US1612642A - Method of adding aluminum to aluminum-containing alloys - Google Patents
Method of adding aluminum to aluminum-containing alloys Download PDFInfo
- Publication number
- US1612642A US1612642A US37433A US3743325A US1612642A US 1612642 A US1612642 A US 1612642A US 37433 A US37433 A US 37433A US 3743325 A US3743325 A US 3743325A US 1612642 A US1612642 A US 1612642A
- Authority
- US
- United States
- Prior art keywords
- aluminum
- alloy
- nickel
- copper
- added
- 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 28
- 239000000956 alloy Substances 0.000 title description 28
- 229910052782 aluminium Inorganic materials 0.000 title description 17
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title description 17
- 238000000034 method Methods 0.000 title description 2
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 22
- 229910000838 Al alloy Inorganic materials 0.000 description 11
- 229910052759 nickel Inorganic materials 0.000 description 11
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 9
- 229910052802 copper Inorganic materials 0.000 description 9
- 239000010949 copper Substances 0.000 description 9
- 238000004519 manufacturing process Methods 0.000 description 7
- 229910000570 Cupronickel Inorganic materials 0.000 description 6
- -1 aluminum-copper-nickel Chemical compound 0.000 description 4
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 3
- 229910000792 Monel Inorganic materials 0.000 description 3
- YOCUPQPZWBBYIX-UHFFFAOYSA-N copper nickel Chemical compound [Ni].[Cu] YOCUPQPZWBBYIX-UHFFFAOYSA-N 0.000 description 3
- 229910052749 magnesium Inorganic materials 0.000 description 3
- 239000011777 magnesium Substances 0.000 description 3
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N Silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 2
- 239000011449 brick Substances 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000005242 forging Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910052751 metal Inorganic materials 0.000 description 2
- 239000002184 metal Substances 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- 229910052710 silicon Inorganic materials 0.000 description 2
- 239000010703 silicon Substances 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 1
- 229910000990 Ni alloy Inorganic materials 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- JRBRVDCKNXZZGH-UHFFFAOYSA-N alumane;copper Chemical compound [AlH3].[Cu] JRBRVDCKNXZZGH-UHFFFAOYSA-N 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 229910052791 calcium Inorganic materials 0.000 description 1
- 239000011575 calcium Substances 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 238000009826 distribution Methods 0.000 description 1
- 238000005098 hot rolling Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000010405 reoxidation reaction Methods 0.000 description 1
- 239000000377 silicon dioxide Substances 0.000 description 1
- WFKWXMTUELFFGS-UHFFFAOYSA-N tungsten Chemical compound [W] WFKWXMTUELFFGS-UHFFFAOYSA-N 0.000 description 1
- 229910052721 tungsten Inorganic materials 0.000 description 1
- 239000010937 tungsten Substances 0.000 description 1
- 229910052725 zinc Inorganic materials 0.000 description 1
- 239000011701 zinc Substances 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C1/00—Making non-ferrous alloys
- C22C1/02—Making non-ferrous alloys by melting
- C22C1/03—Making non-ferrous alloys by melting using master alloys
Definitions
- the objectof my invention is to overcome this difliculty and also make the process easier for the operator in preparing and pouring the alloy.
- the aluminum to be added to the copper-nickel alloy is made into an alloy prior to its introduction into the copper-aluminum alloy the product is improved particularly in its hot forging and rolling properties.
- the preliminary aluminum alloy made should'not contain materially more than 85% of aluminum in order to give the best results, and should preferably contain from 60% to 70% of aluminum.
- an aluminum-copper-nickel alloy containing aluminum up to 17% (about 2 to 7% preferred) copper from about 1 to 90% (preferably over 10%) and the remainder mainly nickel (the nickel being preferably over 40%) I have added to a bath of Monel metal an aluminum alloy containing 60 to 70%. of aluminum, to 20% of nickel and 15 to 10% of copper.
- the composition of the preformed aluminum alloy mayvar-y widely but the aluminum should run from to not materially over 85%, and for the material desired in my tests the nickel should run from to 10% and the copper from 20 to 5%.
- the aluminum in the added alloy under my invention itself acts as a deox1-.
- the alloy may be added in the furnace or in the ladle, but is preferably added in the furnace as this insures better distribution. I have also found that by adding this alloy of aluminum inconnection with the use of a furnace lining of zirkite brick instead of silica brick the silicon in the final alloy is reduced so that any rolling difliculties which have occurred from the efiect of silicon in the final alloy have been reduced to a considerable extent.
- the preliminary alloy contains 85% of aluminum there will be some temperature increase in the bath when it is added, although not suflicient to ruin the heat.
- my invention also enables the operator to make the addition more rapidly and also avoids the need of holding the metal before teeming in order to avoid pouring at too high a temperature.
- a small amount of magnesium may be added with advantage to the preliminary aluminum alloy as above recited, and the alloy may also contain calcium, zinc, tungsten or other deoxidizing elements.
- the other a1- loying ingredients of the preliminary aluminum alloy may, of course, v9.3 in'accordance with the final alloy desir I claim: v 1.
- the step consisting in adding' to a molten bath consisting mainly of nickel and copper an aluminum alloy containing aluminum and at least one other con stituent of the metal bath.
- the step consisting in adding to a bath consistin mainly of molten nickel and copper an a uminum alloy containing aluminum and at least one other constituent of the bath and a deoxidizer.
- the step consisting of adding to a molten bath consisting mainly ofcopper and nickel an alloy containing from 35 to 85% of aluminum.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture And Refinement Of Metals (AREA)
Description
Patented Dec. 2 8, 1926 UNITED STATES 1,61z,64z PATENT OFFICE.
WILLIAM A. MUDGE, or nnnrmeron, wns'r vrnemm, ASSIGNOB 'ro THE mumm- TIONAL NICKEL warranty, or NEW YORK, 11. 2., A CORPORATION or new JERSEY.
METHOD OF ADDING ALUMINUM TO.ALUKINUM-CONTAINING ALLOY S.
No Drawing.
In the manufacture of aluminum-coppernickel alloys it has been common practice to add aluminum to a molten copper-nickel alloy such, for example, as Monel metal. In such practice there'have been certain difiiculties, particularly as regards the malleability of the alloy While hot.
The objectof my invention is to overcome this difliculty and also make the process easier for the operator in preparing and pouring the alloy.
I have discovered that if the aluminum to be added to the copper-nickel alloy is made into an alloy prior to its introduction into the copper-aluminum alloy the product is improved particularly in its hot forging and rolling properties. I have also found that the preliminary aluminum alloy made should'not contain materially more than 85% of aluminum in order to give the best results, and should preferably contain from 60% to 70% of aluminum.
I believe that this improvement is due to the fact that when a substantially pure aluminum is added to a bath of copper-nickel alloy there is a rise in temperature probably due to the formation and possibly decomposition of certain compounds; and with the use of an aluminum alloy such as I have employed this rise in temperature is greatlyreducedand may be practically done away with. However, I do not wish to be limited to this theory of action.
As an example of carrying out my invention, in making an aluminum-copper-nickel alloy containing aluminum up to 17% (about 2 to 7% preferred) copper from about 1 to 90% (preferably over 10%) and the remainder mainly nickel (the nickel being preferably over 40%), I have added to a bath of Monel metal an aluminum alloy containing 60 to 70%. of aluminum, to 20% of nickel and 15 to 10% of copper. The composition of the preformed aluminum alloy mayvar-y widely but the aluminum should run from to not materially over 85%, and for the material desired in my tests the nickel should run from to 10% and the copper from 20 to 5%. I
I have also found that it magnesium is added to the preliminary aluminum alloy in amounts as low as 20% n) further addition of magnesium in the furnace or in the ladle is necessary in order to give complete dcoxidation and good malleability. In my Application filed June 16, 1925. Serial No. 37,433,
opinion, the aluminum in the added alloy under my invention itself acts as a deox1-.
dizer; and as there is no material tempera: ture rise in the bath when added there is probably no reoxidation resulting.
A large number of, test runs made by add ing an aluminum alloy of varying proportions to Monel metal has given excellent results in reducing difliculties in hot rolling ailild forging of the aluminum-coppermickel a oy.
The alloy may be added in the furnace or in the ladle, but is preferably added in the furnace as this insures better distribution. I have also found that by adding this alloy of aluminum inconnection with the use of a furnace lining of zirkite brick instead of silica brick the silicon in the final alloy is reduced so that any rolling difliculties which have occurred from the efiect of silicon in the final alloy have been reduced to a considerable extent. p
If the preliminary alloy contains 85% of aluminum there will be some temperature increase in the bath when it is added, although not suflicient to ruin the heat.
The use of my invention also enables the operator to make the addition more rapidly and also avoids the need of holding the metal before teeming in order to avoid pouring at too high a temperature. I
The advantages of my invention will be obvious to those skilled in the art since hot working difficulties of the final alloy are greatly reduced or eliminated, less additional deoxidizer is required, and certain operating advantages are also given.
A small amount of magnesium may be added with advantage to the preliminary aluminum alloy as above recited, and the alloy may also contain calcium, zinc, tungsten or other deoxidizing elements. The other a1- loying ingredients of the preliminary aluminum alloy may, of course, v9.3 in'accordance with the final alloy desir I claim: v 1. In the manufacture of aluminum-copper-nickel alloys, the step consisting of adding an aluminumalloy to a molten bath consisting mainly of copper and nickel.
3. In the manufacture of aluminum-copper-nickel alloys, the step consisting in adding' to a molten bath consisting mainly of nickel and copper an aluminum alloy containing aluminum and at least one other con stituent of the metal bath.
4. In the manufacture of aluminum-copper-nickel alloys, the step consisting in adding to a bath consistin mainly of molten nickel and copper an a uminum alloy containing aluminum and at least one other constituent of the bath and a deoxidizer.
5. In the manufacture of alumi num-copper-nickel alloys, the step consisting of adding to a molten bath consisting mainly ofcopper and nickel an alloy containing from 35 to 85% of aluminum.
6. In the manufacture of aluminum-coper-nickel alloys, the step consisting of add.- mg to a molten bath consisting mainly of copper and nickel an alloy containing from 35 to 85% of aluminum, the remainder of said added alloy consisting mainly of cop- 8. In the manufacture of alm'ninum-copper-nickel alloys, the step consisting in adding to a molten bath consisting mainly of copper and nickel an alloy containing alu- 1 m'inum, nickel and copper.
I In testimony whereof I have hereunto set my hand.
WILLIAM A. MUDGE.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US37433A US1612642A (en) | 1925-06-16 | 1925-06-16 | Method of adding aluminum to aluminum-containing alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US37433A US1612642A (en) | 1925-06-16 | 1925-06-16 | Method of adding aluminum to aluminum-containing alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1612642A true US1612642A (en) | 1926-12-28 |
Family
ID=21894308
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US37433A Expired - Lifetime US1612642A (en) | 1925-06-16 | 1925-06-16 | Method of adding aluminum to aluminum-containing alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1612642A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3329498A (en) * | 1962-11-09 | 1967-07-04 | Siderurgie Fse Inst Rech | Refractory alloy |
| DE3500555C1 (en) * | 1985-01-10 | 1986-01-02 | Degussa Ag, 6000 Frankfurt | Use of nickel alloys for jewelry and watch parts |
| DE3500554C1 (en) * | 1985-01-10 | 1986-01-09 | Degussa Ag, 6000 Frankfurt | Use of nickel alloys for glasses frames |
| US4715910A (en) * | 1986-07-07 | 1987-12-29 | Olin Corporation | Low cost connector alloy |
-
1925
- 1925-06-16 US US37433A patent/US1612642A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3329498A (en) * | 1962-11-09 | 1967-07-04 | Siderurgie Fse Inst Rech | Refractory alloy |
| DE3500555C1 (en) * | 1985-01-10 | 1986-01-02 | Degussa Ag, 6000 Frankfurt | Use of nickel alloys for jewelry and watch parts |
| DE3500554C1 (en) * | 1985-01-10 | 1986-01-09 | Degussa Ag, 6000 Frankfurt | Use of nickel alloys for glasses frames |
| US4715910A (en) * | 1986-07-07 | 1987-12-29 | Olin Corporation | Low cost connector alloy |
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