(=S)NC(=O)OC WPBNNNQJVZRUHP-UHFFFAOYSA-L 0.000 description 3
- 239000000470 constituent Substances 0.000 description 2
- 230000001627 detrimental effect Effects 0.000 description 2
- 230000002708 enhancing effect Effects 0.000 description 2
- 229910052720 vanadium Inorganic materials 0.000 description 2
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 2
- 239000002253 acid Substances 0.000 description 1
- 150000007513 acids Chemical class 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000001747 exhibiting effect Effects 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
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
- C22C19/057—Alloys based on nickel or cobalt based on nickel with chromium and Mo or W with the maximum Cr content being less 10%
Definitions
- This invention relates to alloys exhibiting unusual resistance to attack by corrosive agents and more particularly to nickel base alloys having a high percentage of molybdenum and which 5 are highly resistant to attack by solutions containing hydrochloric acid.
- alloys possessing good resistance to acids andv corrosive agents generally can be produced by combining molybdenum and a predominating amount of nickel. Alloys of this type are disclosed in Patents 1,375,082 and 1375,0813 to Clements; 1,'710,445 to Becket; and
- compositions generally include one or more of the following: iron, chromium,
- Silicon and carbon in small amounts are present in the raw n materials used, and are thereby introduced into the alloys and in some instances are specified as constituents thereof.
- amounts of silicon ranging from 0.25, to 0.50% of the alloy are held to be useful in enhancing fluidity in the pour stage, while in Becket, up to 1.5%, but preferably below 0.5%, and in Franks up to 1%, but preferably between 0.25 and 1% of silicon is disclosed, presumably for the same purpose, i. e., of enhancing fluidity whereby ease of handling the alloy in the pour stage is increased.
- An object of my invention is to obtain alloys of improved corrosion resistance. Another object of my invention is to obtain alloys which are more resistant towards hot solutions containing hydrochloric acid than are the alloys now obtainable but which retain the desirable physical characteristics of said alloys now obtainable.
- the objects of my invention are accomplished by carefully-controlling the amount of impurities, especially carbon and silicon, introduced by intention or otherwise'intoelloys of the highmolybdenum nickel base type.
- impurities especially carbon and silicon
- all constituents which do not en- 55 hance the corrosion resistant property are regarded as impurities. This includes iron, chromium, manganese, copper and vanadium which, as pointed out, are added for purposes other than corrosion resistance.
- My alloys like those of the prior art, consist principally of nickel and molybdenum with or without the addition of smaller amounts of iron, manganese, tungsten, copper and other known modifying agents.
- the alloy should contain at least 20% by weight of molybdenum, the carbon content should be below 0.05%, and the silicon content below 0.10%.
- the amount of carbon and silicon should be reduced belowthese limits since further reduction is accompanied by further marked improvement in the corrosion resistance of 'the alloy.
- 'A preferred limit of carbon content within the critical limit above recited is below 0.02% carbon.
- the detrimental efiect of carbon and silicon is considerably increased when the two are present together. In no case should the total content of carbon and silicon exceed 0.15%.
- Chromium and manganese alone in amounts up to 1% are 'without appreciable influence on the corrosion resistance of alloys of the highmolybdenum nickel base type.
- the simultaneous presence of chromium or manganese with appreciable amounts of carbon and silicon is definitely detrimental.
- the carbon content is above approximately 0.025% and/or silicon is present to the extent of 0.10% or more, the presence of chromium and manganese materially decreases the corrosion resistance of the alloy.
- my alloys will contain less than 0.05% carbon, less than 0.10% silicon and less than 0.25% total chromium and manganese, except where the carbon content is below 0.025% and silicon below 0.10%, in which case up to 1% chromium and/or manganese is permissible.
- the preferred ironccntent is 0 to 5% but may be as high as 10%, and the preferred molybdenum content 30 to 40% but may be as low as 28%. Up to 10% tungsten and 5% copper may be' added, the balance of the alloy being nickel in each case.
- Alloys resistant to corrosive agents consist of from 28 to 40% of molybdenum, small but eiTective amounts of iron up to 5%, of copper up to 5%, of tungsten up to 10%, chromium and manganese each in small but effective amounts andtotalling up to 0.25%, carbon up to 0.05%, silicon up to 0.10%, and the balance ofthe alloy being nickel.
- Alloys resistant to corrosive agents which consist of from 28 to 40% of molybdenum, small but effective amounts of iron up to 5%, of copper up to 5%, of tungsten up to 10%, of chromium'up to 1%, of manganese up to 1%, up to 0.025% of carbon, up to 010% silicon, and the balance of the alloy being nickel.
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- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Resistance Heating (AREA)
Description
Patented Feb. 22, 1938 PATENT OFFICE ALLOY Marshall B. Brown, Wilmington, DeL, assignor to E. I. du Pont de Nemours & Company, Wilmington, Del., a corporation of Delaware No Drawing. Application March 26, 1937, Serial No. 133,267
2 Claims.
This invention relates to alloys exhibiting unusual resistance to attack by corrosive agents and more particularly to nickel base alloys having a high percentage of molybdenum and which 5 are highly resistant to attack by solutions containing hydrochloric acid.
It is known that alloys possessing good resistance to acids andv corrosive agents generally can be produced by combining molybdenum and a predominating amount of nickel. Alloys of this type are disclosed in Patents 1,375,082 and 1375,0813 to Clements; 1,'710,445 to Becket; and
1,836,317 to Franks. In addition to molybdenum and nickel, these compositions generally include one or more of the following: iron, chromium,
and lesser amounts of copper, manganeseg tungsten and vanadium, specifically added to impart desired physical characteristics. Silicon and carbon in small amounts are present in the raw n materials used, and are thereby introduced into the alloys and in some instances are specified as constituents thereof. Thus in- Clements, amounts of silicon ranging from 0.25, to 0.50% of the alloy are held to be useful in enhancing fluidity in the pour stage, while in Becket, up to 1.5%, but preferably below 0.5%, and in Franks up to 1%, but preferably between 0.25 and 1% of silicon is disclosed, presumably for the same purpose, i. e., of enhancing fluidity whereby ease of handling the alloy in the pour stage is increased. Carbon appearsto be of more doubtful utility, although amounts up to 2% have been cited as permissible in previous practice. However,none of these added elements other than tungsten, contributes to the corrosion resistance of the alloys and I have found that when they are used in the amounts heretofore regarded as satisfactory, they in fact definitely lessen the resistance of the alloys to corrosion.
An object of my invention is to obtain alloys of improved corrosion resistance. Another object of my invention is to obtain alloys which are more resistant towards hot solutions containing hydrochloric acid than are the alloys now obtainable but which retain the desirable physical characteristics of said alloys now obtainable. These and other objects will more clearly appear hereinafter.
The objects of my invention are accomplished by carefully-controlling the amount of impurities, especially carbon and silicon, introduced by intention or otherwise'intoelloys of the highmolybdenum nickel base type. For purposes of my invention, all constituents which do not en- 55 hance the corrosion resistant property are regarded as impurities. This includes iron, chromium, manganese, copper and vanadium which, as pointed out, are added for purposes other than corrosion resistance.
My alloys, like those of the prior art, consist principally of nickel and molybdenum with or without the addition of smaller amounts of iron, manganese, tungsten, copper and other known modifying agents. The essential and most important difierence between my alloys and others previously described, is the specific limita tion of impurities, especially carbon and silicon,
which are normally present in appreciable amounts. The proportions in which the above elements may be combined will depend upon the particular corrosive to be handled and the physical properties, i. e., tensile strength, ductility, malleability, etc., required. For satisfactory resistance to hot hydrochloric acid solutions, I have found that the alloy should contain at least 20% by weight of molybdenum, the carbon content should be below 0.05%, and the silicon content below 0.10%. Preferably the amount of carbon and silicon should be reduced belowthese limits since further reduction is accompanied by further marked improvement in the corrosion resistance of 'the alloy. 'A preferred limit of carbon content within the critical limit above recited is below 0.02% carbon. I have also found that the detrimental efiect of carbon and silicon is considerably increased when the two are present together. In no case should the total content of carbon and silicon exceed 0.15%.
Chromium and manganese alone in amounts up to 1% are 'without appreciable influence on the corrosion resistance of alloys of the highmolybdenum nickel base type. However, the simultaneous presence of chromium or manganese with appreciable amounts of carbon and silicon is definitely detrimental. For example. if the carbon content is above approximately 0.025% and/or silicon is present to the extent of 0.10% or more, the presence of chromium and manganese materially decreases the corrosion resistance of the alloy. Preferably my alloys will contain less than 0.05% carbon, less than 0.10% silicon and less than 0.25% total chromium and manganese, except where the carbon content is below 0.025% and silicon below 0.10%, in which case up to 1% chromium and/or manganese is permissible.
The preferred ironccntent is 0 to 5% but may be as high as 10%, and the preferred molybdenum content 30 to 40% but may be as low as 28%. Up to 10% tungsten and 5% copper may be' added, the balance of the alloy being nickel in each case.
While corrosion resistance to hot hydrochloric acid solutions has been mentioned as the most important property of the improved alloys, they.
' following claims.
I claim:
1. Alloys resistant to corrosive agents which consist of from 28 to 40% of molybdenum, small but eiTective amounts of iron up to 5%, of copper up to 5%, of tungsten up to 10%, chromium and manganese each in small but effective amounts andtotalling up to 0.25%, carbon up to 0.05%, silicon up to 0.10%, and the balance ofthe alloy being nickel.
2. Alloys resistant to corrosive agents which consist of from 28 to 40% of molybdenum, small but effective amounts of iron up to 5%, of copper up to 5%, of tungsten up to 10%, of chromium'up to 1%, of manganese up to 1%, up to 0.025% of carbon, up to 010% silicon, and the balance of the alloy being nickel.-
MARSHALL H. BROWN.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US133267A US2109285A (en) | 1937-03-26 | 1937-03-26 | Alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US133267A US2109285A (en) | 1937-03-26 | 1937-03-26 | Alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2109285A true US2109285A (en) | 1938-02-22 |
Family
ID=22457777
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US133267A Expired - Lifetime US2109285A (en) | 1937-03-26 | 1937-03-26 | Alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2109285A (en) |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2900252A (en) * | 1954-06-15 | 1959-08-18 | Owens Corning Fiberglass Corp | Apparatus for contacting molten glass |
| US2959480A (en) * | 1956-11-19 | 1960-11-08 | Int Nickel Co | Corrosion resistant nickel-molybdenum alloys |
| US4168188A (en) * | 1978-02-09 | 1979-09-18 | Cabot Corporation | Alloys resistant to localized corrosion, hydrogen sulfide stress cracking and stress corrosion cracking |
| DE3839795A1 (en) * | 1987-11-27 | 1989-06-08 | Haynes Int Inc | NICKEL-BASED ALLOY WITH HIGH MOLYBDAEN CONTENT |
| EP0563720A1 (en) * | 1992-04-02 | 1993-10-06 | Krupp VDM GmbH | Austenitic nickel-molybdenum alloy |
| US6610119B2 (en) | 1994-07-01 | 2003-08-26 | Haynes International, Inc. | Nickel-molybdenum alloys |
| US20090004043A1 (en) * | 2007-06-28 | 2009-01-01 | Tawancy Hani M | Corrosion-resistant nickel-base alloy |
-
1937
- 1937-03-26 US US133267A patent/US2109285A/en not_active Expired - Lifetime
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2900252A (en) * | 1954-06-15 | 1959-08-18 | Owens Corning Fiberglass Corp | Apparatus for contacting molten glass |
| US2959480A (en) * | 1956-11-19 | 1960-11-08 | Int Nickel Co | Corrosion resistant nickel-molybdenum alloys |
| US4168188A (en) * | 1978-02-09 | 1979-09-18 | Cabot Corporation | Alloys resistant to localized corrosion, hydrogen sulfide stress cracking and stress corrosion cracking |
| DE3839795A1 (en) * | 1987-11-27 | 1989-06-08 | Haynes Int Inc | NICKEL-BASED ALLOY WITH HIGH MOLYBDAEN CONTENT |
| EP0563720A1 (en) * | 1992-04-02 | 1993-10-06 | Krupp VDM GmbH | Austenitic nickel-molybdenum alloy |
| US6610119B2 (en) | 1994-07-01 | 2003-08-26 | Haynes International, Inc. | Nickel-molybdenum alloys |
| US20090004043A1 (en) * | 2007-06-28 | 2009-01-01 | Tawancy Hani M | Corrosion-resistant nickel-base alloy |
| US7922969B2 (en) | 2007-06-28 | 2011-04-12 | King Fahd University Of Petroleum And Minerals | Corrosion-resistant nickel-base alloy |
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