US1538360A - Malleable noncorrodible alloy - Google Patents
Malleable noncorrodible alloy Download PDFInfo
- Publication number
- US1538360A US1538360A US279649A US27964919A US1538360A US 1538360 A US1538360 A US 1538360A US 279649 A US279649 A US 279649A US 27964919 A US27964919 A US 27964919A US 1538360 A US1538360 A US 1538360A
- Authority
- US
- United States
- Prior art keywords
- alloy
- malleable
- titanium
- per cent
- 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.)
- Expired - Lifetime
Links
- 229910045601 alloy Inorganic materials 0.000 title description 38
- 239000000956 alloy Substances 0.000 title description 38
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 32
- RTAQQCXQSZGOHL-UHFFFAOYSA-N Titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 24
- 229910052719 titanium Inorganic materials 0.000 description 24
- 239000010936 titanium Substances 0.000 description 24
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 22
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 22
- 229910052804 chromium Inorganic materials 0.000 description 22
- 239000011651 chromium Substances 0.000 description 22
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 17
- 230000007797 corrosion Effects 0.000 description 17
- 238000005260 corrosion Methods 0.000 description 17
- 230000003647 oxidation Effects 0.000 description 17
- 238000007254 oxidation reaction Methods 0.000 description 17
- 229910052710 silicon Inorganic materials 0.000 description 17
- 239000010703 silicon Substances 0.000 description 17
- 229910052759 nickel Inorganic materials 0.000 description 16
- 229910000831 Steel Inorganic materials 0.000 description 15
- 239000010959 steel Substances 0.000 description 15
- 229910052782 aluminium Inorganic materials 0.000 description 14
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 14
- 229910052742 iron Inorganic materials 0.000 description 11
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 8
- 229910052799 carbon Inorganic materials 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- 230000001590 oxidative effect Effects 0.000 description 7
- PWHULOQIROXLJO-UHFFFAOYSA-N Manganese Chemical compound [Mn] PWHULOQIROXLJO-UHFFFAOYSA-N 0.000 description 6
- 229910052748 manganese Inorganic materials 0.000 description 6
- 239000011572 manganese Substances 0.000 description 6
- 238000012937 correction Methods 0.000 description 5
- 239000003517 fume Substances 0.000 description 5
- 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 5
- 239000000463 material Substances 0.000 description 5
- 238000002844 melting Methods 0.000 description 5
- 230000008018 melting Effects 0.000 description 5
- 238000005336 cracking Methods 0.000 description 4
- 239000011248 coating agent Substances 0.000 description 3
- 238000000576 coating method Methods 0.000 description 3
- 230000006872 improvement Effects 0.000 description 3
- 239000007800 oxidant agent Substances 0.000 description 3
- IJGRMHOSHXDMSA-UHFFFAOYSA-N Atomic nitrogen Chemical compound N#N IJGRMHOSHXDMSA-UHFFFAOYSA-N 0.000 description 2
- 239000007789 gas Substances 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000004615 ingredient Substances 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 229910000604 Ferrochrome Inorganic materials 0.000 description 1
- OAICVXFJPJFONN-UHFFFAOYSA-N Phosphorus Chemical compound [P] OAICVXFJPJFONN-UHFFFAOYSA-N 0.000 description 1
- NINIDFKCEFEMDL-UHFFFAOYSA-N Sulfur Chemical compound [S] NINIDFKCEFEMDL-UHFFFAOYSA-N 0.000 description 1
- 239000005864 Sulphur Substances 0.000 description 1
- 230000009471 action Effects 0.000 description 1
- 238000010009 beating Methods 0.000 description 1
- BBBFJLBPOGFECG-VJVYQDLKSA-N calcitonin Chemical compound N([C@H](C(=O)N[C@@H](CC(C)C)C(=O)NCC(=O)N[C@@H](CCCCN)C(=O)N[C@@H](CC(C)C)C(=O)N[C@@H](CO)C(=O)N[C@@H](CCC(N)=O)C(=O)N[C@@H](CCC(O)=O)C(=O)N[C@@H](CC(C)C)C(=O)N[C@@H](CC=1NC=NC=1)C(=O)N[C@@H](CCCCN)C(=O)N[C@@H](CC(C)C)C(=O)N[C@@H](CCC(N)=O)C(=O)N[C@@H]([C@@H](C)O)C(=O)N[C@@H](CC=1C=CC(O)=CC=1)C(=O)N1[C@@H](CCC1)C(=O)N[C@@H](CCCNC(N)=N)C(=O)N[C@@H]([C@@H](C)O)C(=O)N[C@@H](CC(N)=O)C(=O)N[C@@H]([C@@H](C)O)C(=O)NCC(=O)N[C@@H](CO)C(=O)NCC(=O)N[C@@H]([C@@H](C)O)C(=O)N1[C@@H](CCC1)C(N)=O)C(C)C)C(=O)[C@@H]1CSSC[C@H](N)C(=O)N[C@@H](CO)C(=O)N[C@@H](CC(N)=O)C(=O)N[C@@H](CC(C)C)C(=O)N[C@@H](CO)C(=O)N[C@@H]([C@@H](C)O)C(=O)N1 BBBFJLBPOGFECG-VJVYQDLKSA-N 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 230000006866 deterioration Effects 0.000 description 1
- 230000004907 flux Effects 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 238000010348 incorporation Methods 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910052757 nitrogen Inorganic materials 0.000 description 1
- 229910052698 phosphorus Inorganic materials 0.000 description 1
- 239000011574 phosphorus Substances 0.000 description 1
- 239000002893 slag Substances 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000003886 thermite process Methods 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
- the present invention relates to an alloy which has certain properties both chemical and ph sical which render the alloy exneeding y important from a commercial standpoint, for the manufacture of all artielse or parts of structures wherein the article or structure is subjected to repeated heatings to high temperatures, or where the article or structure is subjected to the action of corrosive liquids, solids or fumes, or to oxidizing gases.
- the alloy is exceedingly resistant to wear and also is resistant to warping, cracking and breaking. Furthermore, the alloy is resistant to corrosion by contact with corroding substances or fumes and is not subject to surface flakin which causes rapid deterioration of an article which exhibits this failing.
- a still further desirable property is the fact that the melting point of the alloy is very high, so that an article or part of a structure may be subjected to considerable heat without in any way endangering the structure of the article due to melting or fusing.
- e alloy is also a goo material for the manufacture of electrical resistance elements,- the alloy being non-oxidizing at high temperatures.
- boxes made of the proposed alloy are non-warping and nonscahng even though subjected to repeated heating at high temperature and subsequent cooling, and are free from the fault of cracking. Furthermore, the walls of these boxes may be made comparatively thin, thereby lightenin the weight of these boxes to a considerable egree over that necessary where the boxes are made of iron or steel.
- the alloy does not materially oxidize when heated or subjected to fumes or gases.
- the aluminum and silicon at the sur aces of the alloy forms an oxidizing coating or skin which protects the metal from further oxidizing effects.
- the alloy comprises as its essential elements, chromium, iron, nickel, and a small proportion of titanium.
- manganese, as well as silicon and aluminum maybe present if desired, and also a small proportion of carbon.
- the alloy may contain 15 to 40 er cent of chromium, 1 to 15 per cent 0 nickel, 3/ 100 of 1 per cent to 10 per cent of titanium, 3/10 of l per cent to 2 per cent of silicon, of 1 per cent to 2 per cent of manganese, and 4/100 of 1 per cent to 2 per cent of aluminum if the presence of aluminum is desired, the balance consisting mainly of iron and carbon. If sulphur and phosphorus be present in the alloy, the amount should be kept as low as possible, preferably less than 5/100 of 1 per cent.
- the chromium is the element which imparts the highly resistant ualities as to wear and corrosion to the a 0y as well as the roperty of non-wa ing.
- the manganese gives a good grain to the alloy.
- the silicon and aluminum, (if aluminum is used,) are added just before the metal is poured.
- the silicon acts as a de-oxidizer of the metal bath and also im arts fluidity to the metal so that it is readi y poured.
- the source of ferrochrome used is that of the thermite process
- there is likely to be some aluminum in the fiarro-chrome which appears in the final a lo T e titanium performs two functions. While the alloy is in melted condition within the furnace, it acts as a de-oxidizer, part of the titanium combining with occluded ases, particularly nitrogen, and thls comination with titanium is removed by the slag. Additionally, excess of that required as a de-oxidizer, appears in the final alloy and imparts t e properties of toughness, resiliency and resistance to cracking.
- the quantity of titanium will vary in accordance with the degree in which it is desired to produce the characteristics just mentioned, and may vary within the limits which have before been specified.
- the alloy is produced in the electric fur uses by melting ferr0-chrome together with the various other ingredients of the alloy whichhave been mentioned, and with a suitable flux such as is well known in the art. In making the alloy it is only necessary to bring the temperature of the furnace to a suflicient degree to insure a thorough melting and incorporation of the various elements of the .alloy.
- the final alloy obtained is a metal which is very easily handled in.the foundry and can be poured and cast in manner and by methods similar to those em 10 ed in foundry practice.
- the alloy is tough and resistant to breaka
- the melting point is high, being in 5i; neighborhood of 2700 Fahrenheit.
- the alloy contains a low percentage of carbon, sa .11 per cent to .12 per cent, the alloy is f airly malleable and where the carbon is kept as low as 7/100 per cent to. 8/100 per cent, the alloy 15 also easily machinable. Under many circumstances this qualit of malle ability is important and desirab e.
- titanium which is in 3.
- a malleable alloy resistant to corrosion and to oxidation containing as essential ingredients, substantially 15 to 40 per cent of chromium, substantially 1 to 15 per cent of nickel, substantially 3/100 of 1 per cent to 15 per cent of titanium, balance of iron and carbon.
- a malleable alloy resistant to corrosion and to oxidation consisting of substantially 15% to 40% of chromium, 1% to 15% of nickel, to 2% of manganese, substantially 3/100% to 2 of a metal having the properties of silicon with respect to forming a non-flaking oxide, 2. small quantity of titanium in excess of 3/100%, the balance being iron and carbon.
- a malleable alloy resistant to corrosion and to oxidation consisting of substantially 18 per cent of chromium, 4 per cent of nickel, 1 per cent of manganese, 8/10% of titanium, balance iron and carbon.
- Alloyed malleable soft steel resistant to corrosion and to oxidation containin substantially chromium 15% to 40%, nicke 15%, silicon'2.5%, manganese 2%, and titanium about .08%.
- Alloyed malleable soft steel resistant to common and to oxidation containin substantially chromium 15% to 40%, nicke 15%, materlal having the properties of silicon and aluminum 53% to 4.5%, and titanium about .08%.
- Alloyed malleable soft steel resistant to corrosion and to oxidation containing substantially chromium 15% to 40%, nickel 1% to 15%, silicon 2.5%, manganese 2%, and titanium about .08%.
- Alloyed malleable soft steel resistant to corrosion and to oxidation containing substantially chromium 15% to 40%, nicke 1% to 15%, material having the properties of silicon and aluminum .53% to 4.5%, and titanium about .08%.
- Alloyed malleable soft steel resistant to corrosion and to oxidation containi substantially chromium 15% to 40%, nicke 15%, material having the properties of silicon and aluminum .53% to 4.5%, and tit nium .0370 to 10%.
- Alloyed malleable soft steelnresistant to corrosion and to oxidation containing substantially chromium 15% to 40%, nickel 1% to 15%, silicon 2.5%, manganese 2%,
- Alloyed malleabl soft steel resistant to corrosion and to oxidation containing substantially chromium 15% to 40%, nickel 1% to 15%, material having the properties of silicon and aluminum .53% to 4.5%, and 10 titanium .03% to 10%.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Heat Treatment Of Articles (AREA)
Description
Patented May 19, 1925.
UNITED STATES PATENT OFFICE.
WILLIAM H. SIITH, OF CLEVELAND, OHIO, ASSIGNOB TO LUnuUM STEEL 00., O1 WA'IHVLIET, NEW YORK, A CORPORATION OF NEW JERSEY.
IALLEAIBLE NONGORRODIBLE ALLOY.
No Drawing.
To all whom it may concern:
Be it known that I, WILLIAM H. SMITH, a citizen of the United States, residing at Cleveland in the county of Cuyahoga and State of Ohio, have invented a certain new and useful Improvement in Malleable Noncorrodible Alloys, of which the following is a full, clear, and exact description.
The present invention relates to an alloy which has certain properties both chemical and ph sical which render the alloy exneeding y important from a commercial standpoint, for the manufacture of all artielse or parts of structures wherein the article or structure is subjected to repeated heatings to high temperatures, or where the article or structure is subjected to the action of corrosive liquids, solids or fumes, or to oxidizing gases.
Among thev important properties of the alloy may be mentioned the fact that the alloy is exceedingly resistant to wear and also is resistant to warping, cracking and breaking. Furthermore, the alloy is resistant to corrosion by contact with corroding substances or fumes and is not subject to surface flakin which causes rapid deterioration of an article which exhibits this failing.
A still further desirable property is the fact that the melting point of the alloy is very high, so that an article or part of a structure may be subjected to considerable heat without in any way endangering the structure of the article due to melting or fusing.
The fact that articles and parts of structures made from this alloy do not warp and do not grow, or in other words, increase their dimensions b repeated beatings, makes the alloy excee 'ngly useful in a great many instances.
Among the important uses to which the allo may be put we may mention containers or eat treating boxes, saggars, furnace arts, crucibles, glass molds, metal molds or foundry use, retorts, dies, die rings, and in fact, any structure in the use of which the important roperties of this allo may be utilized. e alloy is also a goo material for the manufacture of electrical resistance elements,- the alloy being non-oxidizing at high temperatures.
One very important use to which the al- Lpplication filed February 27, 1919. Serial No. 278,848.
10y may be put is the making of heat treating boxes, or containers. Boxes made of the proposed alloy are non-warping and nonscahng even though subjected to repeated heating at high temperature and subsequent cooling, and are free from the fault of cracking. Furthermore, the walls of these boxes may be made comparatively thin, thereby lightenin the weight of these boxes to a considerable egree over that necessary where the boxes are made of iron or steel.
The alloy does not materially oxidize when heated or subjected to fumes or gases. The aluminum and silicon at the sur aces of the alloy forms an oxidizing coating or skin which protects the metal from further oxidizing effects.
The alloy comprises as its essential elements, chromium, iron, nickel, and a small proportion of titanium. In addition it is found advantageous to use manganese, as well as silicon and aluminum maybe present if desired, and also a small proportion of carbon.
The alloy may contain 15 to 40 er cent of chromium, 1 to 15 per cent 0 nickel, 3/ 100 of 1 per cent to 10 per cent of titanium, 3/10 of l per cent to 2 per cent of silicon, of 1 per cent to 2 per cent of manganese, and 4/100 of 1 per cent to 2 per cent of aluminum if the presence of aluminum is desired, the balance consisting mainly of iron and carbon. If sulphur and phosphorus be present in the alloy, the amount should be kept as low as possible, preferably less than 5/100 of 1 per cent.
As an example, atypical analysls of an alloy found to contain the desirable qualities, the following is given:
18 per cent chromium, 4 er cent nickel, 1% per cent manganese, 8/1 0 per cent titanium, 1 er cent silicon, 3/100 per cent aluminum i aluminum is present at all, balance iron and carbon.
The chromium is the element which imparts the highly resistant ualities as to wear and corrosion to the a 0y as well as the roperty of non-wa ing. The nickel ren ers the alloy more omogeneous and less likely to cracking when sulnected to repeated hcatings. The manganese gives a good grain to the alloy.
The silicon and aluminum, (if aluminum is used,) are added just before the metal is poured. The silicon acts as a de-oxidizer of the metal bath and also im arts fluidity to the metal so that it is readi y poured.
In the event that the source of ferrochrome used is that of the thermite process, there is likely to be some aluminum in the fiarro-chrome which appears in the final a lo T e titanium performs two functions. While the alloy is in melted condition within the furnace, it acts as a de-oxidizer, part of the titanium combining with occluded ases, particularly nitrogen, and thls comination with titanium is removed by the slag. Additionally, excess of that required as a de-oxidizer, appears in the final alloy and imparts t e properties of toughness, resiliency and resistance to cracking. The quantity of titanium will vary in accordance with the degree in which it is desired to produce the characteristics just mentioned, and may vary within the limits which have before been specified.
The alloy is produced in the electric fur uses by melting ferr0-chrome together with the various other ingredients of the alloy whichhave been mentioned, and with a suitable flux such as is well known in the art. In making the alloy it is only necessary to bring the temperature of the furnace to a suflicient degree to insure a thorough melting and incorporation of the various elements of the .alloy. The final alloy obtained is a metal which is very easily handled in.the foundry and can be poured and cast in manner and by methods similar to those em 10 ed in foundry practice.
The a oy as a high tensile strength, and on fracture shows a fine compact grain. The alloy is tough and resistant to breaka The melting point is high, being in 5i; neighborhood of 2700 Fahrenheit.
It has been found that when the alloy contains a low percentage of carbon, sa .11 per cent to .12 per cent, the alloy is f airly malleable and where the carbon is kept as low as 7/100 per cent to. 8/100 per cent, the alloy 15 also easily machinable. Under many circumstances this qualit of malle ability is important and desirab e.
iHaving described my invention, I claim:
1'. A malleable alloyed soft steel resistant to corrosion and to oxidation containing iron in excess of chromium not less than 15% and not greater than 40%, to-
ther with nickel and titanium not greater t anthe chromium. A
2. A 'malleable alloyed soft steel resistant to corrosion and to oxidation containing iron in excess of 50%, nickel not less than 1% and not greater than 15% together with chromium and titanium not greater than 50% nor less than 15%.
the titanium which is in 3. A malleable alloyed soft steel resistant to corrosion and to oxidation containing iron in excess of 50%, nickel about 515%, titanium not less than .08% nor greater than 10%, together with chromium.
4. A malleable alloyed soft steel resistant to corrosion and to oxidation containing iron in excess of 50%, chromium approximately 18%, nickel not less than 1% nor greater than 15% and a small quantity of titanium.
5. A malleable alloy resistant to corrosion and to oxidation containing as essential ingredients, substantially 15 to 40 per cent of chromium, substantially 1 to 15 per cent of nickel, substantially 3/100 of 1 per cent to 15 per cent of titanium, balance of iron and carbon.
6. A malleable alloy resistant to corrosion and to oxidation consisting of substantially 15% to 40% of chromium, 1% to 15% of nickel, to 2% of manganese, substantially 3/100% to 2 of a metal having the properties of silicon with respect to forming a non-flaking oxide, 2. small quantity of titanium in excess of 3/100%, the balance being iron and carbon.
7. A malleable alloy resistant to corrosion and to oxidation consisting of substantially 18 per cent of chromium, 4 per cent of nickel, 1 per cent of manganese, 8/10% of titanium, balance iron and carbon.
8. Alloyed malleable soft steel resistant to corrosion and to oxidation containin substantially chromium 15% to 40%, nicke 15%, silicon'2.5%, manganese 2%, and titanium about .08%.
9. Alloyed malleable soft steel resistant to common and to oxidation containin substantially chromium 15% to 40%, nicke 15%, materlal having the properties of silicon and aluminum 53% to 4.5%, and titanium about .08%.
10. Alloyed malleable soft steel resistant to corrosion and to oxidation containing substantially chromium 15% to 40%, nickel 1% to 15%, silicon 2.5%, manganese 2%, and titanium about .08%.
11. Alloyed malleable soft steel resistant to corrosion and to oxidation containing substantially chromium 15% to 40%, nicke 1% to 15%, material having the properties of silicon and aluminum .53% to 4.5%, and titanium about .08%.
12. Alloyed malleable soft steel resistant to corrosion and to oxidation containing substantially chromium 15% to 40%, nicke 15%, silicon 2.5%, manganese 2%, and titanium .03% to 10%. T
13. Alloyed malleable soft steel resistant to corrosion and to oxidation containi substantially chromium 15% to 40%, nicke 15%, material having the properties of silicon and aluminum .53% to 4.5%, and tit nium .0370 to 10%.
14. Alloyed malleable soft steelnresistant to corrosion and to oxidation containing substantially chromium 15% to 40%, nickel 1% to 15%, silicon 2.5%, manganese 2%,
5 and titanium 03% to 10%.
15. Alloyed malleabl soft steel resistant to corrosion and to oxidation containing substantially chromium 15% to 40%, nickel 1% to 15%, material having the properties of silicon and aluminum .53% to 4.5%, and 10 titanium .03% to 10%.
In testimony whereof, I
my signature.
hereunto afiix WILLIAM H. SMITH.
14. Alloyed malleable soft steel.resistant substantially chromium 15% to 40%, nickel to OOIIOSIOII and to oxidation containing 1% to 15%, material having the properties substantially chromium 15% to 40%, nickel of silicon and aluminum 53% to 4.5%, and 10 1% to 15%, silicon 2.5%, manganese 2%, titanium .03% to 10%. 5 and titanium .03% to 10%. In testimony whereof, I hereunto aflix 15. Alloyed malleable soft steel resistant my signature. to corrosion and to oxidation containing WILLIAM H. SMITH.
Certificate or Correction.
It is hereby certified that in Letters Patent/No. 1,538,360, granted May 19, 1925, upon the application of William H. Smith, of Cleveland, Ohio, for an improvement in Malleable Noncorrodible Alloys, errors appear in the punted specification requiring correction as follows: Page 1, line 66, before the word fumes insert the word omieiizing, and line 68 for oxidizing read coating; and that the said Letters Patent should be read with these corrections therein that the same may conform to the record of the case in the Patent Ofiice.
Signed and sealed this 30th day of June, A. D. 1925.
[emu] KARL FENNING,
Acting Ouwwnissiamr of Piltemts.
Certificate oI Gorrection.
It is hereby certified that in Letters Patent No. 1,538,360, granted May 19, 1925, upon the application of William H. Smith, of Cleveland, Ohio, for an improvement in Malleable Noncorrodible Alloys, errors appear in the painted specification requiring correction as follows: Page 1, line 66, before the word fumes insert the word oxidizing, and line 68 for oxidizing read coating; and that the said Letters Patent should he read with these corrections therein that the same may conform to the record of the case in the Patent Ofiice.
Signed and sealed this 30th day of June, A. D. 1925.
[emu] KARL FENNING,
Acting Commissioner of Patents.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US279649A US1538360A (en) | 1919-02-27 | 1919-02-27 | Malleable noncorrodible alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US279649A US1538360A (en) | 1919-02-27 | 1919-02-27 | Malleable noncorrodible alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1538360A true US1538360A (en) | 1925-05-19 |
Family
ID=23069872
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US279649A Expired - Lifetime US1538360A (en) | 1919-02-27 | 1919-02-27 | Malleable noncorrodible alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1538360A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3131055A (en) * | 1960-03-11 | 1964-04-28 | Soc Metallurgique Imphy | Alloy based on iron, containing nickel, chromium and aluminium, and process for obtaining same |
| US3366263A (en) * | 1964-07-15 | 1968-01-30 | Allegheny Ludlum Steel | Hot water tank |
| US4802894A (en) * | 1984-11-09 | 1989-02-07 | Hitachi, Ltd. | Method of using a structural member of anti-sulfur-attack cr-ni-al-si alloy steel for coal gasification system |
-
1919
- 1919-02-27 US US279649A patent/US1538360A/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3131055A (en) * | 1960-03-11 | 1964-04-28 | Soc Metallurgique Imphy | Alloy based on iron, containing nickel, chromium and aluminium, and process for obtaining same |
| US3366263A (en) * | 1964-07-15 | 1968-01-30 | Allegheny Ludlum Steel | Hot water tank |
| US4802894A (en) * | 1984-11-09 | 1989-02-07 | Hitachi, Ltd. | Method of using a structural member of anti-sulfur-attack cr-ni-al-si alloy steel for coal gasification system |
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