US1832992A - Zinc alloy - Google Patents
Zinc alloy Download PDFInfo
- Publication number
- US1832992A US1832992A US379330A US37933029A US1832992A US 1832992 A US1832992 A US 1832992A US 379330 A US379330 A US 379330A US 37933029 A US37933029 A US 37933029A US 1832992 A US1832992 A US 1832992A
- Authority
- US
- United States
- Prior art keywords
- zinc
- alloy
- bearing
- zinc alloy
- metal
- 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
- 229910001297 Zn alloy Inorganic materials 0.000 title description 10
- HCHKCACWOHOZIP-UHFFFAOYSA-N Zinc Chemical compound [Zn] HCHKCACWOHOZIP-UHFFFAOYSA-N 0.000 description 18
- 229910052725 zinc Inorganic materials 0.000 description 18
- 239000011701 zinc Substances 0.000 description 18
- 229910052751 metal Inorganic materials 0.000 description 15
- 239000002184 metal Substances 0.000 description 15
- 238000012360 testing method Methods 0.000 description 11
- 229910045601 alloy Inorganic materials 0.000 description 7
- 239000000956 alloy Substances 0.000 description 7
- 229910052782 aluminium Inorganic materials 0.000 description 7
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 description 7
- 150000002739 metals Chemical class 0.000 description 6
- 229910001369 Brass Inorganic materials 0.000 description 4
- RYGMFSIKBFXOCR-UHFFFAOYSA-N Copper Chemical compound [Cu] RYGMFSIKBFXOCR-UHFFFAOYSA-N 0.000 description 4
- 239000010951 brass Substances 0.000 description 4
- 229910052802 copper Inorganic materials 0.000 description 4
- 239000010949 copper Substances 0.000 description 4
- 229910000906 Bronze Inorganic materials 0.000 description 3
- 239000010974 bronze Substances 0.000 description 3
- KUNSUQLRTQLHQQ-UHFFFAOYSA-N copper tin Chemical compound [Cu].[Sn] KUNSUQLRTQLHQQ-UHFFFAOYSA-N 0.000 description 3
- 238000002844 melting Methods 0.000 description 3
- 230000008018 melting Effects 0.000 description 3
- 229910000897 Babbitt (metal) Inorganic materials 0.000 description 2
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 2
- 238000004519 manufacturing process Methods 0.000 description 2
- PDYXSJSAMVACOH-UHFFFAOYSA-N [Cu].[Zn].[Sn] Chemical compound [Cu].[Zn].[Sn] PDYXSJSAMVACOH-UHFFFAOYSA-N 0.000 description 1
- 229910052793 cadmium Inorganic materials 0.000 description 1
- BDOSMKKIYDKNTQ-UHFFFAOYSA-N cadmium atom Chemical compound [Cd] BDOSMKKIYDKNTQ-UHFFFAOYSA-N 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000001816 cooling Methods 0.000 description 1
- 239000004615 ingredient Substances 0.000 description 1
- 229910052742 iron Inorganic materials 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 238000003754 machining Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 229910001092 metal group alloy Inorganic materials 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000012384 transportation and delivery Methods 0.000 description 1
- 238000005406 washing Methods 0.000 description 1
Classifications
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22C—ALLOYS
- C22C18/00—Alloys based on zinc
- C22C18/02—Alloys based on zinc with copper as the next major constituent
Definitions
- the general object of this invention is to provide a zinc alloy for use more particularly as bearing metal and which shall pos'ess properties which render it markedly superior,
- Th'e characteristics which distinguish my improved alloy from other alloys used in forming bearing metals are, low co-eiiicient of friction; small bearing temperature rise; great transverse strength; absence of material shrinkage in cooling; and satisfactory machining properties.
- I In producing the alloy, I first ⁇ provide a fixed metal by mixing together equal parts by weight of copper and zinc. This, in reality, forms a brass. I then take one ounce of this fixed metal or brass and combine with it fourteen ounces of zinc and one-half ounce of aluminum. The combined metals are, of course, melted together and the resultant product is a metal alloy about five times harder than zinc and having a melting point but slightly greater than that of zinc. For purposes of comparison, it may be stated that the melting point of brass composed of equal parts by weight of copper and zinc is v1175 F.; that of aluminum is 1217o F.; and
- the melting point of my alloy is from 815 to 820 F.
- my improved alloy is composed as follows:
- I may vary the quantity used relative to the other lngredients within a range extending from thirteen ounces to sixteen ounces; as stated, however, I prefer to use approximately fourteen ounces.
- Friction tests were conducted with bearing blocks machined from my improved alloy which were used in conjunction with a Riehle friction testing machine.
- the zinc alloy friction test was parallel with a similar test using copper-tin-zinc bronze blocks, all test conditions being equal except the bearing blocks.
- my zinc alloy blocks were run-in under full lubrication for eight hours at full-load.
- the test run consisted of an eight-hour run beginning with the bearing at room temperature. Readings of the bearing friction and temperature rise were taken at frequent intervals throughout the run. The readings showed the stabilized conditions of operation for the t'wo alloys to be as follows:
- a zinc alloy which consists in forming a fixed metal by combining equal parts by weight of copper and zinc, and then combining with a/given )o quantity of said xed metal aluminum and zinc theresultant allo having the metals combined in substantial y the following percentages by weight, namely: fixed metal, 614/31%; aluminum, 37/3l%; and zinc, 9am/31%.
Landscapes
- Chemical & Material Sciences (AREA)
- Engineering & Computer Science (AREA)
- Materials Engineering (AREA)
- Mechanical Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Sliding-Contact Bearings (AREA)
Description
Patented Nov. 24, 1931 UNITED sTATEs PATENT oFFicE HENRY J'. LORANG, OF ST. LOUIS, MISSOURI, 'ASSIGOIR 0F ONE-'HALE T0 FRANK J'. KUNL OF ST. LOUIS, MISSOURI ZINC ALLOY No Drawing.
The general object of this invention is to provide a zinc alloy for use more particularly as bearing metal and which shall pos'ess properties which render it markedly superior,
both from an economical and functional stand-point, to commercial bearing metals now on the market.
Th'e characteristics which distinguish my improved alloy from other alloys used in forming bearing metals are, low co-eiiicient of friction; small bearing temperature rise; great transverse strength; absence of material shrinkage in cooling; and satisfactory machining properties.
In producing the alloy, I first `provide a fixed metal by mixing together equal parts by weight of copper and zinc. This, in reality, forms a brass. I then take one ounce of this fixed metal or brass and combine with it fourteen ounces of zinc and one-half ounce of aluminum. The combined metals are, of course, melted together and the resultant product is a metal alloy about five times harder than zinc and having a melting point but slightly greater than that of zinc. For purposes of comparison, it may be stated that the melting point of brass composed of equal parts by weight of copper and zinc is v1175 F.; that of aluminum is 1217o F.; and
that of zinc. 786 F. The melting point of my alloy is from 815 to 820 F.
Stated in terms of percentages by weight, my improved alloy is composed as follows:
Brass (equal parts of copper and zinc), 6-14/31% Aluminum, 3-7/31% Zinz (prime western), 9010/31%.
The proportions of the metals named, I have found to give the most satisfactory results. However, the invention is not limited to these exact proportionsas, particularly in the case of zinc, the proportions named may be varied within reasonable limits without departing from the spirit of the invention and still produce a satisfactory bearing metal. Referring particularly to the zinc ingredient,
I may vary the quantity used relative to the other lngredients within a range extending from thirteen ounces to sixteen ounces; as stated, however, I prefer to use approximately fourteen ounces. l
Application mea July 1s,
Friction tests were conducted with bearing blocks machined from my improved alloy which were used in conjunction with a Riehle friction testing machine. The zinc alloy friction test was parallel with a similar test using copper-tin-zinc bronze blocks, all test conditions being equal except the bearing blocks. Previous to the test run, my zinc alloy blocks were run-in under full lubrication for eight hours at full-load. The test run consisted of an eight-hour run beginning with the bearing at room temperature. Readings of the bearing friction and temperature rise were taken at frequent intervals throughout the run. The readings showed the stabilized conditions of operation for the t'wo alloys to be as follows:
Zinc alloy Bronze Coecent of f1'cton....v .00221 .00184 Temperature rise of bearing F 32. 2 28.8
It will thus be seen that the friction characteristics of the zinc alloy used in this test approach those of a high-grade bearing bronze.
The above test was conducted at the laboratories of the Massachusetts Institute of Technology, Cambridge, Massachusetts.
Tests for transverse strength were conducted at the testing laboratory of .Washing possessed by my improved zinc alloy, I utilize a relatively low grade of zinc in its composition. Commercial deliveries of prime Western slab zinc analyze, -as to constituents, about as follows:
lOLepi, .5U-1.50; iron, .O1-.08; cadmium,
The use of this grade of zinc thus enables me to produce a verly high-grade bearin metal at a relatively ow cost, as compa with other bearing metals now on the market. j I claim:
1. The method of making a zinc alloy, which consists in forming a fixed metal by combining equal parts by weight of copper and zinc, and then combining with a/given )o quantity of said xed metal aluminum and zinc theresultant allo having the metals combined in substantial y the following percentages by weight, namely: fixed metal, 614/31%; aluminum, 37/3l%; and zinc, 9am/31%. Y
` 2. rl`he method of making a zinc alloy which consists in forming a. fixed metal by combining equal parts by weight of copperi y and zinc, and then combining sa/id xed metal With aluminum and zinc in substantially the proportions of one ounce ofthe fixed metal to fourteen ounces of zinc and one-half ounce s of aluminum. F Q In testimony whereof, I have hereunto set 2.', my hand.
HENRY J. LORANG.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US379330A US1832992A (en) | 1929-07-18 | 1929-07-18 | Zinc alloy |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US379330A US1832992A (en) | 1929-07-18 | 1929-07-18 | Zinc alloy |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1832992A true US1832992A (en) | 1931-11-24 |
Family
ID=23496800
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US379330A Expired - Lifetime US1832992A (en) | 1929-07-18 | 1929-07-18 | Zinc alloy |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1832992A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2927856A (en) * | 1952-03-31 | 1960-03-08 | Chemalloy Electronics Corp | Multi-purpose alloys of controlled homogeneity |
| US5945066A (en) * | 1997-11-20 | 1999-08-31 | Griffin; James D. | Zinc-copper based alloy and castings made therefrom |
-
1929
- 1929-07-18 US US379330A patent/US1832992A/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2927856A (en) * | 1952-03-31 | 1960-03-08 | Chemalloy Electronics Corp | Multi-purpose alloys of controlled homogeneity |
| US5945066A (en) * | 1997-11-20 | 1999-08-31 | Griffin; James D. | Zinc-copper based alloy and castings made therefrom |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2210593A (en) | Bearing alloy | |
| JPS61133357A (en) | Cu base alloy for bearing superior in workability and seizure resistance | |
| US1832992A (en) | Zinc alloy | |
| US2128954A (en) | Hot workable bronze | |
| JP2761181B2 (en) | Tin-based white metal bearing alloy with excellent heat and fatigue resistance | |
| US2306667A (en) | Alloy | |
| Lunn | The wear resistance of tin bronzes and related alloys | |
| US2238399A (en) | Bearing alloy | |
| US2270716A (en) | Copper alloy | |
| US1933390A (en) | Copper zinc silicon alloys | |
| US1988504A (en) | Cadmium base bearing metal | |
| JPS6086237A (en) | Cu-alloy for slide member | |
| US2102998A (en) | Liner for bearings | |
| US3833344A (en) | Friction material of the sintered bronze type | |
| US1874617A (en) | Non-ferrous alloy | |
| US2558523A (en) | Self-lubricating alloy | |
| US1932848A (en) | Aluminum alloys | |
| US1936397A (en) | Copper silicon manganese alloy | |
| US2185809A (en) | Alloy | |
| US2212017A (en) | Cuprous alloy | |
| US2597461A (en) | Lead base alloy | |
| US2076281A (en) | Aluminium alloy and article made therefrom | |
| US2137639A (en) | Light metal alloy | |
| US2043588A (en) | Cadmium-cobalt bearing alloy | |
| US1680577A (en) | Alloy |