US2186710A - Steel alloy - Google Patents
Steel alloy Download PDFInfo
- Publication number
- US2186710A US2186710A US393835A US39383529A US2186710A US 2186710 A US2186710 A US 2186710A US 393835 A US393835 A US 393835A US 39383529 A US39383529 A US 39383529A US 2186710 A US2186710 A US 2186710A
- Authority
- US
- United States
- Prior art keywords
- chromium
- titanium
- nickel
- carbon
- alloy
- 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.)
- Expired - Lifetime
Links
- 229910000851 Alloy steel Inorganic materials 0.000 title description 15
- 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 17
- 229910045601 alloy Inorganic materials 0.000 description 17
- 239000000956 alloy Substances 0.000 description 17
- 229910052799 carbon Inorganic materials 0.000 description 17
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 14
- 239000010936 titanium Substances 0.000 description 14
- 229910052719 titanium Inorganic materials 0.000 description 14
- VNNRSPGTAMTISX-UHFFFAOYSA-N chromium nickel Chemical compound [Cr].[Ni] VNNRSPGTAMTISX-UHFFFAOYSA-N 0.000 description 9
- 229910052759 nickel Inorganic materials 0.000 description 9
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 8
- 229910052804 chromium Inorganic materials 0.000 description 8
- 239000011651 chromium Substances 0.000 description 8
- 239000000470 constituent Substances 0.000 description 6
- 239000000126 substance Substances 0.000 description 6
- 238000003466 welding Methods 0.000 description 6
- 229910052720 vanadium Inorganic materials 0.000 description 5
- GPPXJZIENCGNKB-UHFFFAOYSA-N vanadium Chemical compound [V]#[V] GPPXJZIENCGNKB-UHFFFAOYSA-N 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 238000010276 construction Methods 0.000 description 4
- 238000010438 heat treatment Methods 0.000 description 4
- 238000012360 testing method Methods 0.000 description 4
- 229910000831 Steel Inorganic materials 0.000 description 3
- VHHVGPDQBHJHFB-UHFFFAOYSA-N [Ti].[Cr].[Ni] Chemical compound [Ti].[Cr].[Ni] VHHVGPDQBHJHFB-UHFFFAOYSA-N 0.000 description 3
- 239000010959 steel Substances 0.000 description 3
- 150000001875 compounds Chemical class 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 229910052739 hydrogen Inorganic materials 0.000 description 2
- 239000001257 hydrogen Substances 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- 206010011416 Croup infectious Diseases 0.000 description 1
- UFHFLCQGNIYNRP-UHFFFAOYSA-N Hydrogen Chemical compound [H][H] UFHFLCQGNIYNRP-UHFFFAOYSA-N 0.000 description 1
- 235000014676 Phragmites communis Nutrition 0.000 description 1
- QAOWNCQODCNURD-UHFFFAOYSA-N Sulfuric acid Chemical compound OS(O)(=O)=O QAOWNCQODCNURD-UHFFFAOYSA-N 0.000 description 1
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 description 1
- 239000013043 chemical agent Substances 0.000 description 1
- UFGZSIPAQKLCGR-UHFFFAOYSA-N chromium carbide Chemical compound [Cr]#C[Cr]C#[Cr] UFGZSIPAQKLCGR-UHFFFAOYSA-N 0.000 description 1
- 230000002939 deleterious effect Effects 0.000 description 1
- 230000001066 destructive effect Effects 0.000 description 1
- 150000002431 hydrogen Chemical class 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000005259 measurement Methods 0.000 description 1
- 150000001247 metal acetylides Chemical class 0.000 description 1
- 229910052760 oxygen Inorganic materials 0.000 description 1
- 239000001301 oxygen Substances 0.000 description 1
- 238000001556 precipitation Methods 0.000 description 1
- 238000003303 reheating Methods 0.000 description 1
- 235000011149 sulphuric acid Nutrition 0.000 description 1
- 239000001117 sulphuric acid Substances 0.000 description 1
- 229910003470 tongbaite Inorganic materials 0.000 description 1
- MTPVUVINMAGMJL-UHFFFAOYSA-N trimethyl(1,1,2,2,2-pentafluoroethyl)silane Chemical compound C[Si](C)(C)C(F)(F)C(F)(F)F MTPVUVINMAGMJL-UHFFFAOYSA-N 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
- C22C38/40—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
Definitions
- titanium or vanadium which forms a stable chemical compound with a portion of the carbon dissolved in the austenitic 3 base structure.
- the proportion of this alloy constituent to the carbon is so determined that v practically all the carbon is bound to this alloy constituent which means, of course, that in the case of titanium, for example, the alloy will be 40 made to contain sufllcient titanium to aflord an opportunity for practically all of the carbon to combine with the titanium to form titanium carbide.
- Our invention is of particular value in connection with articles of welded construction, for use in the chemical and metallurgical fields, which, without being annealed after welding, stubbornly resist intergranular corrosion within the zone tempered by the welding operation, (that is to say, maintained by such operation for an appreciable period of time within the deleterious temperature range referred to) when subjected to corroding media, because substantially the whole of the carbon in the alloy is in stable combination with the additional alloy constituent.
- the proportion of carbon in such articles of welded construction is a small one, being less than 1%.
- the proportion of chromium is from 18-25% and the proportion of nickel from 7-12%, but it should be understood that a departure from one or the other of such ranges, to an extent which leaves the proportion of the ingredient approximate to the range specifled, would be within the spirit of our invention and embody the advantages thereof.
- An article of welded construction for use in the chemical and metallurgical fields which, without being annealed after welding, stubbornly resists intergranular corrosion within the zone tempered by the welding operation when subjected to corroding media, and which is made of a stable austenitic alloy composed of approximately iii-% chromium, approximately 7-12% nickel, a small proportion of carbon and an additional alloy constituent having the property possessed by titanium of forming a stable chemical compound with the carbon of said alloy, the ratio of said additional alloy constituent to the carbon being such that practically the whole oi the latter is bound thereto, the balance bein substantially all iron.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Steel (AREA)
Description
PatentcdJan. 1:940
UNITED STATES "PATENT OFFICE STEEL ALLOY Paul Schafmeistcr and Eduard Houdrcmont,
Essen, Germany, alsignors, by memo assignments, to Krupp Nirosta Company, Inc., New York, N. Y., a corporation of Delaware No Drawing. Application September 19. 1029,
Serial No. 393,835. In
4 Claims.
- C. which can be compared to a drawing treatment, as occurs for instance in welding constructional parts. It has already been proposed, with satisfying results to employ for the manufacture of objects of austenitic chromium-nickel steel al- 1' loys which either in their manufacture or during service are exposed to a heating equivalent to .tion by adding to the austenitic chromiumnickel steel alloys, for instance to those containing 18 to 25% of chromium and '7 to 12% of nickel, toi prevent them from becoming brittle 30 when heated up to the chromium carbide precipitation range of about 500 to 800 degrees 0., an alloy constituent, e. g. titanium or vanadium, which forms a stable chemical compound with a portion of the carbon dissolved in the austenitic 3 base structure. The proportion of this alloy constituent to the carbon is so determined that v practically all the carbon is bound to this alloy constituent which means, of course, that in the case of titanium, for example, the alloy will be 40 made to contain sufllcient titanium to aflord an opportunity for practically all of the carbon to combine with the titanium to form titanium carbide.
Tests made with two chromium-nickel steel 5- alloys that contained about 18% of chromium, 9% of nickel, 0.12% of carbon, and, respectively,
' 0.5 and 2% of titanium, have shown that steel alloys of this type are fully resistant to active chemical attacks even when in. a condition re- 60 sulting from exposure toa heating up to about 500 to 800 degrees C. without a subsequent high heat treatment. Measurements ofthe magnetic saturation made to investigate the structure have shown that the values of the magnetic saturation ll of the material when quenched and drawn, are
Germany June 28, I929 not substantially higher than those of the magnetic saturation of the same material when merely quenched. For comparison purposes it may be noted that the corresponding values of a titaniumless austenitic chromium-nickel steel alloy are far higher in the temperature range of 500 to 800 degrees C. than in cooled state. The fact that the values of saturation are practically equal in the reheated and in the quenched state,
in contradistinction to titaniumless chromiuml0 1 nickel. steels, proves that in the titanium-chromium-nickel steel alloys the drawing operation is much less capable of altering the nature of the base structure than in the corresponding titaniumless chromium-nlckel-steel alloys. In the inventors opinion the reason for this phenomenon resides in the following:
The presence of titanium or vanadium or of a mixture of both these substances has the eifect that nearly the entire carbon is bound'to the titanium or vanadium in a manner not jeopardising the chemical stability of the alloy, so that the base structure which as to the rest is austenitic, practically is free of dissolved carbon, which therefore cannot assume another form causing the alloy to become brittle when the alloy is heated to-about 500 to 800 degrees 0.
Potential tests made with the above two titanium-chromium-nickel steel alloys have shown that these alloys even after having been drawn to about 500 to 800 degrees C. and tested in a solution of sulphuric acid 01' 5% at room temperature and practically i'reed of oxygen by evacuation, possess a potential that is above the potential' of hydrogen, whilst corresponding chromium-nickel-steel alloys that do not contain titanium, after reheating and under equal other conditions, show a potential which is below that of hydrogen. The addition of titanium therefore causes an increase of the potential beyond 40 that ofhydrogen and thus an increase of the chemical stability, whereby these alloys are made resistant tov very severe attacks by chemical agents and more particularly are protected from becoming brittle under the action of adrawing treatment.
In a corresponding manner two chromiumnickel steel alloys have been tested which contain about 18%; ,of chromium, 9% of nickel, 0.12% of carbon and; respectively, 0.5 and 2% of vanadium. The results of these tests corresponded in all substantial points to those obtained in testing the'x'above chromium-nickel titanium steel alloy.
It is to be understood that the temperature range" of 500 to 800 C. referred to in the foregoing specification is not intended to represent any specific outside limits of the range, but rather to indicate the approximate nature of heat treatment which is employed; for example, a.
temperature range such as is imparted as the result of a welding operation to that section of welded plates or the like where the destructive effect would manifest itself with ordinary austenitic chromium nickel steel alloys.
Any other elements, or mixtures of elements which have the property possessed by titanium of being able to combine with carbon to form stable carbides in austenitic chromium nickel steel alloys in the manner hereinabove described would constitute equivalents of the titanium for the purpose of our invention insofar as the same relates to welded articles.
Our invention is of particular value in connection with articles of welded construction, for use in the chemical and metallurgical fields, which, without being annealed after welding, stubbornly resist intergranular corrosion within the zone tempered by the welding operation, (that is to say, maintained by such operation for an appreciable period of time within the deleterious temperature range referred to) when subjected to corroding media, because substantially the whole of the carbon in the alloy is in stable combination with the additional alloy constituent. The proportion of carbon in such articles of welded construction is a small one, being less than 1%.
In the broader form of our invention which we have given by way of instance, the proportion of chromium is from 18-25% and the proportion of nickel from 7-12%, but it should be understood that a departure from one or the other of such ranges, to an extent which leaves the proportion of the ingredient approximate to the range specifled, would be within the spirit of our invention and embody the advantages thereof.
The invention with reference to the species embodying vanadium is claimed in our application Ser. No. 276,230, filed May 26, 1939.
What we claim is:
1. An article of welded construction for use in the chemical and metallurgical fields which, without being annealed after welding, stubbornly resists intergranular corrosion within the zone tempered by the welding operation when subjected to corroding media, and which is made of a stable austenitic alloy composed of approximately iii-% chromium, approximately 7-12% nickel, a small proportion of carbon and an additional alloy constituent having the property possessed by titanium of forming a stable chemical compound with the carbon of said alloy, the ratio of said additional alloy constituent to the carbon being such that practically the whole oi the latter is bound thereto, the balance bein substantially all iron.
2. An article of welded construction as defined in claim 1, in which the proportion of chromium in the alloy is approximately 18% and the proportion of nickel is approximately 9%.
3. An austenitic chromium nickel steel alloy containing approximately 18-25% chromium, approximately '712% nickel, a small proportion of carbon, and titanium in a proportion suflicient to combine with practically the whole of the carbon in stable combination, the balance being substantially all iron.
4. An austenitic chromium nickel steel alloy as defined in claim 3, in which the proportion of chromium is approximately 18%, that of nickel is approximately 9%, that of carbon is approximately .12%, and that of titanium is approximately .5% to 2%.
PAUL SCHAFMEISTER. EDUARD HOUDREMONT.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US276230A US2187525A (en) | 1929-09-19 | 1939-05-27 | Article of welded construction |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| DE2186710X | 1929-06-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US2186710A true US2186710A (en) | 1940-01-09 |
Family
ID=7989136
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US393835A Expired - Lifetime US2186710A (en) | 1929-06-26 | 1929-09-19 | Steel alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US2186710A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2531155A (en) * | 1945-11-06 | 1950-11-21 | Carnegie Illinois Steel Corp | Stainless steel |
-
1929
- 1929-09-19 US US393835A patent/US2186710A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2531155A (en) * | 1945-11-06 | 1950-11-21 | Carnegie Illinois Steel Corp | Stainless steel |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4099966A (en) | Austenitic stainless steel | |
| JPS6128738B2 (en) | ||
| GB1582504A (en) | Anticorrosive bellows | |
| JPS6036649A (en) | Precipitation hardening martensitic stainless steel with superior toughness | |
| US2999039A (en) | Martensitic steel | |
| US3171738A (en) | Austenitic stainless steel | |
| US4002510A (en) | Stainless steel immune to stress-corrosion cracking | |
| KR0166357B1 (en) | Iron-chromium-nickel-silicon alloys for steel instruments that are resistant to high temperature concentrated sulfuric acid or fuming sulfuric acid and steel appliances manufactured therefrom | |
| US2955934A (en) | High temperature alloy | |
| US3168397A (en) | Steel alloy | |
| US2186710A (en) | Steel alloy | |
| US2083524A (en) | Corrosion resistant alloy | |
| US2909425A (en) | Austenitic cr-mn-c-n steels for elevated temperature service | |
| US2187525A (en) | Article of welded construction | |
| US2251163A (en) | Corrosion resistant alloy | |
| EP0169373A1 (en) | Machines or machine parts made of austenitic cast iron having resistance to stress corrosion cracking | |
| US2138289A (en) | Chromium-manganese-nickel steel | |
| GB1564243A (en) | Austenitic stainless steel | |
| US3257200A (en) | Alloy steel for elevated temperature service | |
| JPS5827958A (en) | Spring steel with excellent fatigue resistance | |
| US2891859A (en) | Alloy steel | |
| US2315156A (en) | Low-alloy corrosion-resistant steel | |
| US3316085A (en) | Martensitic stainless steel | |
| US2246445A (en) | Stabilization of austenitic chromium nickel steels | |
| US2001123A (en) | Stable chromium-nickel-iron alloy |