US1916496A - Method of making lead alloys - Google Patents
Method of making lead alloys Download PDFInfo
- Publication number
- US1916496A US1916496A US491081A US49108130A US1916496A US 1916496 A US1916496 A US 1916496A US 491081 A US491081 A US 491081A US 49108130 A US49108130 A US 49108130A US 1916496 A US1916496 A US 1916496A
- Authority
- US
- United States
- Prior art keywords
- lead
- calcium
- alloy
- aluminum
- magnesium
- 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
- 229910000978 Pb alloy Inorganic materials 0.000 title description 7
- 238000004519 manufacturing process Methods 0.000 title description 4
- OYPRJOBELJOOCE-UHFFFAOYSA-N Calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 28
- 229910052791 calcium Inorganic materials 0.000 description 28
- 239000011575 calcium Substances 0.000 description 28
- UXVMQQNJUSDDNG-UHFFFAOYSA-L Calcium chloride Chemical compound [Cl-].[Cl-].[Ca+2] UXVMQQNJUSDDNG-UHFFFAOYSA-L 0.000 description 18
- 229910001628 calcium chloride Inorganic materials 0.000 description 18
- 239000001110 calcium chloride Substances 0.000 description 18
- FYYHWMGAXLPEAU-UHFFFAOYSA-N Magnesium Chemical compound [Mg] FYYHWMGAXLPEAU-UHFFFAOYSA-N 0.000 description 17
- 229910052782 aluminium Inorganic materials 0.000 description 17
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 17
- 229910052749 magnesium Inorganic materials 0.000 description 17
- 239000011777 magnesium Substances 0.000 description 17
- 229910052751 metal Inorganic materials 0.000 description 15
- 239000002184 metal Substances 0.000 description 15
- 229910045601 alloy Inorganic materials 0.000 description 13
- 239000000956 alloy Substances 0.000 description 13
- QSHDDOUJBYECFT-UHFFFAOYSA-N mercury Chemical compound [Hg] QSHDDOUJBYECFT-UHFFFAOYSA-N 0.000 description 12
- 229910052753 mercury Inorganic materials 0.000 description 12
- 238000000034 method Methods 0.000 description 12
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 11
- 150000002739 metals Chemical class 0.000 description 11
- 229910052718 tin Inorganic materials 0.000 description 11
- WHXSMMKQMYFTQS-UHFFFAOYSA-N Lithium Chemical compound [Li] WHXSMMKQMYFTQS-UHFFFAOYSA-N 0.000 description 8
- ZLMJMSJWJFRBEC-UHFFFAOYSA-N Potassium Chemical compound [K] ZLMJMSJWJFRBEC-UHFFFAOYSA-N 0.000 description 8
- 229910052744 lithium Inorganic materials 0.000 description 8
- 229910052700 potassium Inorganic materials 0.000 description 8
- 239000011591 potassium Substances 0.000 description 8
- 238000013329 compounding Methods 0.000 description 7
- 230000004907 flux Effects 0.000 description 7
- 238000002844 melting Methods 0.000 description 7
- 230000008018 melting Effects 0.000 description 7
- 239000000155 melt Substances 0.000 description 5
- 230000003647 oxidation Effects 0.000 description 5
- 238000007254 oxidation reaction Methods 0.000 description 5
- 229910001128 Sn alloy Inorganic materials 0.000 description 4
- 239000004615 ingredient Substances 0.000 description 4
- RSWGJHLUYNHPMX-UHFFFAOYSA-N Abietic-Saeure Natural products C12CCC(C(C)C)=CC2=CCC2C1(C)CCCC2(C)C(O)=O RSWGJHLUYNHPMX-UHFFFAOYSA-N 0.000 description 3
- KHPCPRHQVVSZAH-HUOMCSJISA-N Rosin Natural products O(C/C=C/c1ccccc1)[C@H]1[C@H](O)[C@@H](O)[C@@H](O)[C@@H](CO)O1 KHPCPRHQVVSZAH-HUOMCSJISA-N 0.000 description 3
- DAEJUPKPHRBQHZ-UHFFFAOYSA-N [Sn].[Hg] Chemical compound [Sn].[Hg] DAEJUPKPHRBQHZ-UHFFFAOYSA-N 0.000 description 3
- KHPCPRHQVVSZAH-UHFFFAOYSA-N trans-cinnamyl beta-D-glucopyranoside Natural products OC1C(O)C(O)C(CO)OC1OCC=CC1=CC=CC=C1 KHPCPRHQVVSZAH-UHFFFAOYSA-N 0.000 description 3
- YVIMHTIMVIIXBQ-UHFFFAOYSA-N [SnH3][Al] Chemical compound [SnH3][Al] YVIMHTIMVIIXBQ-UHFFFAOYSA-N 0.000 description 2
- -1 calclum Chemical class 0.000 description 2
- 230000007797 corrosion Effects 0.000 description 2
- 238000005260 corrosion Methods 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 239000002142 lead-calcium alloy Substances 0.000 description 2
- 229910000897 Babbitt (metal) Inorganic materials 0.000 description 1
- UNMYWSMUMWPJLR-UHFFFAOYSA-L Calcium iodide Chemical compound [Ca+2].[I-].[I-] UNMYWSMUMWPJLR-UHFFFAOYSA-L 0.000 description 1
- 241000896693 Disa Species 0.000 description 1
- 229910001622 calcium bromide Inorganic materials 0.000 description 1
- WGEFECGEFUFIQW-UHFFFAOYSA-L calcium dibromide Chemical compound [Ca+2].[Br-].[Br-] WGEFECGEFUFIQW-UHFFFAOYSA-L 0.000 description 1
- 229940046413 calcium iodide Drugs 0.000 description 1
- 229910001640 calcium iodide Inorganic materials 0.000 description 1
- 238000005266 casting Methods 0.000 description 1
- 150000001875 compounds Chemical class 0.000 description 1
- 230000007547 defect Effects 0.000 description 1
- 238000005187 foaming Methods 0.000 description 1
- 239000003517 fume Substances 0.000 description 1
- 229910052736 halogen Inorganic materials 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 150000002611 lead compounds Chemical class 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 150000002736 metal compounds Chemical class 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 239000004848 polyfunctional curative Substances 0.000 description 1
- 239000000047 product Substances 0.000 description 1
- 230000013707 sensory perception of sound Effects 0.000 description 1
- 239000006228 supernatant Substances 0.000 description 1
- 239000011135 tin 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
- C22C11/00—Alloys based on lead
- C22C11/02—Alloys based on lead with an alkali or an alkaline earth metal as the next major constituent
Definitions
- This invention relates to the production of lead alloys and its object is to provide certain novel procedures in the compounding of such alloys, having in view convenience of .operation, low cost of manufacture, uniformity and homogeneity of the product and particularly the provision of a method whereby small quantities of metals, such as calclum, aluminum, magnesium and the like, whlch are susceptible of oxidation may be introduced into and dissolved in a molten batch of'calcium, tin, mercury, magnesium and aluminum.
- the mercury is optional, where maximum hardness is not required; and for some purposes, potassium and/or lithium may be used for (part or all of the magneslum with the disa vantage, however, of making the alloy somewhat unstable and subject.
- composition of this particular type of alloy according to the preferred formula is as follows:
- the quantities of the readily oxidizable ingredients, calcium, magnesiumand aluminum may be somewhat greater than indicated, depending upon the care taken to prevent or limit oxidation in compounding and remelting.
- the mercury is optional, but preferred. It is essential if a high degree of "hardness is required, and it acts cumulatively with the calcium, tin and magnesium, in increasing the hardness of the lead. Calcium, mercury, tin and magnesium all act as hardeners of the lead and can be used in an aggregate amount considerablv greater than the amount of any single one of them which it is practical to use.
- the allo also comprises .aluminum, the function 0 which is to prevent the calcium and magnesium from drossing out while the alloy is being compounded and also in relting, for example, in melting up the inots for casting.
- the amount used may vary between the limits as above indicated Application filed October 24, 1930. Serial No. 491,081.
- Alloys containing magnesium and/or lithium and/ or potassium may be represented by the following table:
- the addition of the lithium and potassium increases the hardness of the alloy where hardness is a desideratum, but at the cost of increased corrosibility.
- the hardness of the alloy may vary from 18 to 26 Brinell. It may be raised to 28 Brinell by increase of the calcium, but in this .case the danger of corrosion and drossing is somewhat increased.
- the alloy as above described, or other hardened or toughened lead compound containing easily oxidizable metals, may be made by one of the two following methods:
- the lead is melted and covered with calcium chloride and the temperature raised to approximately 1600 Fahronheit, to insure the melting of the calcium chloride, which may form a layer of an inch in thickness on the lead.
- the metals to be compounded with the lead and which are of a readily oxidizable character are introduced into the molten lead through the calcium chloride flux or covering stratum.
- the tinand aluminum may be so introduced either as separate metals or, (which is preferable as a matter of convenience), the aluminum and the tin, in whole or part, may be introduced as tin-aluminum .alloy.
- the batch is stirred until the aluminum is completely dissolved in the lead, or so much dissolved as can be held in solution in the lead.
- the magnesium is next introduced into the batch in the same manner and thereafter the calcium, as metallic calcium.
- the calcium is introduced into the lead' after the other ingredients above named, in order to prevent foaming of the calcium chloride covering, which is like- 1y to occur if the calcium is put in first or if all of the before mentioned ingredients are introduced into the lead at the same time.
- the lead is now allowed to cool down to a temperature of about 600 to 700 F. the calcium chloride covering stripped off, at
- themercury added preferably as a mercury tin alloy.
- the crucible may be removed from the furnace and allowed to cool to dull red heat, approximately 1200 to 1300 F. and the mercury tin alloy introduced through the flux. This causes a slight loss of mercury but tends to give a better pouring metal.
- lithium and/or potassium are used, they are introduced into the melt with the mercury, that is while the batch is at a relatively low temperature, and rosin is added, which by burning creates fumes which keep the air from coming in contact with the metal.
- the supernatant calcium chloride stratum on the lead batch serves to keep the air from contact with the molten metal and thereby prevents or materially lessens oxidation of the lead and other metals. Any metal susceptible to oxidation is likely to be covered with a film of oxide. In passing the pieces of tinaluminum alloy, magnesium and calcium through the calcium chloride stratum, the oxide films on these metals are dissolved by the calcium chloride- The lead will also be, ordinarily, superficially oxidized and in the melting of the lead the oxide will rise to the top of the batch and be dissolved andretained by the calcium chloride stratum.
- Secmid method The lead is melted and covered with a calcium chloride covering, as described in connection with the first method.
- the tin and aluminum, preferably as aluminum-tin alloy and metallic magnesium are introduced into the lead through the flux, as in the first method.
- the calcium is next introduced, not as metallic calcium, but as calcium-lead alloy.
- the amount of calcium in this case may be slightly less than when metallic calcium is used.
- the crucible is taken from the furnace and the melt allowed to cool to 600 to 700 F., the flux being stripped off.
- the mercury is then added as mercury-tin alloy; or one may introduce this ingredient to the flux as in the first method.
- Method of compounding a lead alloy which consists in melting the lead under a. molten covering; introducing the tin, aluminum and magnesium into the lead through said covering and thereafter the calcium; and introducing the mercury, lithium, or potassium into the metallic body while it is at a temperature not substantially in excess of 700 degrees Fahrenheit.
- Method of compounding a lead alloy which comprises: melting the lead and holding the same at a temperature of approxi mately ,1600 degrees Fahrenheit under 2. molten covering of calcium chloride; introduc ing the tin, aluminum and magnesium into the lead under said covering and thereafter the calcium; allowing the melt to come down to a temperature of approximately 600 degrees to 700 degrees Fahrenheit and introducing the mercury, lithium and potassium body at approximately this temperature.
- Method of compounding a lead allo which comprises: melting the lead and hol ing the same at a temperature of approximately 1600 de rees Fahrenheit under a moltencovering 0 calcium chloride; introducing the tin, aluminum, and magnesium into the lead under said covering and thereafter the calcium; introducing rosin into the lead when the latter is at a temperature of about 600 to 700 degrees Fahrenheit, and while the rosin is burning introducing lithium or potassium into the molten body.
- Method of compounding a hardened lead alloy which comprises melting the lead under a covering of calcium chloride, introducing tin, aluminum, magnesium and calcium into the lead through the calcium chloride covering, reducin the temperature of the melt and introduclng mercury into the
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 July 4, 1933 UNITED STATES PATENT OFFICE ROBERT 3". SEOEMAKER, OF CHICAGO, ILLINOIS, ASSIGNOR TO B. & T. METALOOMPANY,
OF CHICAGO, ILLINOIS, A CORPORATION OF ILLINOIS METHOD OI MAKING LEAD ALLOYS Io Drawing.
This invention relates to the production of lead alloys and its object is to provide certain novel procedures in the compounding of such alloys, having in view convenience of .operation, low cost of manufacture, uniformity and homogeneity of the product and particularly the provision of a method whereby small quantities of metals, such as calclum, aluminum, magnesium and the like, whlch are susceptible of oxidation may be introduced into and dissolved in a molten batch of'calcium, tin, mercury, magnesium and aluminum. The mercury is optional, where maximum hardness is not required; and for some purposes, potassium and/or lithium may be used for (part or all of the magneslum with the disa vantage, however, of making the alloy somewhat unstable and subject.
to drossing or corrosion.
The composition of this particular type of alloy, according to the preferred formula is as follows:
Calcium 0.3% to 1.0%Preferred amount 0 5% Tin 0.5% to 2.0%P1eferred amount 1.0% Mercury 0.1g; to 0.5%Preferred amount 0.25% Magnesium 0.0 to 0.1 %Preferred amount 0.07 Aluminum 0.02% to 0.1%Preferred amount 0.05%
Lead to make up 100%.
In the batch, the quantities of the readily oxidizable ingredients, calcium, magnesiumand aluminum, may be somewhat greater than indicated, depending upon the care taken to prevent or limit oxidation in compounding and remelting.
The mercury is optional, but preferred. It is essential if a high degree of "hardness is required, and it acts cumulatively with the calcium, tin and magnesium, in increasing the hardness of the lead. Calcium, mercury, tin and magnesium all act as hardeners of the lead and can be used in an aggregate amount considerablv greater than the amount of any single one of them which it is practical to use.
The allo also comprises .aluminum, the function 0 which is to prevent the calcium and magnesium from drossing out while the alloy is being compounded and also in relting, for example, in melting up the inots for casting. The amount used may vary between the limits as above indicated Application filed October 24, 1930. Serial No. 491,081.
but apparently only about 0.03% remains in the alloy. The rest is carried off by the flux or covering which is employed in compounding the metals as will be described. It is preferable to use, however, more aluminum than actually goes into the compound in order to be certain that a sufficient amount is actually dissolved in the lead.
Alloys containing magnesium and/or lithium and/ or potassium may be represented by the following table:
Calcium 0.3% to 1.0% Preferable amount 0.5% Tin 0.5% to 2.0% Preferable amount 1.0% Mercury 0.1% to 0.5% Preferable amount 0.25% Aluminum 0.02% to 0.05%-Preferab1e amount 0.03%
. Magnesium" 0.05% to 0.1% -Preterab1e amount 0.075% Lithium 0.02% to 0.06%-Preferable amount 0.04% Potassium 0.02% to 0.06%'Preferable amount 0.04%
Lead to make up 100%.
The addition of the lithium and potassium increases the hardness of the alloy where hardness is a desideratum, but at the cost of increased corrosibility.
The hardness of the alloy may vary from 18 to 26 Brinell. It may be raised to 28 Brinell by increase of the calcium, but in this .case the danger of corrosion and drossing is somewhat increased.
The alloy, as above described, or other hardened or toughened lead compound containing easily oxidizable metals, may be made by one of the two following methods:
7 First method.The lead is melted and covered with calcium chloride and the temperature raised to approximately 1600 Fahronheit, to insure the melting of the calcium chloride, which may form a layer of an inch in thickness on the lead. The metals to be compounded with the lead and which are of a readily oxidizable character are introduced into the molten lead through the calcium chloride flux or covering stratum. The tinand aluminum may be so introduced either as separate metals or, (which is preferable as a matter of convenience), the aluminum and the tin, in whole or part, may be introduced as tin-aluminum .alloy. The batch is stirred until the aluminum is completely dissolved in the lead, or so much dissolved as can be held in solution in the lead. The magnesium is next introduced into the batch in the same manner and thereafter the calcium, as metallic calcium. The calcium is introduced into the lead' after the other ingredients above named, in order to prevent foaming of the calcium chloride covering, which is like- 1y to occur if the calcium is put in first or if all of the before mentioned ingredients are introduced into the lead at the same time. The lead is now allowed to cool down to a temperature of about 600 to 700 F. the calcium chloride covering stripped off, at
' about 1000 F., and themercury added, preferably as a mercury tin alloy. Alternatively the crucible may be removed from the furnace and allowed to cool to dull red heat, approximately 1200 to 1300 F. and the mercury tin alloy introduced through the flux. This causes a slight loss of mercury but tends to give a better pouring metal. If lithium and/or potassium are used, they are introduced into the melt with the mercury, that is while the batch is at a relatively low temperature, and rosin is added, which by burning creates fumes which keep the air from coming in contact with the metal.
The supernatant calcium chloride stratum on the lead batch serves to keep the air from contact with the molten metal and thereby prevents or materially lessens oxidation of the lead and other metals. Any metal susceptible to oxidation is likely to be covered with a film of oxide. In passing the pieces of tinaluminum alloy, magnesium and calcium through the calcium chloride stratum, the oxide films on these metals are dissolved by the calcium chloride- The lead will also be, ordinarily, superficially oxidized and in the melting of the lead the oxide will rise to the top of the batch and be dissolved andretained by the calcium chloride stratum. It is only possible to dissolve metals of the t e ind1- cated in the lead if such metals are ree from oxide and the lead itself is. free from oxide. The batch must be stirred and if the calcium chloride were not present to absorb floating oxides of the metals, these oxides would be stirred into the body of the lead. The stratum of molten calcium chloride serves the triple function of cleansing the metals introduced into the lead, absorbing oxide from the lead itself and protecting the melt from oxidation by contact with the air.
Secmid method-The lead is melted and covered with a calcium chloride covering, as described in connection with the first method. The tin and aluminum, preferably as aluminum-tin alloy and metallic magnesium are introduced into the lead through the flux, as in the first method. The calcium is next introduced, not as metallic calcium, but as calcium-lead alloy. The amount of calcium in this case may be slightly less than when metallic calcium is used. The crucible is taken from the furnace and the melt allowed to cool to 600 to 700 F., the flux being stripped off. The mercury is then added as mercury-tin alloy; or one may introduce this ingredient to the flux as in the first method.
One advantage of using calcium-lead alloy instead of metallic calcium is that the alloy is .cheaper. It also contains less impurities into the molten than metallic calcium. Moreover, for a hear ing metal compound, the alloy will be slightly harder, stronger and in machining will cut more smoothly than when metallic calcium is used. There are fewer defects, such as laps, porous spots and shrinkages.
Except for the matter of expense, it is possible to use another halogen salt of calcium,
calcium bromide or calcium iodide in place of calcium chloride for the flux stratum.
This application is a continuation in part of my copending application Serial No. 297,- 119, filed Aug. 2, 1928, for Bearing metal.
I claim:
1. Method of compounding a lead alloy which consists in melting the lead under a. molten covering; introducing the tin, aluminum and magnesium into the lead through said covering and thereafter the calcium; and introducing the mercury, lithium, or potassium into the metallic body while it is at a temperature not substantially in excess of 700 degrees Fahrenheit.
2. Method of compounding a lead alloy which comprises: melting the lead and holding the same at a temperature of approxi mately ,1600 degrees Fahrenheit under 2. molten covering of calcium chloride; introduc ing the tin, aluminum and magnesium into the lead under said covering and thereafter the calcium; allowing the melt to come down to a temperature of approximately 600 degrees to 700 degrees Fahrenheit and introducing the mercury, lithium and potassium body at approximately this temperature.
3. Method of compounding a lead allo which comprises: melting the lead and hol ing the same at a temperature of approximately 1600 de rees Fahrenheit under a moltencovering 0 calcium chloride; introducing the tin, aluminum, and magnesium into the lead under said covering and thereafter the calcium; introducing rosin into the lead when the latter is at a temperature of about 600 to 700 degrees Fahrenheit, and while the rosin is burning introducing lithium or potassium into the molten body.
4. Method of making a lead alloy containing aluminum, magnesium and calcium in which the lead in the molten state is covered by a stratum vof calcium chloride and the aluminum and magnesium first introduced into the lead and thereafter the calcium, all through said calcium chloride stratum.
5. Method of compounding a hardened lead alloy which comprises melting the lead under a covering of calcium chloride, introducing tin, aluminum, magnesium and calcium into the lead through the calcium chloride covering, reducin the temperature of the melt and introduclng mercury into the
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US491081A US1916496A (en) | 1930-10-24 | 1930-10-24 | Method of making lead alloys |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US491081A US1916496A (en) | 1930-10-24 | 1930-10-24 | Method of making lead alloys |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1916496A true US1916496A (en) | 1933-07-04 |
Family
ID=23950702
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US491081A Expired - Lifetime US1916496A (en) | 1930-10-24 | 1930-10-24 | Method of making lead alloys |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1916496A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3647545A (en) * | 1969-06-02 | 1972-03-07 | Gould National Batteries Inc | Battery electrode grids made from tin-lithium-lead alloy |
| US3881953A (en) * | 1973-11-26 | 1975-05-06 | St Joe Minerals Corp | Battery electrode grids and method of making same from a lead-calcium-lithium-tin alloy |
| US4233070A (en) * | 1978-05-26 | 1980-11-11 | Chloride Group Limited | Lead alloys for electric storage battery |
| US4439398A (en) * | 1981-11-13 | 1984-03-27 | Rsr Corporation | Method of alloying calcium and aluminum into lead |
-
1930
- 1930-10-24 US US491081A patent/US1916496A/en not_active Expired - Lifetime
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3647545A (en) * | 1969-06-02 | 1972-03-07 | Gould National Batteries Inc | Battery electrode grids made from tin-lithium-lead alloy |
| US3881953A (en) * | 1973-11-26 | 1975-05-06 | St Joe Minerals Corp | Battery electrode grids and method of making same from a lead-calcium-lithium-tin alloy |
| US4233070A (en) * | 1978-05-26 | 1980-11-11 | Chloride Group Limited | Lead alloys for electric storage battery |
| US4439398A (en) * | 1981-11-13 | 1984-03-27 | Rsr Corporation | Method of alloying calcium and aluminum into lead |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US3620716A (en) | Magnesium removal from aluminum alloy scrap | |
| US1916496A (en) | Method of making lead alloys | |
| US2768893A (en) | Brazing alloys | |
| US1906567A (en) | Metal alloy | |
| US2261906A (en) | Method of alloying magnesium with manganese | |
| US2793115A (en) | Brazing alloys | |
| US2678267A (en) | Method of making an alloy comprising magnesium and thorium | |
| US2134905A (en) | Manufacture of cast iron | |
| US2266122A (en) | Silicon alloy | |
| US2261905A (en) | Method of alloying magnesium with manganese | |
| US2604394A (en) | Magnesium base alloys | |
| US1452750A (en) | Readily-fusible alloy | |
| JPS6035418B2 (en) | Manufacturing method of lead-calcium-aluminum alloy | |
| US2472025A (en) | Method of treatment of magnesiumbase alloys | |
| US2281528A (en) | Method of heating and melting precious metals and flux composition therefor | |
| US2073020A (en) | Method of improving the physical and mechanical properties of alloys | |
| US2497538A (en) | Fluxes for use in the treatment of light metals | |
| US1731210A (en) | Gold alloy | |
| US2686946A (en) | Refining beryllium in the presence of a flux | |
| US1915932A (en) | Magnesium-cerium alloy | |
| US2266123A (en) | Silicon alloy and its use in the treatment of iron and steel | |
| US1745721A (en) | Bearing metal | |
| US1983604A (en) | Production of refined metal | |
| US2409020A (en) | Method for desulphurizing iron with molten calcium carbide | |
| US935863A (en) | Alloy and process for its production. |