US2754202A - Aluminum base bearing - Google Patents
Aluminum base bearing Download PDFInfo
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- US2754202A US2754202A US346780A US34678053A US2754202A US 2754202 A US2754202 A US 2754202A US 346780 A US346780 A US 346780A US 34678053 A US34678053 A US 34678053A US 2754202 A US2754202 A US 2754202A
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- bearing
- chromium
- silicon
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- 229910052782 aluminium Inorganic materials 0.000 title claims description 25
- XAGFODPZIPBFFR-UHFFFAOYSA-N aluminium Chemical compound [Al] XAGFODPZIPBFFR-UHFFFAOYSA-N 0.000 title claims description 25
- VYZAMTAEIAYCRO-UHFFFAOYSA-N Chromium Chemical compound [Cr] VYZAMTAEIAYCRO-UHFFFAOYSA-N 0.000 claims description 24
- 229910052804 chromium Inorganic materials 0.000 claims description 24
- 239000011651 chromium Substances 0.000 claims description 24
- 229910052710 silicon Inorganic materials 0.000 claims description 24
- 239000010703 silicon Substances 0.000 claims description 24
- ATJFFYVFTNAWJD-UHFFFAOYSA-N Tin Chemical compound [Sn] ATJFFYVFTNAWJD-UHFFFAOYSA-N 0.000 claims description 17
- 239000000956 alloy Substances 0.000 description 69
- 229910045601 alloy Inorganic materials 0.000 description 69
- 239000011133 lead Substances 0.000 description 26
- XUIMIQQOPSSXEZ-UHFFFAOYSA-N Silicon Chemical compound [Si] XUIMIQQOPSSXEZ-UHFFFAOYSA-N 0.000 description 23
- 235000010210 aluminium Nutrition 0.000 description 23
- 239000011135 tin Substances 0.000 description 16
- 239000000463 material Substances 0.000 description 7
- 229910052751 metal Inorganic materials 0.000 description 7
- 239000002184 metal Substances 0.000 description 7
- XEEYBQQBJWHFJM-UHFFFAOYSA-N Iron Chemical compound [Fe] XEEYBQQBJWHFJM-UHFFFAOYSA-N 0.000 description 6
- 239000001996 bearing alloy Substances 0.000 description 6
- 238000005260 corrosion Methods 0.000 description 5
- 230000007797 corrosion Effects 0.000 description 5
- 239000000470 constituent Substances 0.000 description 4
- 238000000034 method Methods 0.000 description 4
- 239000000203 mixture Substances 0.000 description 4
- 239000002253 acid Substances 0.000 description 3
- 238000005275 alloying Methods 0.000 description 3
- 238000005266 casting Methods 0.000 description 3
- 239000012535 impurity Substances 0.000 description 3
- 229910052742 iron Inorganic materials 0.000 description 3
- LQBJWKCYZGMFEV-UHFFFAOYSA-N lead tin Chemical compound [Sn].[Pb] LQBJWKCYZGMFEV-UHFFFAOYSA-N 0.000 description 3
- 239000010687 lubricating oil Substances 0.000 description 3
- 238000005096 rolling process Methods 0.000 description 3
- 229910000838 Al alloy Inorganic materials 0.000 description 2
- CWYNVVGOOAEACU-UHFFFAOYSA-N Fe2+ Chemical compound [Fe+2] CWYNVVGOOAEACU-UHFFFAOYSA-N 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 2
- 150000007513 acids Chemical class 0.000 description 2
- 229910052797 bismuth Inorganic materials 0.000 description 2
- JCXGWMGPZLAOME-UHFFFAOYSA-N bismuth atom Chemical compound [Bi] JCXGWMGPZLAOME-UHFFFAOYSA-N 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 2
- 238000005336 cracking Methods 0.000 description 2
- 238000010438 heat treatment Methods 0.000 description 2
- 239000000155 melt Substances 0.000 description 2
- 238000001556 precipitation Methods 0.000 description 2
- 239000007787 solid Substances 0.000 description 2
- 239000010959 steel Substances 0.000 description 2
- 230000008016 vaporization Effects 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 229910000906 Bronze Inorganic materials 0.000 description 1
- OKTJSMMVPCPJKN-UHFFFAOYSA-N Carbon Chemical compound [C] OKTJSMMVPCPJKN-UHFFFAOYSA-N 0.000 description 1
- 229910000846 In alloy Inorganic materials 0.000 description 1
- 240000007594 Oryza sativa Species 0.000 description 1
- 235000007164 Oryza sativa Nutrition 0.000 description 1
- 229910001128 Sn alloy Inorganic materials 0.000 description 1
- 230000009286 beneficial effect Effects 0.000 description 1
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000010974 bronze Substances 0.000 description 1
- 230000001627 detrimental effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 239000000374 eutectic mixture Substances 0.000 description 1
- 230000006870 function Effects 0.000 description 1
- 229910002804 graphite Inorganic materials 0.000 description 1
- 239000010439 graphite Substances 0.000 description 1
- 230000005484 gravity Effects 0.000 description 1
- 239000007788 liquid Substances 0.000 description 1
- 238000004519 manufacturing process Methods 0.000 description 1
- 230000008018 melting Effects 0.000 description 1
- 238000002844 melting Methods 0.000 description 1
- 150000002736 metal compounds Chemical class 0.000 description 1
- 150000002739 metals Chemical class 0.000 description 1
- 238000012856 packing Methods 0.000 description 1
- 238000010791 quenching Methods 0.000 description 1
- 230000000171 quenching effect Effects 0.000 description 1
- 235000009566 rice Nutrition 0.000 description 1
- 238000005204 segregation Methods 0.000 description 1
- 238000009834 vaporization 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
- C22C21/00—Alloys based on aluminium
- C22C21/02—Alloys based on aluminium with silicon as the next major constituent
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/12—Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing
- F16C33/121—Use of special materials
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12701—Pb-base component
-
- 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
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/12—All metal or with adjacent metals
- Y10T428/12493—Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
- Y10T428/12736—Al-base component
Definitions
- This invention relates to bearings and particularly to an improved aluminum base alloy which is especially suitable for use as a bearing material in the as-cast condition.
- Aluminum and most of its alloys are generally quite unsuitable for use in bearings for ferrous metal machine parts because the aluminum tends to adhere to, or combine with, the ferrous metal, thereby causing scoring or seizing. I have found, however, that by suitable combination of alloying constituents, this difficulty can be overcome and a bearing alloy produced having not only anti friction properties but other characteristics especially suitable in a bearing material.
- a principal object of the present invention is to provide an inexpensive aluminum base bearing alloy which has excellent corrosion resistance, as well as satisfactory hardness and high score resistance.
- a further object of this invention is to provide a corrosionresistant aluminum base alloy which not only has desirable frictional properties when used as a bearing, but which also may be used either as a cast alloy or a wrought alloy.
- an aluminum base alloy containing minor proportions of silicon, lead, chromium and tin.
- an alloy of this composition is a stronger metal than the aluminum alloys generally heretofore used for bearing purposes, solid bearings may be formed from it and no packing of steel or similar metals is necessary.
- a bearing formed from my alloy may be advantageously provided with a thin overlay of lead or a' lead base alloy. Examples of these overlays include the lead-tin and lead-indium alloys which are used for this purpose and in which lead is the major constituent.
- the alloy formed in accordance with the present invention is characterized by greater corrosion resistance, increased hardness and a correspondingly longer fatigue life than related aluminum base alloys heretofore used.
- solid bearings made from this alloy retain their original shapes better than many of the bearings which up to the present time have been formed of softer alloys.
- the former do not take a set at temperatures to which they are normally -subjected,.'and they undergo a negligible amount of shrinkage after extensive use type of inexpensive bearing a loy is found to 2,754,202 Patented July 10, 1956 be particularly valuable for low speed applications where it may be used in the as-cast condition. Hence it may be satisfactorily employed as a cast bell end bearing in fractional horsepower motors.
- the silicon content is not used near its upper limit, the alloy can be easily rolled down by conventional methods and used as a Wrought alloy.
- an alloy comprising, by weight, approximately 0.2% to 10% silicon, 0.1% to 3% lead, 0.1% to 0.6% chromium, 0.01% to 0.3% tin, and the balance substantially all aluminum.
- incidental impurities may be included in this alloy in the usual small amounts without any substantial detrimental effects.
- aluminum as used herein, embraces the usual impurities which are found in aluminum ingots of commercial grade or which are introduced during the handling operations incident to ordinary melting practice.
- iron which together with silicon is found in commercial aluminum, may be present in amounts not greater than approximately 0.5% without causing any harmful results.
- an alloy should be used which consists essentially of approximately 2% to 5% silicon, 0.5% to 1.5% lead, 0.2% to 0.35% chromium, 0.05% to 0.15% tin, and the balance substantially all aluminum.
- alloys having the above compositions show excellent anti-friction properties so that bearings formed of this alloy do not score or gall when in contact with a rotating steel shaft, and neither the shaft nor the bearing show an appreciable amount of Wear after long and severe use. I have also found that the resistance of this alloy to cracking or crumbling is extraordinarily high.
- silicon in my aluminum base bearing alloy improves its frictional properties and also increases its strength.
- the alloy in order to obtain a high degree of score resistance and adequate strength, it is necessary that the alloy have a silicon content of at least 0.2%, and for best results it is desirable to use at least 2% silicon. More than approximately 10% silicon should not be included in the alloy, however, because of casting difficulties; and the resultant bearing is too brittle for practical applications if the silicon content is excessive. Inasmuch as a high silicon content also interferes with rolling processes, the maximum amount of silicon to be added necessarily is governed by the method to be used in forming the bearing or other article.
- silicon may be added in amounts as high as 10% in the cast alloy, it should not be present in amounts greater than about 5%, and preferably not in excess of 4%, in the wrought alloy because such an alloy needs to be rolled. Furthermore, while an increased silicon content improves score resistance, the addition of silicon in amounts greater than 5% provides only slight additional beneficial prop erties in this respect. Accordingly, best results are obtained for most purposes when the silicon content is kept Within the preferred range of approximately 2% to 5%.
- the lead performs the important function of conferring desirable frictional properties to the alloy.
- the alloy In order to obtain these properties to a satisfactory extent, it is necessary that the alloy have a minimum lead content of at least 0.1%; and at least 05% lead should be present for optimum score resistance, particularly if bismuth is omitted from the alloy.
- the lead should not be included in amounts above 3%, however, because a lead content greater than this amount results in segregation of. the lead with localized areas having poor frictional properties.
- the presence of lead has very little effect on the ductility of the aluminum base alloy. Hence an alloy containing about 0.1% to 1.5% lead can readily be rolled into a thin strip using conventional methods for rolling an aluminum alloy. It is generally preferred that the lead content not be raised above 1.5 however, if the alloy is to be used in the Wrought form.
- the amount of tin present should range from approximately to 15% of the lead. Therefore, a tin content between about 0.01% to 0.3% of the total weight of the alloy is satisfactory for increasing the corrosion resistance of the lead, while the preferred tin content is between 0.05% and 0.15%.
- the lead and tin combine to a certain extent into a lead-tin alloy which is formed principally at the grain boundaries.
- the as-cast metal may be heat treated, if desired, to place the leadtin alloy in aspheroidal form; If the final aluminum base alloy is to be used as a Wrought alloy to form a hearing, it is particularly important that the tin content does not exceed approximately 0.3% inasmuch as greater amounts of tin make the alloy too brittle. Hence, in order that the material may be properly rolled, the tin content should not exceed the aforementioned maximum amount.
- chromium greatly contributes to the hardness and machinability of the resultant alloy. While the hardness may be substantially reduced if the chromium content is too low, the addition of approximately 0.3% chromium is all that is necessary in order to obtain a completely satisfactory degree of hardness. Moreover, a chromium content of only 0.2% chromium increases the hardness of the alloy considerably and makes it suitable for many bearing applications.
- chromium in amounts greater than about 0.6%, however, reduces the ductility of the resultant alloy to too great an extent, a high ductility being particularly necessary if the material is to be used as a wrought alloy. It is also not feasible to add more than 0.6% chromium because increasing the chromium content above this amount raises alloy costs by greatly increasing the difi'iculty in casting and fabrication of the cast parts. Too high a temperature is required to place and hold greater quantities of chromium in solution in the liquid state, the chromium segregating out unless the temperature of the melt is raised excessively. The resultant formation ofhard spots in the alloy prevents the obtaining of a uniform casting.
- a chromium content below 0.1% is insufiicient to confer the necessary hardness and strength to the alloy. Furthermore, the score resistance of the alloy is slightly improved as the chromium content is increased. As' a result of the above considerations, I have found that a chromium content within the preferred range of approximately 0.2% to 0.35% provides excellent results in all respects. 7
- An example of the above alloy which possesses the aforementioned desirable characteristics to an outstanding degree, therefore, is one consisting of 4% silicon, 1.5% lead, 0.3% chromium, 0.15% tin, and the balance all aluminum and incidental impurities.
- the alloy In order to obtain the high degree of resistance to pounding, such as is encountered in a bearing, it is preferable that the alloy have a physical structure typified by the absence of continuous networks of relatively brittle eutectic mixtures. Unlike many of the aluminum base bearing alloys heretofore used, alloying the above composition does not involve problems due to vaporizing of any of the constituents, and close controls" are not required because all' of the elements used have relatively low vapor pressures. The temperature of the men may be raised as high as approximately 1600 F. before difficulty is encountered because of vaporization of lead, the element in the present alloy having the highest vapor pressure.
- Simple, conventional alloying procedures may be employed in the" present instance, therefore", with intermediate alloys, "such as 'alumiriun'zi s'ilieon' and aluminumctaomiam alloys, being usedto introduce the silicon 4 and chromium.
- the lead may then be added to the melt, which is subsequently stirred and cast, usually in metal or graphite molds.
- the alloy may be either cast in the desired form for use in bearings or, if bismuth is not added, it may be cast in ingots, rolled down to strip material of the desired thickness, and bearing elements formed from the stock.
- Cast articles having a metallo'graphic structure showing acontinuous network of segregated metal compounds may be improved as to strength and fatigue resistance by suitable heat treatment.
- suitable heat treatment For example, I have found that a solution treatment at atemperature between approximately 900 F. and 1050 F. for a period of eight to fifteen hours is particularly effective.
- Upon removing the alloy from the furnace following the solution treatment it is preferable to cool it immediately by quenching in water. This treatment provides the alloy with the high degree of ductility, such as is desirable for rolling operations; and it may then be easily rolled down to strip material of the desired thickness.
- a precipitation treatment may thereafter be employed to substantially increase the hardness of the alloy. This process is preferably carried out by heating the article for five to ten hours at a temperature in the range between approximately 300 F. and 400 F., a precipitation treatment at 370 F. for eight hours being particularly satisfactory. The alloy then may be again cooled, preferably in water, and suitably machined. Such a heat treating process results in an article which is three or four times as hard as it was in the as-cast condition and whose fatigue strength is proportionally improved.
- the specific gravity of the above-described alloy is about one-third that of a tin-bronze bearing alloy, and has muchgreater resistance to fatigue or to cracking under the pounding-action to which many types of bearin'gs are subjected. This property renders such an alloy suitable as abearing for use under extreme conditions, tests onsuch bearings indicating the relative absence of wear, either of the bearing of the shaft. In addition, the alloy appears to be resistant to corrosion by acid con stituents of lubricating oils which attack many other bearing compositions.
- A-bearing formed of an alloy consisting essentially of approximately 0.2% to 10% silicon, 0.1% to 3% lead, 0.1% to 0.6% chromium, 0.01% to'0.3'% tin, and the balance substantially all aluminum;
- a bearing as in claim 2 in which a surface thereof is provided with a thin overlay of a metal of a class consisting of lead and lead base alloys.
- a bearing characterized by high anti-friction .properties and resistance to disintegration under impact and to attack by acids;developed in lubricating oils; said hearing being formed of an alloy consisting essentially of 2% to 5% silicon, 0.5% to 1.5% lead, 0.2% to 0.35% chromium, 0. 5%" to 0.15% tin, iron not in excess of 0.5%, and the balance substantially all aluminum.
- a bearing formed from an alloy capable of being rolled into sheet form from cast ingots and having high anti-friction properties and fatigue resistance; said alloy consisting" essefiasuypr 2% to.5% silicon, 0.5% 191.5% le d, 012% 156' 0.35% chromium, i0105%-to 0.15% tin, and the ,ba rice 6'.
- a hearing refinedtrain a 1165i rename wrou ht alloy consisting of approximately 0.2% to 4% silicon, 0.1% to 3% lead, 0.1% to 0.35% chromium, 0.01% to 0.3% tin, iron not in excess of 0.5%, and the balance substantially all aluminum.
Description
AL 1 BASE BEARING No Drawing. Application April 3, 1953, Serial No. 346,780
6 Claims. (Cl. 75148) This invention relates to bearings and particularly to an improved aluminum base alloy which is especially suitable for use as a bearing material in the as-cast condition.
Aluminum and most of its alloys are generally quite unsuitable for use in bearings for ferrous metal machine parts because the aluminum tends to adhere to, or combine with, the ferrous metal, thereby causing scoring or seizing. I have found, however, that by suitable combination of alloying constituents, this difficulty can be overcome and a bearing alloy produced having not only anti friction properties but other characteristics especially suitable in a bearing material.
Many aluminum base alloys, such as the type disclosed in my co-pending patent application S. N. 328,265, filed December 27, 1952, are satisfactory bearing materials in most respects. However, many of these alloys do not possess sutficient resistance to corrosion to enable them to be satisfactorily used for many purposes, and bearings formed from such alloys have relatively short lives because of the tendency to corrode in the presence of the acids which are formed in lubricating oils during use.
- Accordingly, a principal object of the present invention is to provide an inexpensive aluminum base bearing alloy which has excellent corrosion resistance, as well as satisfactory hardness and high score resistance. A further object of this invention is to provide a corrosionresistant aluminum base alloy which not only has desirable frictional properties when used as a bearing, but which also may be used either as a cast alloy or a wrought alloy.
In accordance with my invention, therefore, the foregoing and other objects and advantages are attained to a particularly high degree in an aluminum base alloy containing minor proportions of silicon, lead, chromium and tin. Inasmuch as an alloy of this composition is a stronger metal than the aluminum alloys generally heretofore used for bearing purposes, solid bearings may be formed from it and no packing of steel or similar metals is necessary. If desired, a bearing formed from my alloy may be advantageously provided with a thin overlay of lead or a' lead base alloy. Examples of these overlays include the lead-tin and lead-indium alloys which are used for this purpose and in which lead is the major constituent.
The alloy formed in accordance with the present invention is characterized by greater corrosion resistance, increased hardness and a correspondingly longer fatigue life than related aluminum base alloys heretofore used. As a result of this hardness, solid bearings made from this alloy retain their original shapes better than many of the bearings which up to the present time have been formed of softer alloys. The former do not take a set at temperatures to which they are normally -subjected,.'and they undergo a negligible amount of shrinkage after extensive use type of inexpensive bearing a loy is found to 2,754,202 Patented July 10, 1956 be particularly valuable for low speed applications where it may be used in the as-cast condition. Hence it may be satisfactorily employed as a cast bell end bearing in fractional horsepower motors. Furthermore, if the silicon content is not used near its upper limit, the alloy can be easily rolled down by conventional methods and used as a Wrought alloy.
Accordingly, I have found that satisfactory bearing properties are obtained with an alloy comprising, by weight, approximately 0.2% to 10% silicon, 0.1% to 3% lead, 0.1% to 0.6% chromium, 0.01% to 0.3% tin, and the balance substantially all aluminum. Various incidental impurities may be included in this alloy in the usual small amounts without any substantial detrimental effects. Thus the term aluminum, as used herein, embraces the usual impurities which are found in aluminum ingots of commercial grade or which are introduced during the handling operations incident to ordinary melting practice. For example, iron, which together with silicon is found in commercial aluminum, may be present in amounts not greater than approximately 0.5% without causing any harmful results. For optimum results I have found that an alloy should be used which consists essentially of approximately 2% to 5% silicon, 0.5% to 1.5% lead, 0.2% to 0.35% chromium, 0.05% to 0.15% tin, and the balance substantially all aluminum.
Under severe test conditions, alloys having the above compositions show excellent anti-friction properties so that bearings formed of this alloy do not score or gall when in contact with a rotating steel shaft, and neither the shaft nor the bearing show an appreciable amount of Wear after long and severe use. I have also found that the resistance of this alloy to cracking or crumbling is extraordinarily high.
The inclusion of silicon in my aluminum base bearing alloy improves its frictional properties and also increases its strength. Hence, in order to obtain a high degree of score resistance and adequate strength, it is necessary that the alloy have a silicon content of at least 0.2%, and for best results it is desirable to use at least 2% silicon. More than approximately 10% silicon should not be included in the alloy, however, because of casting difficulties; and the resultant bearing is too brittle for practical applications if the silicon content is excessive. Inasmuch as a high silicon content also interferes with rolling processes, the maximum amount of silicon to be added necessarily is governed by the method to be used in forming the bearing or other article. Accordingly, although silicon may be added in amounts as high as 10% in the cast alloy, it should not be present in amounts greater than about 5%, and preferably not in excess of 4%, in the wrought alloy because such an alloy needs to be rolled. Furthermore, while an increased silicon content improves score resistance, the addition of silicon in amounts greater than 5% provides only slight additional beneficial prop erties in this respect. Accordingly, best results are obtained for most purposes when the silicon content is kept Within the preferred range of approximately 2% to 5%.
In the present aluminum base bearing alloy, the lead performs the important function of conferring desirable frictional properties to the alloy. In order to obtain these properties to a satisfactory extent, it is necessary that the alloy have a minimum lead content of at least 0.1%; and at least 05% lead should be present for optimum score resistance, particularly if bismuth is omitted from the alloy. The lead should not be included in amounts above 3%, however, because a lead content greater than this amount results in segregation of. the lead with localized areas having poor frictional properties. It should also be noted that the presence of lead has very little effect on the ductility of the aluminum base alloy. Hence an alloy containing about 0.1% to 1.5% lead can readily be rolled into a thin strip using conventional methods for rolling an aluminum alloy. It is generally preferred that the lead content not be raised above 1.5 however, if the alloy is to be used in the Wrought form.
For best results,- the amount of tin present should range from approximately to 15% of the lead. Therefore, a tin content between about 0.01% to 0.3% of the total weight of the alloy is satisfactory for increasing the corrosion resistance of the lead, while the preferred tin content is between 0.05% and 0.15%. The lead and tin combine to a certain extent into a lead-tin alloy which is formed principally at the grain boundaries. Of course, the as-cast metal may be heat treated, if desired, to place the leadtin alloy in aspheroidal form; If the final aluminum base alloy is to be used as a Wrought alloy to form a hearing, it is particularly important that the tin content does not exceed approximately 0.3% inasmuch as greater amounts of tin make the alloy too brittle. Hence, in order that the material may be properly rolled, the tin content should not exceed the aforementioned maximum amount.
The presence of chromium greatly contributes to the hardness and machinability of the resultant alloy. While the hardness may be substantially reduced if the chromium content is too low, the addition of approximately 0.3% chromium is all that is necessary in order to obtain a completely satisfactory degree of hardness. Moreover, a chromium content of only 0.2% chromium increases the hardness of the alloy considerably and makes it suitable for many bearing applications.
The addition of chromium in amounts greater than about 0.6%, however, reduces the ductility of the resultant alloy to too great an extent, a high ductility being particularly necessary if the material is to be used as a wrought alloy. It is also not feasible to add more than 0.6% chromium because increasing the chromium content above this amount raises alloy costs by greatly increasing the difi'iculty in casting and fabrication of the cast parts. Too high a temperature is required to place and hold greater quantities of chromium in solution in the liquid state, the chromium segregating out unless the temperature of the melt is raised excessively. The resultant formation ofhard spots in the alloy prevents the obtaining of a uniform casting. A chromium content below 0.1%, on the other hand, is insufiicient to confer the necessary hardness and strength to the alloy. Furthermore, the score resistance of the alloy is slightly improved as the chromium content is increased. As' a result of the above considerations, I have found that a chromium content within the preferred range of approximately 0.2% to 0.35% provides excellent results in all respects. 7
An example of the above alloy which possesses the aforementioned desirable characteristics to an outstanding degree, therefore, is one consisting of 4% silicon, 1.5% lead, 0.3% chromium, 0.15% tin, and the balance all aluminum and incidental impurities.
In order to obtain the high degree of resistance to pounding, such as is encountered in a bearing, it is preferable that the alloy have a physical structure typified by the absence of continuous networks of relatively brittle eutectic mixtures. Unlike many of the aluminum base bearing alloys heretofore used, alloying the above composition does not involve problems due to vaporizing of any of the constituents, and close controls" are not required because all' of the elements used have relatively low vapor pressures. The temperature of the men may be raised as high as approximately 1600 F. before difficulty is encountered because of vaporization of lead, the element in the present alloy having the highest vapor pressure. Simple, conventional alloying procedures may be employed in the" present instance, therefore", with intermediate alloys, "such as 'alumiriun'zi s'ilieon' and aluminumctaomiam alloys, being usedto introduce the silicon 4 and chromium. The lead may then be added to the melt, which is subsequently stirred and cast, usually in metal or graphite molds. The alloy may be either cast in the desired form for use in bearings or, if bismuth is not added, it may be cast in ingots, rolled down to strip material of the desired thickness, and bearing elements formed from the stock.
Cast articles having a metallo'graphic structure showing acontinuous network of segregated metal compounds may be improved as to strength and fatigue resistance by suitable heat treatment. For example, I have found that a solution treatment at atemperature between approximately 900 F. and 1050 F. for a period of eight to fifteen hours is particularly effective. Upon removing the alloy from the furnace following the solution treatment, it is preferable to cool it immediately by quenching in water. This treatment provides the alloy with the high degree of ductility, such as is desirable for rolling operations; and it may then be easily rolled down to strip material of the desired thickness.
A precipitation treatment may thereafter be employed to substantially increase the hardness of the alloy. This process is preferably carried out by heating the article for five to ten hours at a temperature in the range between approximately 300 F. and 400 F., a precipitation treatment at 370 F. for eight hours being particularly satisfactory. The alloy then may be again cooled, preferably in water, and suitably machined. Such a heat treating process results in an article which is three or four times as hard as it was in the as-cast condition and whose fatigue strength is proportionally improved.
The specific gravity of the above-described alloy is about one-third that of a tin-bronze bearing alloy, and has muchgreater resistance to fatigue or to cracking under the pounding-action to which many types of bearin'gs are subjected. This property renders such an alloy suitable as abearing for use under extreme conditions, tests onsuch bearings indicating the relative absence of wear, either of the bearing of the shaft. In addition, the alloy appears to be resistant to corrosion by acid con stituents of lubricating oils which attack many other bearing compositions.
It is to be understood that, while the invention has been described bymeans of certain s'pecific'exa'mples, the scope of the invention is not to be limited thereby except as defined in the following'claims.
I claim:
1. A-bearing formed of an alloy consisting essentially of approximately 0.2% to 10% silicon, 0.1% to 3% lead, 0.1% to 0.6% chromium, 0.01% to'0.3'% tin, and the balance substantially all aluminum;
2. A bearing formed of an alloy capable of being rolled into sheet form from east ingots and having high antifriction properties and fatigueresistance, said alloy con sisting essenfally of approximately 2% to' 5% silicon, 0.5% to 1.5 leadf, 0.2% to 0.35% chromium, 0.05% to 0.15% tin, and the balance substantially all alu minum. A
3. A bearing as in claim 2 in which a surface thereof is provided with a thin overlay of a metal of a class consisting of lead and lead base alloys.
4. A bearing characterized by high anti-friction .properties and resistance to disintegration under impact and to attack by acids;developed in lubricating oils; said hearing being formed of an alloy consisting essentially of 2% to 5% silicon, 0.5% to 1.5% lead, 0.2% to 0.35% chromium, 0. 5%" to 0.15% tin, iron not in excess of 0.5%, and the balance substantially all aluminum.
5. A bearing formed from an alloy capable of being rolled into sheet form from cast ingots and having high anti-friction properties and fatigue resistance; said alloy consisting" essefiasuypr 2% to.5% silicon, 0.5% 191.5% le d, 012% 156' 0.35% chromium, i0105%-to 0.15% tin, and the ,ba rice 6'. A hearing refinedtrain a 1165i rename wrou ht alloy consisting of approximately 0.2% to 4% silicon, 0.1% to 3% lead, 0.1% to 0.35% chromium, 0.01% to 0.3% tin, iron not in excess of 0.5%, and the balance substantially all aluminum.
References Cited in the file of this patent UNITED STATES PATENTS Kempf et a1. Apr. 13, 1937 Vaders Sept. 17, 1940 Murray July 27, 1943 Hunsicker June 14, 1949 FOREIGN PATENTS Great Britain Oct. 2, 1919 Great Britain May 18, 1945
Claims (1)
1. A BEARING FORMED OF AN ALLOY CONSISTING ESSENTIALLY OF APPROXIMATELY 0.2% TO 10% SILICON, 0.1% TO 3% LEAD, 0.1% TO 0.6% CHROMIUM, 0.01% TO 0.3% TIN, AND THE BALANCE SUBSTANTIALLY ALL ALUMINUM.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US346780A US2754202A (en) | 1953-04-03 | 1953-04-03 | Aluminum base bearing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US346780A US2754202A (en) | 1953-04-03 | 1953-04-03 | Aluminum base bearing |
Publications (1)
Publication Number | Publication Date |
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US2754202A true US2754202A (en) | 1956-07-10 |
Family
ID=23361023
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US346780A Expired - Lifetime US2754202A (en) | 1953-04-03 | 1953-04-03 | Aluminum base bearing |
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US (1) | US2754202A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2845825A (en) * | 1955-08-18 | 1958-08-05 | Bernice L Bessinger | Bit dressing device |
US4792430A (en) * | 1987-07-24 | 1988-12-20 | Aluminum Company Of America | Aluminum anode alloy |
US4865651A (en) * | 1987-07-24 | 1989-09-12 | Aluminum Company Of America | Method of making an aluminum base alloy anode |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
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GB132984A (en) * | 1900-01-01 | |||
US2062329A (en) * | 1932-04-21 | 1936-12-01 | Aluminum Co Of America | Thermal treatment of aluminum alloys containing copper |
US2076578A (en) * | 1935-12-28 | 1937-04-13 | Aluminum Co Of America | Free cutting alloys |
US2076571A (en) * | 1935-12-28 | 1937-04-13 | Aluminum Co Of America | Free cutting alloys |
US2215444A (en) * | 1937-12-15 | 1940-09-17 | Ver Deutsche Metallwerke Ag | Aluminum alloy as bearing metal |
US2325071A (en) * | 1940-11-30 | 1943-07-27 | Indium Corp America | Bearing and like article |
GB569337A (en) * | 1940-11-09 | 1945-05-18 | Horace Campbell Hall | Bearings |
US2473060A (en) * | 1945-11-14 | 1949-06-14 | Aluminum Co Of America | Bearing alloys |
-
1953
- 1953-04-03 US US346780A patent/US2754202A/en not_active Expired - Lifetime
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB132984A (en) * | 1900-01-01 | |||
US2062329A (en) * | 1932-04-21 | 1936-12-01 | Aluminum Co Of America | Thermal treatment of aluminum alloys containing copper |
US2076578A (en) * | 1935-12-28 | 1937-04-13 | Aluminum Co Of America | Free cutting alloys |
US2076571A (en) * | 1935-12-28 | 1937-04-13 | Aluminum Co Of America | Free cutting alloys |
US2215444A (en) * | 1937-12-15 | 1940-09-17 | Ver Deutsche Metallwerke Ag | Aluminum alloy as bearing metal |
GB569337A (en) * | 1940-11-09 | 1945-05-18 | Horace Campbell Hall | Bearings |
US2325071A (en) * | 1940-11-30 | 1943-07-27 | Indium Corp America | Bearing and like article |
US2473060A (en) * | 1945-11-14 | 1949-06-14 | Aluminum Co Of America | Bearing alloys |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2845825A (en) * | 1955-08-18 | 1958-08-05 | Bernice L Bessinger | Bit dressing device |
US4792430A (en) * | 1987-07-24 | 1988-12-20 | Aluminum Company Of America | Aluminum anode alloy |
US4865651A (en) * | 1987-07-24 | 1989-09-12 | Aluminum Company Of America | Method of making an aluminum base alloy anode |
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