US1916087A - Aluminum alloy - Google Patents
Aluminum alloy Download PDFInfo
- Publication number
- US1916087A US1916087A US668666A US66866633A US1916087A US 1916087 A US1916087 A US 1916087A US 668666 A US668666 A US 668666A US 66866633 A US66866633 A US 66866633A US 1916087 A US1916087 A US 1916087A
- Authority
- US
- United States
- Prior art keywords
- alloys
- aluminum
- boron
- silicon
- 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
- 229910000838 Al alloy Inorganic materials 0.000 title description 3
- 229910045601 alloy Inorganic materials 0.000 description 24
- 239000000956 alloy Substances 0.000 description 24
- 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
- ZOXJGFHDIHLPTG-UHFFFAOYSA-N Boron Chemical compound [B] ZOXJGFHDIHLPTG-UHFFFAOYSA-N 0.000 description 16
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 16
- 229910052796 boron Inorganic materials 0.000 description 16
- 229910052710 silicon Inorganic materials 0.000 description 16
- 239000010703 silicon Substances 0.000 description 16
- 229910052751 metal Inorganic materials 0.000 description 13
- 239000002184 metal Substances 0.000 description 13
- 150000002739 metals Chemical class 0.000 description 10
- PXHVJJICTQNCMI-UHFFFAOYSA-N Nickel Chemical compound [Ni] PXHVJJICTQNCMI-UHFFFAOYSA-N 0.000 description 6
- 239000000203 mixture Substances 0.000 description 5
- 238000005260 corrosion Methods 0.000 description 4
- 230000007797 corrosion Effects 0.000 description 4
- 229910052720 vanadium Inorganic materials 0.000 description 4
- LEONUFNNVUYDNQ-UHFFFAOYSA-N vanadium atom Chemical compound [V] LEONUFNNVUYDNQ-UHFFFAOYSA-N 0.000 description 4
- 230000007423 decrease Effects 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- 229910052759 nickel Inorganic materials 0.000 description 3
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 2
- 239000003610 charcoal Substances 0.000 description 2
- 229910017052 cobalt Inorganic materials 0.000 description 2
- 239000010941 cobalt Substances 0.000 description 2
- GUTLYIVDDKVIGB-UHFFFAOYSA-N cobalt atom Chemical compound [Co] GUTLYIVDDKVIGB-UHFFFAOYSA-N 0.000 description 2
- 229910052802 copper Inorganic materials 0.000 description 2
- 239000010949 copper Substances 0.000 description 2
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 description 1
- ZOKXTWBITQBERF-UHFFFAOYSA-N Molybdenum Chemical compound [Mo] ZOKXTWBITQBERF-UHFFFAOYSA-N 0.000 description 1
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 1
- 229910052810 boron oxide Inorganic materials 0.000 description 1
- 239000002775 capsule Substances 0.000 description 1
- 229910052804 chromium Inorganic materials 0.000 description 1
- 239000011651 chromium Substances 0.000 description 1
- 239000004020 conductor Substances 0.000 description 1
- JKWMSGQKBLHBQQ-UHFFFAOYSA-N diboron trioxide Chemical compound O=BOB=O JKWMSGQKBLHBQQ-UHFFFAOYSA-N 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 229910052750 molybdenum Inorganic materials 0.000 description 1
- 239000011733 molybdenum Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 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
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
Definitions
- My invention relates to a series of aluminum alloys of novel composition and properties.
- the alloys of my invention are particularly characterized by the presence of boron, magnesium and silicon.
- Alloys consisting principally of aluminum and containing substantial amounts of boron, magnesium and silicon are characterized by being lighter, harder and stronger than aluminum.
- the amount of magnesium in the new alloys may vary from about 0.25 to about 5.0%, although it is generally desirable to add hot more than about 1.5% of magnesium.
- the amount of boron may vary from about 0.05% to about 2.0, although at least 0.25% is preferable, and in many cases it ispreferable to add not more than 1% of boron due to the increased brittleness caused by higher amounts.
- the silicon may advantageously be present in amounts of from about 0.5% to about 7.5%, and in general it is preferable that not more than about 4.5% of silicon be present.
- the amount of aluminum should in general be at least about 90%. For many purposes it is advantageous to use aluminum in amounts of from about 93% to about 96%.
- alloys consisting substantially solely of aluminum, magnesium, boron and silicon are valuable for many uses, the alloys are particularly valuable when they also contain other metals.
- Alloys of aluminum, magnesium, boron and silicon containing such metals as copper, nickel, cobalt, zinc, vanadium, tungsten, molybdenum and chromium provide a series of alloys characterized by 5 their light weight, together with high hardvness, tensile strength, and resistance to corrosion. In general, the new alloys have a surprisingly high electrical conductivity.
- An alloy which is particularly valuable for the manufacture of electrical conductors, because of its high conductivity and tensile strength, has the. following composition:
- vanadium Percent Magnesium 1.50 Boron 0.75 Silicon 3.00 Cobalt 2.25 Aluminum Remainder
- An example of a useful alloy of the invention containing vanadium is the following:
- a principal function of boron in the alloys of the inven tion is to increase the hardness and conductivity of the alloys and to increase their resistance to corrosion
- a principal function of the magnesium is to decrease the specific gravity and increase the resistance to corrosion
- a principal function of the silicon 15 to increase the tensile strength and corrosiomresistance and to decrease the specific gravity.
- the metals may be utilized in the cast condition or they may be rolled, drawn or otherwise worked.
- Mechanical working is advancarried out at a temperature of 150-450 C. and such working efiects a material increase in the tensile strength of the alloys.
- An advantageous method of producing the alloys of the invention is as follows: The aluminum is melted in a crucible and covered with a layer of powdered charcoal.
- The. charcoal serves to protect the metal from oxidation and to reduce those metals which are added the form of oxides.
- the magnesium and silicon are added as metal and the boron as oxides.
- Other metals may be added as such or in the form of their oxides, according to the nature of the particular metal.
- the added metals or their oxides are advantageously added enclosed in aluminum capsules.
- the boron oxide is preferably added to the melted aluminum first. The other metals or oxides may be added together.
- Alloys consisting principally of aluminum and characterized by containing from 0.05% to 2.0% of boron, from 0.25% to 5.0% of magnesium, and from 0.5% to 7.5% of silicon.
- Alloys consisting principally of aluminum and characterized by containing from 0.25% to 1.0% of boron, from 0.25% to 1.5% of magnesium, and from 0.5% to 4.5% of silicon.
- Alloys consisting principally of aluminum and characterized by containing about 0.25% .of boron, about 0.50% of magnesium, and about 0.65% of silicon.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Manufacture Of Alloys Or Alloy Compounds (AREA)
Description
Patented June 27, 1933 UNITED STATES PATENT, OFFICE C0 I TBT C. TITUS, OF NEW YORK, N. Y.
ALUMINUM ALLOY No Drawing.
My invention relates to a series of aluminum alloys of novel composition and properties. The alloys of my invention are particularly characterized by the presence of boron, magnesium and silicon. Y
Alloys consisting principally of aluminum and containing substantial amounts of boron, magnesium and silicon are characterized by being lighter, harder and stronger than aluminum. The amount of magnesium in the new alloys may vary from about 0.25 to about 5.0%, although it is generally desirable to add hot more than about 1.5% of magnesium. The amount of boron may vary from about 0.05% to about 2.0, although at least 0.25% is preferable, and in many cases it ispreferable to add not more than 1% of boron due to the increased brittleness caused by higher amounts. The silicon may advantageously be present in amounts of from about 0.5% to about 7.5%, and in general it is preferable that not more than about 4.5% of silicon be present. The amount of aluminum should in general be at least about 90%. For many purposes it is advantageous to use aluminum in amounts of from about 93% to about 96%.
While the alloys consisting substantially solely of aluminum, magnesium, boron and silicon are valuable for many uses, the alloys are particularly valuable when they also contain other metals. Alloys of aluminum, magnesium, boron and silicon containing such metals as copper, nickel, cobalt, zinc, vanadium, tungsten, molybdenum and chromium provide a series of alloys characterized by 5 their light weight, together with high hardvness, tensile strength, and resistance to corrosion. In general, the new alloys have a surprisingly high electrical conductivity.
The following specific formulae are illusfrom 0.25 to 7.5%,
trative of the wide range of compositions of the invention:
An alloy which is particularly valuable for the manufacture of electrical conductors, because of its high conductivity and tensile strength, has the. following composition:
' Percent Magnesium 0.50 Boron 0.25
a Silicon 0.65 Aluminum Remainder An alloy of high malleability and good Application filed April 29,
1933. Serial N0. 688,666.
conductivity is represented by the following composition Percent Magnesium 0.75 Boron 0.50 SiliOOll 3.50 0 Copper 3.00
lummum Remamder The following alloy is characterized by its high tensile strength: V
Percent Magnesium 1.00
oron 0.50 Silicon" 3.50 Nickel 3.00 7 Aluminum Remainder Another alloy of high tensile strength has the composition:
Percent Magnesium 1.50 Boron 0.75 Silicon 3.00 Cobalt 2.25 Aluminum Remainder The presence of vanadium in alloys of the an invention increases their tensile strength and toughness and decreases the tendency to crystalhzation in use. An example of a useful alloy of the invention containing vanadium is the following:
f Percent Magnesium 0.50 Boron 0.35 Silicon 2.75 Nickel 2.65 Vanadium 0.75 Aluminum Remainder Metals other than aluminum, magnesium, boron and silicon may, in general, be present In the alloys. of the invention in amounts of although the presence of not more than 5% of such other metals is frequently desirable.
In'general it may be said that a principal function of boron in the alloys of the inven tion is to increase the hardness and conductivity of the alloys and to increase their resistance to corrosion, a principal function of the magnesium is to decrease the specific gravity and increase the resistance to corrosion, While a principal function of the silicon 15 to increase the tensile strength and corrosiomresistance and to decrease the specific gravity.
2.7 4, a tensile strength when cast tageously As indicated above, other metals may be added for the purpose of increasing tensile strength, malleability, resistance to corrosion, electrical conductivity and other special properties.
Alloys of the invention as described above have been obtained having a specific gravity of from 2.60 to 2.80, more generally 2.66 to of 27,000 to 35,000 pounds per square inch, and when mechanically worked of from 36,000 to 55,000
ounds; and an electrical conductivity as high as 56 (Ag=100). Rolled sheets of alloys of the invention have shown an elongation at break as high as 26%.
The metals may be utilized in the cast condition or they may be rolled, drawn or otherwise worked. Mechanical working is advancarried out at a temperature of 150-450 C. and such working efiects a material increase in the tensile strength of the alloys.
An advantageous method of producing the alloys of the invention is as follows: The aluminum is melted in a crucible and covered with a layer of powdered charcoal. The. charcoal serves to protect the metal from oxidation and to reduce those metals which are added the form of oxides. The magnesium and silicon are added as metal and the boron as oxides. Other metals may be added as such or in the form of their oxides, according to the nature of the particular metal. The added metals or their oxides are advantageously added enclosed in aluminum capsules. The boron oxide is preferably added to the melted aluminum first. The other metals or oxides may be added together.
I claim: Y
1. Alloys consisting principally of aluminum and characterized by containing from 0.05% to 2.0% of boron, from 0.25% to 5.0% of magnesium, and from 0.5% to 7.5% of silicon.
2. Alloys consisting principally of aluminum and characterized by containing from 0.25% to 1.0% of boron, from 0.25% to 1.5% of magnesium, and from 0.5% to 4.5% of silicon.
3. Alloys consisting principally of aluminum and characterized by containing about 0.25% .of boron, about 0.50% of magnesium, and about 0.65% of silicon.
Intestimony whereof, I afiix my signature.
' COURT' G. TITUSW
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US668666A US1916087A (en) | 1933-04-29 | 1933-04-29 | Aluminum alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US668666A US1916087A (en) | 1933-04-29 | 1933-04-29 | Aluminum alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1916087A true US1916087A (en) | 1933-06-27 |
Family
ID=24683274
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US668666A Expired - Lifetime US1916087A (en) | 1933-04-29 | 1933-04-29 | Aluminum alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1916087A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3149001A (en) * | 1962-04-05 | 1964-09-15 | Aluminum Co Of America | Enameled aluminous metal product |
| US3807969A (en) * | 1970-07-13 | 1974-04-30 | Southwire Co | Aluminum alloy electrical conductor |
| US3807016A (en) * | 1970-07-13 | 1974-04-30 | Southwire Co | Aluminum base alloy electrical conductor |
| US3830635A (en) * | 1971-05-26 | 1974-08-20 | Southwire Co | Aluminum nickel alloy electrical conductor and method for making same |
| US4631236A (en) * | 1984-02-23 | 1986-12-23 | Swiss Aluminium Ltd. | Process for manufacturing a device and extrusion billet for this |
-
1933
- 1933-04-29 US US668666A patent/US1916087A/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3149001A (en) * | 1962-04-05 | 1964-09-15 | Aluminum Co Of America | Enameled aluminous metal product |
| US3807969A (en) * | 1970-07-13 | 1974-04-30 | Southwire Co | Aluminum alloy electrical conductor |
| US3807016A (en) * | 1970-07-13 | 1974-04-30 | Southwire Co | Aluminum base alloy electrical conductor |
| US3830635A (en) * | 1971-05-26 | 1974-08-20 | Southwire Co | Aluminum nickel alloy electrical conductor and method for making same |
| US4631236A (en) * | 1984-02-23 | 1986-12-23 | Swiss Aluminium Ltd. | Process for manufacturing a device and extrusion billet for this |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US1916087A (en) | Aluminum alloy | |
| US3725056A (en) | Aluminum bronze alloy having improved mechanical properties at elevated temperatures | |
| US2306667A (en) | Alloy | |
| US2310231A (en) | Brazing solder | |
| US2072911A (en) | Alloy | |
| US1933390A (en) | Copper zinc silicon alloys | |
| US1903843A (en) | Aluminum alloy | |
| US2073515A (en) | Alloy | |
| US2371531A (en) | Magnesium base alloy | |
| US2270193A (en) | Magnesium base alloy | |
| US1903842A (en) | Aluminum alloy | |
| US1886251A (en) | Magnesium-manganese-zinc alloys | |
| US1932843A (en) | Aluminum alloys | |
| US2072910A (en) | Alloy | |
| US2305825A (en) | Magnesium alloy | |
| US2661285A (en) | Nonferrous alloy | |
| US2090895A (en) | Aluminium alloy | |
| US2279712A (en) | Magnesium base alloy | |
| US2944892A (en) | Silver alloys | |
| US2163369A (en) | Lead alloy | |
| US2116275A (en) | Aluminium alloy | |
| US2270194A (en) | Magnesium base alloy | |
| US2270195A (en) | Magnesium base alloy | |
| US2108050A (en) | Alloys | |
| US2270191A (en) | Magnesium base alloy |