US451405A - Aluminium alloy - Google Patents
Aluminium alloy Download PDFInfo
- Publication number
- US451405A US451405A US451405DA US451405A US 451405 A US451405 A US 451405A US 451405D A US451405D A US 451405DA US 451405 A US451405 A US 451405A
- Authority
- US
- United States
- Prior art keywords
- aluminium
- alloy
- titanium
- oxide
- per cent
- 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 10
- 239000004411 aluminium Substances 0.000 description 46
- 229910052782 aluminium Inorganic materials 0.000 description 46
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminum Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 46
- 229910045601 alloy Inorganic materials 0.000 description 26
- 239000000956 alloy Substances 0.000 description 26
- REDXJYDRNCIFBQ-UHFFFAOYSA-N aluminium(3+) Chemical class [Al+3] REDXJYDRNCIFBQ-UHFFFAOYSA-N 0.000 description 24
- RTAQQCXQSZGOHL-UHFFFAOYSA-N titanium Chemical compound [Ti] RTAQQCXQSZGOHL-UHFFFAOYSA-N 0.000 description 22
- 239000010936 titanium Substances 0.000 description 22
- 229910052719 titanium Inorganic materials 0.000 description 22
- 150000003839 salts Chemical class 0.000 description 14
- 239000011780 sodium chloride Substances 0.000 description 14
- 150000002222 fluorine compounds Chemical class 0.000 description 12
- KRHYYFGTRYWZRS-UHFFFAOYSA-M fluoride anion Chemical compound [F-] KRHYYFGTRYWZRS-UHFFFAOYSA-M 0.000 description 10
- XEEYBQQBJWHFJM-UHFFFAOYSA-N iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 8
- 229910052751 metal Inorganic materials 0.000 description 8
- 239000002184 metal Substances 0.000 description 8
- KEAYESYHFKHZAL-UHFFFAOYSA-N sodium Chemical compound [Na] KEAYESYHFKHZAL-UHFFFAOYSA-N 0.000 description 8
- 239000011734 sodium Substances 0.000 description 8
- 229910052708 sodium Inorganic materials 0.000 description 8
- 230000004927 fusion Effects 0.000 description 6
- 229910001069 Ti alloy Inorganic materials 0.000 description 4
- 238000005275 alloying Methods 0.000 description 4
- 239000002585 base Substances 0.000 description 4
- OKTJSMMVPCPJKN-UHFFFAOYSA-N carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 4
- 229910052799 carbon Inorganic materials 0.000 description 4
- 229910052742 iron Inorganic materials 0.000 description 4
- 238000004519 manufacturing process Methods 0.000 description 4
- 239000000047 product Substances 0.000 description 4
- 238000005096 rolling process Methods 0.000 description 4
- VYPSYNLAJGMNEJ-UHFFFAOYSA-N silicium dioxide Chemical compound O=[Si]=O VYPSYNLAJGMNEJ-UHFFFAOYSA-N 0.000 description 4
- 229910052710 silicon Inorganic materials 0.000 description 4
- 239000010703 silicon Substances 0.000 description 4
- 229910001369 Brass Inorganic materials 0.000 description 2
- REHXRBDMVPYGJX-UHFFFAOYSA-H Sodium hexafluoroaluminate Chemical compound [Na+].[Na+].[Na+].F[Al-3](F)(F)(F)(F)F REHXRBDMVPYGJX-UHFFFAOYSA-H 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 239000002253 acid Substances 0.000 description 2
- 239000003513 alkali Substances 0.000 description 2
- 239000010951 brass Substances 0.000 description 2
- OYPRJOBELJOOCE-UHFFFAOYSA-N calcium Chemical compound [Ca] OYPRJOBELJOOCE-UHFFFAOYSA-N 0.000 description 2
- 239000011575 calcium Substances 0.000 description 2
- 229910052791 calcium Inorganic materials 0.000 description 2
- 150000001875 compounds Chemical class 0.000 description 2
- 239000000470 constituent Substances 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 229910001610 cryolite Inorganic materials 0.000 description 2
- 230000002950 deficient Effects 0.000 description 2
- 230000002939 deleterious Effects 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- -1 fluorides chlorides Chemical class 0.000 description 2
- 230000005484 gravity Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 229910001092 metal group alloy Inorganic materials 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- 239000000203 mixture Substances 0.000 description 2
- MYMOFIZGZYHOMD-UHFFFAOYSA-N oxygen Chemical compound O=O MYMOFIZGZYHOMD-UHFFFAOYSA-N 0.000 description 2
- 229910052760 oxygen Inorganic materials 0.000 description 2
- 239000001301 oxygen Substances 0.000 description 2
- 239000002893 slag Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 239000000126 substance Substances 0.000 description 2
- 239000006228 supernatant Substances 0.000 description 2
- GWEVSGVZZGPLCZ-UHFFFAOYSA-N titan oxide Chemical compound O=[Ti]=O GWEVSGVZZGPLCZ-UHFFFAOYSA-N 0.000 description 2
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
Definitions
- My invention which relates to an improvement in alloys of aluminium, is based upon a lo discovery which I have made that aluminium when alloyed with titanium, especially in certain proportions, gives a new product, which, together with the many useful properties of aluminium which render it capable of such 5 varied application in the arts, possesses other beneficial properties in which aluminium is deficient.
- pure aluminium is somewhat soft and only slightly elastic, even after hammering or rolling, if it be alloyed with less than ten per cent, preferably between one-half of one per cent. and ten per cent.
- titanium a product is obtained intrinsicallyharder than aluminium, approximately as incorrodible, and ca- 5 pable of acquiring by hammering or rolling a degree of elasticity and hardness comparable to spring-brass.
- Such alloy is fusible at a temperature below the melting-point of steel, and it is with reference to this tempera 3 ture that I use the word fusible in the specification and claims. Its fusing-point and specific gravity increase with the proportion of titanium which it contains. WVhen the proportion of titanium is less than five per cent, the alloy is nearly as malleable as pure aluminium, and its malleability decreases and its hardness increases as the proportion of titanium in the alloy is increased.
- the oxide or salt is reduced. Its oxygen or acid radical combines with a part of the aluminium, and the freed metallic base immediately alloys with the remainder of the aluminium.
- the contents of the crucible are poured into a suitable receptable, and after cooling somewhat the melted fluoride can be separated as a supernatant slag from the metallic alloy at the bottom of the vessel.
- the alloy is then col- It is important that the reduction of the oxide orsaltof titanium and its alloying with the aluminium should be conducted in a non-silicious crucible, (preferably a carbon crueible,) since if the vessel be silicious in its composition a considerable portion of silicon will be alloyed with the aluminium and titanium, producing a compound of inferior quality.
- an alloy of titanium and aluminium containing less than ten per cent. of titanium substantially as specified.
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
UNITED STATES PATENT OFFICE.
JOHN IV. LANGLEY, OF EDGE\VOODVILLE, ASIGNOR OF ONE-HALF 'lO IIUNI & OLAPP, OF PITTSBURG, PENNSYLVANIA.
ALUMINIUM ALLOY.
SPECIFICATION forming part of Letters Patent No. 451,405, dated April 28, 1891.
Application filed September 20, 1890. Serial No. 365,658. (No specimens.)
To all whom, it may concern.-
Be it known that 1, JOHN W. LANGLEY, of Edgewoodville, in the county of Allegheny and State of Pennsylvania, have invented a new and useful Improvement in Aluminium Alloys, of which the following is a full, clear, and exact description.
My invention, which relates to an improvement in alloys of aluminium, is based upon a lo discovery which I have made that aluminium when alloyed with titanium, especially in certain proportions, gives a new product, which, together with the many useful properties of aluminium which render it capable of such 5 varied application in the arts, possesses other beneficial properties in which aluminium is deficient. Thus I have found that although pure aluminium is somewhat soft and only slightly elastic, even after hammering or rolling, if it be alloyed with less than ten per cent, preferably between one-half of one per cent. and ten per cent. of titanium, a product is obtained intrinsicallyharder than aluminium, approximately as incorrodible, and ca- 5 pable of acquiring by hammering or rolling a degree of elasticity and hardness comparable to spring-brass. Such alloy is fusible at a temperature below the melting-point of steel, and it is with reference to this tempera 3 ture that I use the word fusible in the specification and claims. Its fusing-point and specific gravity increase with the proportion of titanium which it contains. WVhen the proportion of titanium is less than five per cent, the alloy is nearly as malleable as pure aluminium, and its malleability decreases and its hardness increases as the proportion of titanium in the alloy is increased. I have found that the best material for commercial 4 use, where elasticity combined with easy malleability is required, is an alloy containing titanium from about one half of one per cent. (more or less) to two per cent. The alloy, when it contains less than ten per cent. of titanium,is of marked value in the arts. I
have foundthat the presence of iron or silicon in the alloy is deleterious and tends to make it brittle and non-malleable. Care should therefore be taken in the manufacture 5 of the alloy that these elements should not be combined in any considerable proportion.
I shall now describe a method by which my improved alloy can be made economically and with facility. This method, which I deem to be the best to be used for thispurpose, Ihave made the subject of a separate'patent application, and I do notintend to limit the claims of this application to its employment, since within the scope of the present invention my new alloy can be produced by fusion with aluminium of a rich alloy containing aluminium and titanium. In practicing said method I proceed as follows: I make by fusion a bath of fluorides of aluminium and sodium, or of fluoride of sodium, or of fluorides of aluminium, sodium, and calcium, or generally a fluoride or fluorides of a metal or metals more clectro-positive than aluminium. I may add to these fluorides chlorides of the alkalies or alkaline earths; but these are unnec- 7o essary. Cryolite of commerce may be used as the fluoride constituent of the bath; but, although I do not exclude its use from the scope of the broad claim of this application, it is in some respects disadvantageous because of its iron, which in the alloying processhercinafter described is reduced, and by mingling with the alloyimpairs its quality. For this reason I prefer to employ the above-mentioned fluorides in as pure state as possible. Either before or after the fusion of this fluoride bath I add to it a reducible oxide or salt of the rare metal to be alloyed (in making an alloy of aluminium and titanium titanic oxide is preferably used) and after thorough admixture of these substances I introduce the aluminium.
A reaction between the aluminium and said oxide or salt at once takes place. The oxide or salt is reduced. Its oxygen or acid radical combines with a part of the aluminium, and the freed metallic base immediately alloys with the remainder of the aluminium.
In practice I prefer to use as the fluoride loath fluorides of aluminium and sodium, which may be employed in amount ranging from one hundred to four hundred per cent. of the weight of the aluminium intended to be added. This bath I melt in a carbon crucible and add thereto the oxide or salt of the metal to be alloyed. hen the whole mass is incorporated and as nearly fluid as possible, I charge metallic aluminium into the cru- IOO cible, the relative proportions of the aluminium and oxide or salt being such that the percentage of oxide or salt shall be about twice the percentage in which its metallic base is desired to be present in the alloy. Immediately on the introduction of the aluminium the reaction above noted takes place between the aluminium and the oxide or salt, and is accompanied by a rapid elevation of temperature of the bath. After waiting until further reaction ceases, which is indicated by cessation of rise of the temperature, the contents of the crucible are poured into a suitable receptable, and after cooling somewhat the melted fluoride can be separated as a supernatant slag from the metallic alloy at the bottom of the vessel. The alloy is then col- It is important that the reduction of the oxide orsaltof titanium and its alloying with the aluminium should be conducted in a non-silicious crucible, (preferably a carbon crueible,) since if the vessel be silicious in its composition a considerable portion of silicon will be alloyed with the aluminium and titanium, producing a compound of inferior quality.
As a new article of manufacture, an alloy of titanium and aluminium containing less than ten per cent. of titanium, substantially as specified.
In testimony whereof I have hereunto set my hand this 18th day of September, A. D. 1890.
JOHN XV. LANGLEY.
\Vitnesses:
THOMAS W. BAKEWELL, W. B. Oonwm.
Publications (1)
Publication Number | Publication Date |
---|---|
US451405A true US451405A (en) | 1891-04-28 |
Family
ID=2520287
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US451405D Expired - Lifetime US451405A (en) | Aluminium alloy |
Country Status (1)
Country | Link |
---|---|
US (1) | US451405A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2768075A (en) * | 1942-12-12 | 1956-10-23 | Sterental Volf | Melting, remelting and recovering of aluminium and its alloys |
US2931722A (en) * | 1956-11-21 | 1960-04-05 | Nat Lead Co | Aluminum-titanium master alloys |
US2939786A (en) * | 1955-07-29 | 1960-06-07 | Vaw Ver Aluminium Werke Ag | Method of producing titanium and titanium alloys |
US2955935A (en) * | 1956-11-21 | 1960-10-11 | Nat Lead Co | Manufacture of aluminum titanium alloys |
-
0
- US US451405D patent/US451405A/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2768075A (en) * | 1942-12-12 | 1956-10-23 | Sterental Volf | Melting, remelting and recovering of aluminium and its alloys |
US2939786A (en) * | 1955-07-29 | 1960-06-07 | Vaw Ver Aluminium Werke Ag | Method of producing titanium and titanium alloys |
US2931722A (en) * | 1956-11-21 | 1960-04-05 | Nat Lead Co | Aluminum-titanium master alloys |
US2955935A (en) * | 1956-11-21 | 1960-10-11 | Nat Lead Co | Manufacture of aluminum titanium alloys |
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