US3729347A - High-strength,centrifugally cast copper-base alloy bearing cage - Google Patents
High-strength,centrifugally cast copper-base alloy bearing cage Download PDFInfo
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- US3729347A US3729347A US00097193A US3729347DA US3729347A US 3729347 A US3729347 A US 3729347A US 00097193 A US00097193 A US 00097193A US 3729347D A US3729347D A US 3729347DA US 3729347 A US3729347 A US 3729347A
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- strength
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- bearing cage
- centrifugally cast
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- 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
- F16C33/30—Parts of ball or roller bearings
- F16C33/38—Ball cages
- F16C33/44—Selection of substances
-
- 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
- C22C9/04—Alloys based on copper with zinc 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
- F16C33/30—Parts of ball or roller bearings
- F16C33/38—Ball cages
- F16C33/3837—Massive or moulded cages having cage pockets surrounding the balls, e.g. machined window cages
- F16C33/3843—Massive or moulded cages having cage pockets surrounding the balls, e.g. machined window cages formed as one-piece cages, i.e. monoblock cages
- F16C33/385—Massive or moulded cages having cage pockets surrounding the balls, e.g. machined window cages formed as one-piece cages, i.e. monoblock cages made from metal, e.g. cast or machined window cages
-
- 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
- F16C2204/00—Metallic materials; Alloys
- F16C2204/10—Alloys based on copper
- F16C2204/14—Alloys based on copper with zinc 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
- F16C2220/00—Shaping
- F16C2220/02—Shaping by casting
-
- 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
- Y10T428/12361—All metal or with adjacent metals having aperture or cut
Definitions
- ABSTRACT OF THE DISCLOSURE Alloys consisting essentially of from about 26.0 to about 34.0% zinc, from about 4.5 to about 10.0% (preferably from about 4.5 to about 6.0%) manganese, from about 0.5 to about 1.5% iron, from about 1.0 to about 2.5 aluminum, and the balance copper. Lead can be optionally added, in amount of from about 0.5 to about 1.5%.
- the alloys have improved physical properties, particularly at elevated temperatures, and can be centrif ugally cast for manufacture in antifriction bearing cages.
- Alcop was developed in the 1930s to combat a rash of bearing cage failures which occurred at that time, when it was conventional to manufacture the cages from red brass containing 85% copper, 5% tin, 5% lead, and 5% zinc.
- Alcop was very successful in overcoming the problems of the day, and over the years became a very popular material for antifriction bearing cages. As minimum physical properties, Alcop has a yield tensile strength of 25,000 p.s.i., an ultimate tensile strength of 65,000 p.s.i., a Rockwell hardness of 55 on the b scale, and 25% elongation in a 2" gauge length.
- a main object of the invention is the fulfillment of this need.
- the centrifugal casting of the cylinders is a delicate operation.
- Each cylinder is cast in a permanent, cylindrical, mold or die which is disposed with its longitudinal axis in horizontal or vertical orientation and which is rotated at high speeds around the axis while molten metal is introduced into one end of the die.
- the die size and speed of rotation, desired cylinder wall thickness, G- forces on the molten metal, and other factors, all must be carefully interrelated to successfully produce sound castings.
- Alcop was so successful is that it lent itself well to this process. Attempts to change the chemistryof Alcop encountered difiiculties in the cylinder casting procedure. The cast cylinders tended to be unsound because of cracks formed during the centrifugal casting process.
- Another object of the invention is the provision of improved and strengthened copper-base alloys and bearing cages which can be successfully centrifugally cast.
- Alloys in accordance with the invention consist essentially of from about 26.0 to about 34.0% zinc, from about 4.5 to about 10.0% (preferably from about 4.5% to about 6.0%) manganese, from about 0.5 to about 1.5% iron, from about 1.0 toabout 2.5% aluminum, and the balance copper.
- the alloys can also contain from about 0.5 to about 1.5% lead as an optional additive where increased machinability is desired.
- the phrase consisting essentially of embraces materials, e.g., impurities and diluents, which do not materially affect the basic properties of the composition. All composition percentages herein are by weight.
- Alloys in accordance with the invention are characterized by a minimum room-temperature yield tensile strength of about 32,000 p.s.i., an increase of about 28% over Alcop.
- the minimum room-temperature ultimate tensile strength is about 70,000 p.s.i., an increase of about 8% from Alcop.
- the minimum room temperature Rockwell b hardness is 75, up about 36% over Alcop. Fatigue strength is improved, as are stress-rupture properties. Ductility is good.
- the strength properties of the alloys can be still further improved by heat treatment.
- the allo'ys exhibit a martensitic type of structure after solution treating and quenching.
- the alloys can be cast into cylinders for manufacture of bearing cages in accordance with conventional procedures.
- the foregoing properties are very much sought after and highly desirable, but it is in respect to elevatedtemperature properties that outstanding results are obtained.
- the alloys have excellent strength and hardness stability, at elevated temperatures, and this is very important because many bearings are subject to such temperatures in service.
- the manganese content is important. Alloys having manganese contents below the range specified have insufficient strength. Further, alloys with the low manganese tend not to respond to heat treatment. Alloys containing more manganese than the preferred range of from about 4.5 to about 6.0% are difficult to centrifugally cast with success. Close control over the speed of rotaappended claims.
- the alloy of Example I has the following room-temperature properties: A Rockwell b hardness of 75; a yield tensile strength of 32,000 p.s.i.; an ultimate tensile strength of 70,000 p.s.i.; and 35% elongation in 2".
- the alloy can withstand over 6.8 million cycles of fluctuation between 40,000 and 4,000 p.s.i. axial tension.
- the fatigue life is over 4.1 million cycles of fluctuation between 25,000 and 2,500 p.s.i. tenslon.
- the alloy of Example I has a yield tensile strength of 30,200 p.s.i. and an ultimate tensile strength of 54,000 p.s.i.
- the alloy not only retains a Rockwell b hardness of 75 after 20.5 hours at 450 F., but also actually increases in hardness to 78.5 Rockwell b after 138.5 hours at 450 F.
- stress-rupture the alloy can withstand a stress of 29,000 p.s.i. at 450 F. for 100 hours. Such stress is about 96% of the yield strength at that temperature, and it is surprising that the alloy has such elevated-temperature strength.
- the alloy of Example II has the following properties: a Rockwell b hardness of 79; a yield tensile strength of 33,000 p.s.i.; an ultimate tensile strength of 80,000 p.s.i.; a fatigue strength of 39,000 p.s.i.; and 34% elongation in 2".
- the yield tensile strength is 32,000 p.s.i. and the ultimate tensile strength is 55,000 p.s.i.
- the alloy surprisingly can withstand 30,000 p.s.i. (94% of the yield strength) for 100 hours at 450 F.
- the alloy of Example III has a Rockwell b hardness of 85, a yield tensile strength of 52,000 p.s.i., an ultimate tensile strength of 95,000 p.s.i., and a fatigue strength of 30,000 p.s.i.
- the alloy has a yield tensile strength of 52,000 p.s.i. and an ultimate tensile strength of 68,000 p.s.i.
- the alloy can withstand 32,000 p.s.i. stress for 100 hours.
- a centrifugally cast antifriction bearing cage composed of an alloy consisting essentially of from about 26.0 to about 34.0% zinc, from about 4.5 to about 6.0% manganese, from about 0.5 to about 1.5% iron, from about 1.0 to about 2.5% aluminum, from about 0.5 to about 1.5 lead, and the balance copper.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Materials Engineering (AREA)
- Metallurgy (AREA)
- Organic Chemistry (AREA)
- Rolling Contact Bearings (AREA)
Abstract
ALLOYS CONSISTING ESSENTIALLY OF FROM ABOUT 26.0 TO ABOUT 34.0% ZINC, FROM ABOUT 4.5 TO ABOUT 10.0% (PREFERABLY FROM ABOUT 4.5 TO ABOUT 6.0%) MANGANESE, FROM ABOUT .0.5 TO ABOUT 1.5% IRON, FROM ABOUT 1.0 TO ABOUT 2.5 ALUMINUM, AND THE BALANCE COOPPR. LEAD CAN BE OPTIONALLY ADDED, IN AMOUNT OF FROM ABOUT 0.5 TO ABOUT 1.5%. THE ALLOYS HAVE IMPROVED PHYSICAL PROPERTIES, PARTICULARLY AT ELEVATED TEMPERATURES, AND CAN BE CENTRIFUGALLY CAST FOR MANUFACTURE INA NTIFRICTION BEARING CAGES.
Description
April 24, 1973 w. D. BROWN ETAL HIGH-STRENGTH,
CENTRIFUGALLY CAST COPPER-BASB ALLOY BEARING CAGE Filed Dec. 11, 1970 w S Ca H n R SM 0 A TNR N E EW O w W O MSR AAE UMN L M M WT G VI B ATTORNEYS United States Patent Office 3,729,347 Patented Apr. 24, 1973 ABSTRACT OF THE DISCLOSURE Alloys consisting essentially of from about 26.0 to about 34.0% zinc, from about 4.5 to about 10.0% (preferably from about 4.5 to about 6.0%) manganese, from about 0.5 to about 1.5% iron, from about 1.0 to about 2.5 aluminum, and the balance copper. Lead can be optionally added, in amount of from about 0.5 to about 1.5%. The alloys have improved physical properties, particularly at elevated temperatures, and can be centrif ugally cast for manufacture in antifriction bearing cages.
BACKGROUND OF THE INVENTION For decades, it has been the practice to manufacture cages for ball or roller bearings from an alloy known as Alcop. This alloy has a nominal composition of 63% copper, 35% zinc, 1% aluminum, and 1% lead.
Alcop was developed in the 1930s to combat a rash of bearing cage failures which occurred at that time, when it was conventional to manufacture the cages from red brass containing 85% copper, 5% tin, 5% lead, and 5% zinc.
Alcop was very successful in overcoming the problems of the day, and over the years became a very popular material for antifriction bearing cages. As minimum physical properties, Alcop has a yield tensile strength of 25,000 p.s.i., an ultimate tensile strength of 65,000 p.s.i., a Rockwell hardness of 55 on the b scale, and 25% elongation in a 2" gauge length.
As the years went by, however, bearing service applications became more severe and a need developed for bearing cage alloys having increased strength, particularly at high temperatures, and having extended service life. A main object of the invention is the fulfillment of this need.
There are a number of known expedients for strengthening copper-base alloys. However, attempts to apply such expedients to the strengthening of Alcop have encountered complicating factors. One of such factors appeared in the bearing cage manufacturing process.
In the manufacturing of bearing cages, one of which is generally indicated at in the drawing, it is common practice to first centrifugally cast a hollow cylinder and then cut transverse slices from the cylinder at closely spaced locations along the longitudinal axis of the cylinder to produce a plurality of rings, as 12. Each ring is then machined at spaced locations around its periphery to form apertures, as 14, which receive the individual balls or rollers of the bearing. There are many, many variants which can be practiced within the framework of this basic procedure, but the essentials of the process remain the same.
The centrifugal casting of the cylinders is a delicate operation. Each cylinder is cast in a permanent, cylindrical, mold or die which is disposed with its longitudinal axis in horizontal or vertical orientation and which is rotated at high speeds around the axis while molten metal is introduced into one end of the die. The die size and speed of rotation, desired cylinder wall thickness, G- forces on the molten metal, and other factors, all must be carefully interrelated to successfully produce sound castings. One of the reasons that Alcop was so successful is that it lent itself well to this process. Attempts to change the chemistryof Alcop encountered difiiculties in the cylinder casting procedure. The cast cylinders tended to be unsound because of cracks formed during the centrifugal casting process.
Accordingly, another object of the invention is the provision of improved and strengthened copper-base alloys and bearing cages which can be successfully centrifugally cast.
Other objects and advantages of the invention will appear to those skilled in the art from the following detailed description.
BRIEF DESCRIPTION OF THE DRAWINGS The sole figure, to which reference has already been made, is a perspective view of a bearing cage for a ball bearing.
DETAILED DESCRIPTION It has been found that copper-base alloys containing particular amounts of zinc, manganese, iron and aluminum have the necessary improved strength properties for hearing cages subjected to severe present-day service conditions, while being susceptible of successful centrifugal casting. The alloys have improved room-temperature yield tensile strength, ultimate tensile strength, fatigue strength, and hardness, and moreover, retain good ductility. Further, the allo'ys have surprising elevated-temperature properties, which are important because in present-day technology many bearings must operate successfully at elevated temperatures.
Alloys in accordance with the invention consist essentially of from about 26.0 to about 34.0% zinc, from about 4.5 to about 10.0% (preferably from about 4.5% to about 6.0%) manganese, from about 0.5 to about 1.5% iron, from about 1.0 toabout 2.5% aluminum, and the balance copper. The alloys can also contain from about 0.5 to about 1.5% lead as an optional additive where increased machinability is desired. As used herein, the phrase consisting essentially of embraces materials, e.g., impurities and diluents, which do not materially affect the basic properties of the composition. All composition percentages herein are by weight.
Alloys in accordance with the invention are characterized by a minimum room-temperature yield tensile strength of about 32,000 p.s.i., an increase of about 28% over Alcop. The minimum room-temperature ultimate tensile strength is about 70,000 p.s.i., an increase of about 8% from Alcop. The minimum room temperature Rockwell b hardness is 75, up about 36% over Alcop. Fatigue strength is improved, as are stress-rupture properties. Ductility is good. The strength properties of the alloys can be still further improved by heat treatment. The allo'ys exhibit a martensitic type of structure after solution treating and quenching. The alloys can be cast into cylinders for manufacture of bearing cages in accordance with conventional procedures.
The foregoing properties are very much sought after and highly desirable, but it is in respect to elevatedtemperature properties that outstanding results are obtained. The alloys have excellent strength and hardness stability, at elevated temperatures, and this is very important because many bearings are subject to such temperatures in service.
The manganese content is important. Alloys having manganese contents below the range specified have insufficient strength. Further, alloys with the low manganese tend not to respond to heat treatment. Alloys containing more manganese than the preferred range of from about 4.5 to about 6.0% are difficult to centrifugally cast with success. Close control over the speed of rotaappended claims.
Zn Mn Fe Al Pb Cu Exam lo:
The alloy of Example I has the following room-temperature properties: A Rockwell b hardness of 75; a yield tensile strength of 32,000 p.s.i.; an ultimate tensile strength of 70,000 p.s.i.; and 35% elongation in 2". In fatigue, the alloy can withstand over 6.8 million cycles of fluctuation between 40,000 and 4,000 p.s.i. axial tension. When notched, the fatigue life is over 4.1 million cycles of fluctuation between 25,000 and 2,500 p.s.i. tenslon.
At 450 F., the alloy of Example I has a yield tensile strength of 30,200 p.s.i. and an ultimate tensile strength of 54,000 p.s.i. The alloy not only retains a Rockwell b hardness of 75 after 20.5 hours at 450 F., but also actually increases in hardness to 78.5 Rockwell b after 138.5 hours at 450 F. In stress-rupture, the alloy can withstand a stress of 29,000 p.s.i. at 450 F. for 100 hours. Such stress is about 96% of the yield strength at that temperature, and it is surprising that the alloy has such elevated-temperature strength.
At room temperature, the alloy of Example II has the following properties: a Rockwell b hardness of 79; a yield tensile strength of 33,000 p.s.i.; an ultimate tensile strength of 80,000 p.s.i.; a fatigue strength of 39,000 p.s.i.; and 34% elongation in 2". At 450 F., the yield tensile strength is 32,000 p.s.i. and the ultimate tensile strength is 55,000 p.s.i. In stress-rupture, the alloy surprisingly can withstand 30,000 p.s.i. (94% of the yield strength) for 100 hours at 450 F.
At room temperature, the alloy of Example III has a Rockwell b hardness of 85, a yield tensile strength of 52,000 p.s.i., an ultimate tensile strength of 95,000 p.s.i., and a fatigue strength of 30,000 p.s.i. At 450 F., the alloy has a yield tensile strength of 52,000 p.s.i. and an ultimate tensile strength of 68,000 p.s.i. In stress-rupture, the alloy can withstand 32,000 p.s.i. stress for 100 hours.
We claim:
1. A centrifugally cast antifriction bearing cage composed of an alloy consisting essentially of from about 26.0 to about 34.0% zinc, from about 4.5 to about 6.0% manganese, from about 0.5 to about 1.5% iron, from about 1.0 to about 2.5% aluminum, from about 0.5 to about 1.5 lead, and the balance copper.
2. A centrifugally cast bearing cage as defined in claim 1, wherein the zinc is present in an amount of about 29%, the manganese is present in an amount of about 5.1%, the iron is present in an amount of about 0.7%, the aluminum is present in an amount of about 1.1%, the lead is present in an amount of about 0.6% and the copper is present in an amount of about 63.5%
3. A centrifugally cast bearing cage as defined in claim 1, wherein the zinc is present in an amount of about 29%, the manganese is present in an amount of about 4.7%, the iron is present in an amount of about 1.1%, the aluminum is present in an amount of about 2.0%, the lead is present in an amount of about 0.7 and the copper is present in an amount of about 62.5%
References Cited UNITED STATES PATENTS 1,625,777 4/1927 Kuchen 157.5 1,869,554 8/1932 Ellis 75157.5 3,097,093 7/1963 Fox et a1. 75-461 3,544,313 12/1970 Sadoshima et al. 75-1575 2,479,596 8/1949 Anderson et a1. 75-157.5
OTHER REFERENCES Metals Handbook, vol. 1, 8th ed., 1961, pages 972- 974, 1046 and 1047.
CHARLES N. LOVELL, Primary Examiner US. Cl. X.R.
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US9719370A | 1970-12-11 | 1970-12-11 |
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US3729347A true US3729347A (en) | 1973-04-24 |
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Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4909807A (en) * | 1987-11-04 | 1990-03-20 | Deutsche Automobilgesellschaft Mbh | Welding and backing ring arrangement for an electric cell |
US20040208407A1 (en) * | 2003-01-21 | 2004-10-21 | Ab Skf , Goteborg, Sweden. | Plain bearing bush |
WO2009135483A1 (en) * | 2008-05-08 | 2009-11-12 | Schaeffler Kg | Bearing module |
US20150292558A1 (en) * | 2012-11-08 | 2015-10-15 | Ntn Corporation | Cage for rolling bearing and rolling bearing |
-
1970
- 1970-12-11 US US00097193A patent/US3729347A/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4909807A (en) * | 1987-11-04 | 1990-03-20 | Deutsche Automobilgesellschaft Mbh | Welding and backing ring arrangement for an electric cell |
US20040208407A1 (en) * | 2003-01-21 | 2004-10-21 | Ab Skf , Goteborg, Sweden. | Plain bearing bush |
US7059774B2 (en) * | 2003-01-21 | 2006-06-13 | Ab Skf | Plain bearing bush |
WO2009135483A1 (en) * | 2008-05-08 | 2009-11-12 | Schaeffler Kg | Bearing module |
US20150292558A1 (en) * | 2012-11-08 | 2015-10-15 | Ntn Corporation | Cage for rolling bearing and rolling bearing |
US9416821B2 (en) * | 2012-11-08 | 2016-08-16 | Ntn Corporation | Cage for rolling bearing and rolling bearing |
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