US1510242A - Alloy and apparatus made therefrom - Google Patents
Alloy and apparatus made therefrom Download PDFInfo
- Publication number
- US1510242A US1510242A US385597A US38559720A US1510242A US 1510242 A US1510242 A US 1510242A US 385597 A US385597 A US 385597A US 38559720 A US38559720 A US 38559720A US 1510242 A US1510242 A US 1510242A
- Authority
- US
- United States
- Prior art keywords
- alloy
- silicon
- aluminum
- copper
- made therefrom
- 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 25
- 239000000956 alloy Substances 0.000 title description 25
- 229910052782 aluminium Inorganic materials 0.000 description 32
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 32
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 31
- 229910052710 silicon Inorganic materials 0.000 description 31
- 239000010703 silicon Substances 0.000 description 31
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 25
- 229910052802 copper Inorganic materials 0.000 description 25
- 239000010949 copper Substances 0.000 description 25
- 229910001018 Cast iron Inorganic materials 0.000 description 8
- 238000005266 casting Methods 0.000 description 6
- 239000000203 mixture Substances 0.000 description 6
- 239000000463 material Substances 0.000 description 5
- 229910001092 metal group alloy Inorganic materials 0.000 description 5
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 4
- 238000002485 combustion reaction Methods 0.000 description 3
- 238000004519 manufacturing process Methods 0.000 description 3
- 229910052751 metal Inorganic materials 0.000 description 3
- 239000002184 metal Substances 0.000 description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 3
- 229910000906 Bronze Inorganic materials 0.000 description 2
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 description 2
- 239000010974 bronze Substances 0.000 description 2
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 2
- 230000007423 decrease Effects 0.000 description 2
- 229910052742 iron Inorganic materials 0.000 description 2
- 150000002739 metals Chemical class 0.000 description 2
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000881 Cu alloy Inorganic materials 0.000 description 1
- 229910000760 Hardened steel Inorganic materials 0.000 description 1
- 229910000676 Si alloy Inorganic materials 0.000 description 1
- 229910000831 Steel Inorganic materials 0.000 description 1
- 239000001996 bearing alloy Substances 0.000 description 1
- 229910052799 carbon Inorganic materials 0.000 description 1
- 238000003763 carbonization Methods 0.000 description 1
- 239000003245 coal Substances 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000012535 impurity Substances 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 239000003921 oil Substances 0.000 description 1
- 230000003647 oxidation Effects 0.000 description 1
- 238000007254 oxidation reaction Methods 0.000 description 1
- 230000001590 oxidative effect Effects 0.000 description 1
- 230000002035 prolonged effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
- 238000006467 substitution reaction Methods 0.000 description 1
- 229910002058 ternary alloy Inorganic materials 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C9/00—Alloys based on copper
- C22C9/10—Alloys based on copper with silicon as the next major constituent
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S277/00—Seal for a joint or juncture
- Y10S277/935—Seal made of a particular material
- Y10S277/939—Containing metal
- Y10S277/941—Aluminum or copper
Definitions
- This invention relates to metallic alloys and has for its purpose the provision of a composition of great hardness, moderate heat expansion and good casting qualities for commercial uses.
- Certain of the-properties'of my improved alloy vary according to the proportions of certain ingredients, these properties merging into each other gradually.
- the material In its upper range, the material has a great many properties of cast iron, namely, easy casting, ready machining, absence of ductility or warping, and a high degree of elasticity. In this range, it is particularly useful for the parts of internal combustion or other engines, especially cylinders and piston rings.
- My improved composition consists essentially of the ternary alloy of copper, aluminum, and silicon. Copper is at all times present to an amount of at least 87% and is preferably maintained below 97% because of the increasing softness of the material above that point. It is preferable to keep the silicon content less than that of the aluminum, although if the total amount of silicon is less than about 4% of the whole,
- a useful alloy can be produced having a content of aluminum less than that of silicon.
- Copper 97, silicon 2, aluminum 1, constitutes a rather soft, useful alloy
- aluminum 5 produces a similar alloy of greater hardness; copper 91, silicon 3,
- the limits of copper in my alloy are between about 87% and 97%; the limits of silicon are between about 2% and about 5% the limits of aluminum are between about 1% and about 10%.
- this material for bearings requires no particular description; in general the alloys containing upwards of 90% of copper are fitted for this use.
- the hardened and non-Warping varieties containing less than 90% of copper are peculiarly useful for the cylinders of internal combustion engines.
- the material has a scleroscope hardness of 50 as compared with about 30 for cast iron, it is practically immune to wear; for some unknown reason carbon deposits in such a cylinder are almost unknown; the weight is no greater than that of cast iron; the coeflicient of heat expansion is somewhat greater than cast iron being about midway between iron and aluminum in this regard.
- My improved alloy in its non-warping range also forms a most excellent composition for pistonrings, either in connection with iron cylinders or those of the same material. Another advantage of my alloy is that it isvery nearly immune to oxidation caused by prolonged heating in an oxidizing atmosphere. Its melting point is slightly below that of cast iron.
- the alloy No special precautions are required in the production or manipulation of the alloy. Electricity, gas or coal can beused as desired, and a furnace either of the hearth type or crucible type can be employed though I prefer the latter in small scale work.
- a furnace either of the hearth type or crucible type can be employed though I prefer the latter in small scale work.
- the aluminum and silicon are, first alloyed together in, any suitable manner, and the mixture added to a bath of molten copper. 5 I
- my improved alloy is in the manufacture of rubber molds, such forexample as those used for curing vehicle tires.
- the heat conductivity enables a certain saving in the time of curing, while the polished and incorrodible nature of the alloy avoids rusting and adhesion of the rubber and the ease of castin enables direct production of intricate tread forms,
- my improved alloy not only for .the particular uses mentioned, but also for all others to which it may be applicable, limiting myself in nowise, either use or composition, except as specifically recited in the claims hereto annexed.
- a metallic alloy for the purpose described consisting essentially of copper at least 87%, silicon between 2% and 5% and at least 1% of aluminum.
- a metallic alloy for the purpose de scribed consisting essentially of copper at least 87%, silicon between 2% and 5% and an amount of aluminum greater than the amount of silicon.
- a metallic alloy for the-purpose described containing at least about 87% of copper together with silicon and aluminum, there being at least about 2% of silicon present, and the aluminum content being in excess of the silicon.
- a metallic alloy for the purpose described containing essentially between 87% and 90% of copper, from 2 to 3% of silicon, and the balance aluminum.
- a non-warping, readily cast, non-corrodible, machinable alloy consisting essentially of from 87% to 90% of copper alloyed with silicon and aluminum, the aluminum constituting from 2 to 4K times that of the silicon.
- a non-warping alloy of silicon, aluminum, and copper for engine parts there being at least about 2% and not over about 5% of silicon, and between about 87% and 97% of copper, the balance being mostly aluminum.
- Apparatus for heat exchange made from a non-corrodible, machinable alloy consisting essentially of from 87% to 97% of copper alloyed with from 1% to 3% of silicon, and at least 1% of aluminum.
- a hollow, cylindrical body forming an element of a thermodynamic engine which is made of an alloy containing copper, silicon and aluminum, the copper being present in the amount of between 87% and 97%, the amount of aluminum being not materially less than that of silicon and silicon being present to at least 1%.
- a cylinder of an internal combustion engine formed from an alloy containing copper in the amount of from 87 to 90%, silicon, and aluminum in the amount of from two to four times the amount of the silicon and not less than 2% of the whole.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Cylinder Crankcases Of Internal Combustion Engines (AREA)
- Pistons, Piston Rings, And Cylinders (AREA)
Description
Patented Sept-30, 1924.
warren s'raras ALADAR PACZ, 0F CLEVELAND HEIGHTS, OHIO.
ALLOY .A 1\TI) APPARATUS MADE THEREFROM.
No Drawing.
To all whom it may concern:
Be it known that I, ALADAR PAoz, a citizen of the United States, residing at Cleveland Heights in the county of Cuyahoga and State of Ohio, have invented a certain new and useful Improvement in Alloys and Apparatus Made Therefrom, of which the following is a full, clear, and exact description.
This invention relates to metallic alloys and has for its purpose the provision of a composition of great hardness, moderate heat expansion and good casting qualities for commercial uses. Certain of the-properties'of my improved alloy vary according to the proportions of certain ingredients, these properties merging into each other gradually. In its upper range, the material has a great many properties of cast iron, namely, easy casting, ready machining, absence of ductility or warping, and a high degree of elasticity. In this range, it is particularly useful for the parts of internal combustion or other engines, especially cylinders and piston rings. In its lower range which is characterized by a certain degree of ductility it constitutes a valuable composition for bearings and other devices for which bronzes of tin and aluminum have heretofore been used, thus overcoming on the one hand the expense of tin and on the other hand the difficulty of casting the aluminum bronze. In both ranges the alloy is non-corrodible, non-ca-rbonizing, and easily lubricated.
My improved composition consists essentially of the ternary alloy of copper, aluminum, and silicon. Copper is at all times present to an amount of at least 87% and is preferably maintained below 97% because of the increasing softness of the material above that point. It is preferable to keep the silicon content less than that of the aluminum, although if the total amount of silicon is less than about 4% of the whole,
' a useful alloy can be produced having a content of aluminum less than that of silicon. For example: Copper 97, silicon 2, aluminum 1, constitutes a rather soft, useful alloy;
copper. 96, silicon 3, aluminum 1 is noticeably harder but liable to a tendency towards harshness; copper 95, silicon 3, aluminum 2 forms a good bearing alloy; copper 93, silicon 4, aluminum 3 produces an alloy having very little ductility but good casting properties. p
Application filed June 1,
1920. Serial 1V0. 385,597.
By maintaining the proportion of the silicon less than that of the aluminum it is possible to decrease the amount of copper yet more, for example: Copper 93, silicon 3, aluminum 4 producesa strong, ductile alloy for good bearings. etc.; copper 92, silicon 3,
aluminum 5 produces a similar alloy of greater hardness; copper 91, silicon 3,
produce a most excellent, non-warping, re-
silient alloy.
1- am aware that the alloy of copper 89, aluminum 11 makes a bronze which possesses Very poor casting qualities and almost devoid of elasticity. A ring or other resilient shape, when dropped upon the floor, collapses much the same as lead but the substitution of a small quantity of silicon for some of the aluminum affords to the alloy an elasticity comparable'with that of hardened steel.
The limits of copper in my alloy are between about 87% and 97%; the limits of silicon are between about 2% and about 5% the limits of aluminum are between about 1% and about 10%. I do not here consider the efiect of fourth metals, impurities, etc.; except to point out that metals having an atomic weight between 50 and possess a very pronounced hardening-effect and hence should ordinarily be excluded excepting where this property is peculiarly desired.
The use of this material for bearings requires no particular description; in general the alloys containing upwards of 90% of copper are fitted for this use. The hardened and non-Warping varieties containing less than 90% of copper are peculiarly useful for the cylinders of internal combustion engines. Inasmuch as the material has a scleroscope hardness of 50 as compared with about 30 for cast iron, it is practically immune to wear; for some unknown reason carbon deposits in such a cylinder are almost unknown; the weight is no greater than that of cast iron; the coeflicient of heat expansion is somewhat greater than cast iron being about midway between iron and aluminum in this regard. Accordingly, when used as a sleeve inside a cast aluminum water jacket, there is much less tendency towards separation between the jacket and sleeve than if a steel sleeve is employed; and whether the cylinder be water cooled or air cooled (but especially on the air cooled type) it is possible to fit an aluminum piston with a smaller clearance than in the case of a cast iron cylinder owing to the fact that the cylinder will expand more nearly at the same rate with the piston. The ready casting qualities of the alloy also enable a water jacket to be cast therein, the same as with cast iron. In all cases the higher heat conductivity of the metal maintains the oil film at a lower-temperature than in case cast iron be employed and thus reduces friction, decreases carbonization, minimizes gas leakage, and increase engine power.
My improved alloy in its non-warping range also forms a most excellent composition for pistonrings, either in connection with iron cylinders or those of the same material. Another advantage of my alloy is that it isvery nearly immune to oxidation caused by prolonged heating in an oxidizing atmosphere. Its melting point is slightly below that of cast iron.
No special precautions are required in the production or manipulation of the alloy. Electricity, gas or coal can beused as desired, and a furnace either of the hearth type or crucible type can be employed though I prefer the latter in small scale work. Preferably the aluminum and silicon are, first alloyed together in, any suitable manner, and the mixture added to a bath of molten copper. 5 I
Another very important use for my improved alloy is in the manufacture of rubber molds, such forexample as those used for curing vehicle tires. The heat conductivity enables a certain saving in the time of curing, while the polished and incorrodible nature of the alloy avoids rusting and adhesion of the rubber and the ease of castin enables direct production of intricate tread forms, Many other uses will occur to those skilled in the art, and I claim. and secure my improved alloy, not only for .the particular uses mentioned, but also for all others to which it may be applicable, limiting myself in nowise, either use or composition, except as specifically recited in the claims hereto annexed.
Having thus described my invention, what I claim is: I
1. A metallic alloy for the purpose described, consisting essentially of copper at least 87%, silicon between 2% and 5% and at least 1% of aluminum.
2. A metallic alloy for the purpose de scribed, consisting essentially of copper at least 87%, silicon between 2% and 5% and an amount of aluminum greater than the amount of silicon.
3. A metallic alloy for the-purpose described, containing at least about 87% of copper together with silicon and aluminum, there being at least about 2% of silicon present, and the aluminum content being in excess of the silicon.
4. A metallic alloy for the purpose described, containing essentially between 87% and 90% of copper, from 2 to 3% of silicon, and the balance aluminum.
5. A non-warping, readily cast, non-corrodible, machinable alloy consisting essentially of from 87% to 90% of copper alloyed with silicon and aluminum, the aluminum constituting from 2 to 4K times that of the silicon.
6. A non-warping alloy of silicon, aluminum, and copper for engine parts, there being at least about 2% and not over about 5% of silicon, and between about 87% and 97% of copper, the balance being mostly aluminum.
7. Apparatus for heat exchange made from a non-corrodible, machinable alloy consisting essentially of from 87% to 97% of copper alloyed with from 1% to 3% of silicon, and at least 1% of aluminum.
8. A hollow, cylindrical body forming an element of a thermodynamic engine which is made of an alloy containing copper, silicon and aluminum, the copper being present in the amount of between 87% and 97%, the amount of aluminum being not materially less than that of silicon and silicon being present to at least 1%.
9. A cylinder of an internal combustion engine formed from an alloy containing copper in the amount of from 87 to 90%, silicon, and aluminum in the amount of from two to four times the amount of the silicon and not less than 2% of the whole.
In testimony whereof, I hereunto aflix my signature.
ALADAR PACZ.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US385597A US1510242A (en) | 1920-06-01 | 1920-06-01 | Alloy and apparatus made therefrom |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US385597A US1510242A (en) | 1920-06-01 | 1920-06-01 | Alloy and apparatus made therefrom |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1510242A true US1510242A (en) | 1924-09-30 |
Family
ID=23522081
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US385597A Expired - Lifetime US1510242A (en) | 1920-06-01 | 1920-06-01 | Alloy and apparatus made therefrom |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1510242A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040226636A1 (en) * | 2001-09-06 | 2004-11-18 | Bampton Clifford Charles | Oxidation resistant and burn resistant copper metal matrix composites |
-
1920
- 1920-06-01 US US385597A patent/US1510242A/en not_active Expired - Lifetime
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20040226636A1 (en) * | 2001-09-06 | 2004-11-18 | Bampton Clifford Charles | Oxidation resistant and burn resistant copper metal matrix composites |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2210593A (en) | Bearing alloy | |
| US1947121A (en) | Aluminum base alloys | |
| US2802733A (en) | Process for manufacturing brass and bronze alloys containing lead | |
| US1510242A (en) | Alloy and apparatus made therefrom | |
| US2075090A (en) | Aluminum alloy | |
| US2289449A (en) | Die steel for hot working | |
| US2111278A (en) | Ferrous alloy | |
| US1545094A (en) | Steel alloy | |
| US2956846A (en) | Aluminum piston with aluminum alloy ring carrier | |
| US2238399A (en) | Bearing alloy | |
| US1759477A (en) | Alloy of high surface stability comprising nickel and silicon | |
| US2201405A (en) | Piston | |
| US2214652A (en) | Iron alloy | |
| US2075990A (en) | Cast iron | |
| US2026571A (en) | Free cutting alloys | |
| US2240202A (en) | Copper alloy | |
| US2181947A (en) | Method of making thin walled plated pistons for internal combustion engines | |
| US2400566A (en) | Alloy | |
| US1762109A (en) | Cast-iron alloy | |
| US2131076A (en) | Aluminum alloy and process for making the same, piston and piston ring formed from said alloy | |
| US2026569A (en) | Free cutting alloys | |
| US1562043A (en) | Iron-boron alloy | |
| US3167424A (en) | Alloy for valve seat insert castings | |
| US2035392A (en) | Copper steel alloys | |
| US2179695A (en) | Ferrous alloy |