US2679079A - Method of forming axle bearings - Google Patents

Method of forming axle bearings Download PDF

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US2679079A
US2679079A US775917A US77591747A US2679079A US 2679079 A US2679079 A US 2679079A US 775917 A US775917 A US 775917A US 77591747 A US77591747 A US 77591747A US 2679079 A US2679079 A US 2679079A
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metal
bearing
liner
mandrel
lining
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Lee J Lyons
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B22CASTING; POWDER METALLURGY
    • B22DCASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
    • B22D19/00Casting in, on, or around objects which form part of the product
    • B22D19/08Casting in, on, or around objects which form part of the product for building-up linings or coverings, e.g. of anti-frictional metal
    • B22D19/085Casting in, on, or around objects which form part of the product for building-up linings or coverings, e.g. of anti-frictional metal of anti-frictional metal
    • YGENERAL 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
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T29/00Metal working
    • Y10T29/49Method of mechanical manufacture
    • Y10T29/49636Process for making bearing or component thereof
    • Y10T29/49705Coating or casting

Definitions

  • This invention relates particularly to railway car and locomotive axlev journal bearings, which have a copper alloy back and are lined on the journal side with a softer metal lining of tin or lead base.
  • Such bearings are usually known as A. A. R. standard and are used under practically all freight cars and most passenger cars.
  • the present invention improves the physical characteristics of all such lined bearings made in segments of 180 or less and lined statically as distinguished from bushing type or centrifugally lined bearings.
  • bearings of this kind have usually been poured about a hollow iron mandrel, and sometimes cooled by spraying or lling the inside of the mandrel with water, or by leaving the top and bottom of the mandrel open Aand allowing the mandrel to be air cooled by natural air circulation.
  • the molten lining metal is cooled from the bearing face of the liner inwardly of the metal, thus first solidifying the face of the liner against the mandrel, and as solidication continues inwardly of the metal, the molten metal is pulled away from the copper alloy back and the solder bond previously applied to the solid back. It is Well known in the casting art that when a molten.
  • the main object of the vinvention is to produce a new and improved bearing with a stronger solder bond between the back and the lining and to increase the strength of the soft lining metal adjacent and adhering to the bonding metal; more specically stated, the invention is directed to a method and a bearing wherein the yield point or strength ofthe solder bond and lining metal adjacent and adhering ⁇ thereto is increased so that the soft lining metal will have much greater resistance to the tendency to crack or come loose from the bearing back under severe pounding to which railway carbearings are subjected.
  • the present invention proposes, by means of apparatus covered by the parent application mentioned above, to reverse the direction of progressive solidiiication tendency heretofore present in the formation of axle bearings by applying drastic chilling effect simultaneously over substantially the entire outside surface of the solid back immediately upon pouring the molten lining metal.
  • the quick application of a substantial quantity of liquid coolant to the bearing back insures the solidification of the solder bond and the lining metal adjacent thereto while the lining metal 1/8" to 1A" away is still liquid and there is still a body of molten metal above to feed the shrinkage.
  • FIG. 1 is a top View of a pouring bench showing two mandrels which form parts of molds by which the liner is formed, there being a bearing and a holding device therefor associated with one of the mandrels.
  • Figure 2 is a front view of the structure shown in Figure l.
  • Figure 3 is a detail vertical transverse section taken on the line 3 3 of Figure 2.
  • Figure 4 is a detail view ⁇ of a restricted portion of the holding member and is taken on the line t--t of Figure l.
  • Figure 5 illustrates a small section of the' present A.
  • A. R. standard bearing greatly enlarged (as by a photomicrograph).
  • Figure 6 is a view similar to Figure 5 and illustrates a corresponding section of a bearing contemplated by the present invention.
  • the bench or base a may be of any suitable material and extent and adapted to support one or more circular or semi-circular mandrels 2 each having its axis disposed vertically and having a lower ange 3.
  • the mandrel will be firmly secured to the base.
  • a holding member 4 comprises an elongated arm pivoted on a bracket 5 to swing in a vertical plane from the full line position shown in Figures 1 and 2 to the broken line position shown in Figure 2. In each of these positions, the outer end of the arm will be supported and positioned transversely of the bench by a suitable holding jaw t.
  • member 4 is threaded transversely to receive a clamping screw 'I having a handle il at one end by which it may be rotated in mem ber 4 to feed its inner end 9 against the back of an ordinary journal bearing body ill, the concave face of which is substantially concentric with the surface of the adjacent mandrel 2.
  • the side edges i! of the bearing back will seat against suitable ribs i2 on mandrel 2, and preferably ribs I2 will be shouldered at I3 to Droperly posiiton the bearing transversely of the mandrel.
  • holding member l is hollow and forms a conduit lll leading from a supply pipe I5 to a series of discharge outlets IB abreast of and facing towards bearing back It.
  • this portion of member 4 is enlarged to substantially cover the entire outer face of bearing back lll, as best shown at I? in Figure Ll. Cooling liquid is supplied through pipe I5, cutofi valve I8 and adjusting valve le and is discharged through outlets IB against the outer face of bearing back IB. simultaneously spraying the entire outer face of the back.
  • the bearing back l0 Before being applied to the mandrel, the bearing back l0 has a liquid flux applied to its concave surface and is then immersed in a kettle of molten solder (heated to approximately 600 F.) and allowed to come up to that temperature which is well above the melting temperature of the solder (approximately 370 FJ. The bearing back is then quickly placed against the mandrel and. the clamping screw I tightened to thrust the bearing back edges Ii against the mandrel lips I2.
  • the space between the arcuate portions of the mandrel and the bearing back forms a mold for the liner metal 2l which is poured promptly after the application of the bearing back to the mandrel, the liner metal and the thin coating 22 of solder uniting to form a bond between the liner 2l and the bearing back.
  • valve I8 is opened and water or other cooling liquid is discharged against the rear face of the bearing back Ill, which is cooled rapidly, thus quickly solidifying the solder bond 22 and the portion of the liner metal 2i adiav cent to the bearing back Il) while a substantial portion of the remaining lining metal 2l is still molten.
  • the metal will be most dense and consequently stronger where it is cooled quickly and less dense where it cools slowly. Any shrinkage occurring during the latter portion of the cooling operation will be along the surface which is closer to the mandrel and not along the surface which is ad jacent to the solder bond and bearing back. Hence the bond between the bearing back and the liner will be stronger than if the liner metal were cooled from the mandrel towards the bearing back and there will be less likelihood of minute shrinkage cavities o1' spongy metal between the bearing back and the liner, which weakens the metal and facilitates loosening of the liner from the bearing back after the iinished bearing is put in service and the liner is subject to thrusts and impacts under heavy loads.
  • Figures 5 and 6 of the drawings illustrate the difference in physical characteristics of bearings produced by methods used heretofore and the method of the present invention.
  • Figure 5 illustrating a bearing with liner cast in the usual manner, the metal 2
  • the bonding alloy which is chemically similar to the lining metal, is drawn away from the bearing back and diused into the lining metal, as illustrated at 2E, thus weakening bond 22 and the adjacent lining metal by forming a spongy, weak structure with large voids, as illustrated at 2d, adjacent to the bearing back.
  • clamping screw l Promptly upon completion of the pouring and solidification of the liner metal, clamping screw l is released and holding member fl is swung to bring the clamping screw opposite to the right hand mandrel 2 and another bearing is applied to mandrel 2 and the pouring operation duplicated.
  • mandrels By using the mandrels alternately, their temperature may be held below a point where cooling and hardening oi the liner would be impeded. Also, this alternate use of the mandreis will provide for leaving the cooling liner in a position long enough to permit it to harden so that it may be handled without deformation of its journal-engaging surface 23.
  • the discharge portion VI of the conduit is placed closer to the bottom oi the mandrel than to the top so that cooling and solidiication begins at the lower end of the bearing ( Figure 3) and proceeds upwardly, particularly in view of the fact that the metal is poured from the top, and the lower portion of the liner metal will be cooling while the upper portion is still being poured into the mold.
  • there is always a supply of molten metal just above the point of solidiiication which moves upwardly as the molten metal flows into the mold, and the last point of solidication is at the upper end oi the bearing.
  • bearing backs of the type under consideration are usually formed of copper alloys having a high degree of conductivity, the conduction of heat from the soldered surface of the liner metal will be readily eiected when the outer face of the bearing is cooled by the discharge of cooling liquid from the conduit.
  • the diierential between the rate of cooling or the liner metal at the bearing back and at the mandrei may be increased by using a closed mandrel or by applying heat to the inner face of the mandrel by a gas burner 26 or other suitable means.- Prcierably the temperature of the mandrel is maintained below the solidication temperature of the liner metal.

Description

May 25, 1954` A L. J. I YoNs 2,679,079 v METHOD oF FORMING AxLE BEARINGS Filed Oct. 24, 1947 wv. 34.-. :3; LUM nl."
N INVENTOR:
LE EJ.I YoNs ATTORNEY.
Patented May 25, 1954 UNITED STATES PATENT OFFICE METHOD F FOR-MING AXLE BEARINGS Lee J. Lyons, Webster Groves, Mo.
Application September 24, 1947, Serial No. 775,917
1 Claim.
This invention relates particularly to railway car and locomotive axlev journal bearings, which have a copper alloy back and are lined on the journal side with a softer metal lining of tin or lead base. Such bearings are usually known as A. A. R. standard and are used under practically all freight cars and most passenger cars. The present invention improves the physical characteristics of all such lined bearings made in segments of 180 or less and lined statically as distinguished from bushing type or centrifugally lined bearings.
The present application is a continuation-inpart of a copending application, Serial No. 523,512, led February 23, 1944, now Patent 2,437,107, patented March 2, 1948, by the present inventor.
Heretofore, bearings of this kind have usually been poured about a hollow iron mandrel, and sometimes cooled by spraying or lling the inside of the mandrel with water, or by leaving the top and bottom of the mandrel open Aand allowing the mandrel to be air cooled by natural air circulation. vIn all the above methods, the molten lining metal is cooled from the bearing face of the liner inwardly of the metal, thus first solidifying the face of the liner against the mandrel, and as solidication continues inwardly of the metal, the molten metal is pulled away from the copper alloy back and the solder bond previously applied to the solid back. It is Well known in the casting art that when a molten. body of metal is cooled from two or more sides, the inside portion or the portion last solidifying is softer or weaker than the remainder of the metal which is more quickly chilled and solidiiied. When shrinkage pull is excessive, it results in holes or internal voids, but even a slight internalY shrinkage pull causes a microscopic spongy effect with decided reduction in strength of the metal.
The main object of the vinvention is to produce a new and improved bearing with a stronger solder bond between the back and the lining and to increase the strength of the soft lining metal adjacent and adhering to the bonding metal; more specically stated, the invention is directed to a method and a bearing wherein the yield point or strength ofthe solder bond and lining metal adjacent and adhering` thereto is increased so that the soft lining metal will have much greater resistance to the tendency to crack or come loose from the bearing back under severe pounding to which railway carbearings are subjected.
The present invention proposes, by means of apparatus covered by the parent application mentioned above, to reverse the direction of progressive solidiiication tendency heretofore present in the formation of axle bearings by applying drastic chilling effect simultaneously over substantially the entire outside surface of the solid back immediately upon pouring the molten lining metal. The quick application of a substantial quantity of liquid coolant to the bearing back insures the solidification of the solder bond and the lining metal adjacent thereto while the lining metal 1/8" to 1A" away is still liquid and there is still a body of molten metal above to feed the shrinkage. While this invention is concerned principally with strengthening the solder bond .001 or .002 thick, and the adjacent g1g to 31g" of lining metal, physical tests have shown that the wearing surface 1/4 to fig from the bond in the new bearing is also decidedly hardened and strengthened.
These advantages and other detail objects of the invention are attained by following the method described below and by the resulting product, reference being had to the accompanying drawings, in which- Figure 1 is a top View of a pouring bench showing two mandrels which form parts of molds by which the liner is formed, there being a bearing and a holding device therefor associated with one of the mandrels.
Figure 2 is a front view of the structure shown in Figure l.
Figure 3 is a detail vertical transverse section taken on the line 3 3 of Figure 2.
Figure 4 is a detail view` of a restricted portion of the holding member and is taken on the line t--t of Figure l.
Figure 5 illustrates a small section of the' present A. A. R. standard bearing, greatly enlarged (as by a photomicrograph).
Figure 6 is a view similar to Figure 5 and illustrates a corresponding section of a bearing contemplated by the present invention.
The bench or base a may be of any suitable material and extent and adapted to support one or more circular or semi-circular mandrels 2 each having its axis disposed vertically and having a lower ange 3. The mandrel will be firmly secured to the base. A holding member 4 comprises an elongated arm pivoted on a bracket 5 to swing in a vertical plane from the full line position shown in Figures 1 and 2 to the broken line position shown in Figure 2. In each of these positions, the outer end of the arm will be supported and positioned transversely of the bench by a suitable holding jaw t. intermediate the ends of member 4, it is threaded transversely to receive a clamping screw 'I having a handle il at one end by which it may be rotated in mem ber 4 to feed its inner end 9 against the back of an ordinary journal bearing body ill, the concave face of which is substantially concentric with the surface of the adjacent mandrel 2. The side edges i! of the bearing back will seat against suitable ribs i2 on mandrel 2, and preferably ribs I2 will be shouldered at I3 to Droperly posiiton the bearing transversely of the mandrel.
A substantial portion of holding member l is hollow and forms a conduit lll leading from a supply pipe I5 to a series of discharge outlets IB abreast of and facing towards bearing back It. Preferably, this portion of member 4 is enlarged to substantially cover the entire outer face of bearing back lll, as best shown at I? in Figure Ll. Cooling liquid is supplied through pipe I5, cutofi valve I8 and adjusting valve le and is discharged through outlets IB against the outer face of bearing back IB. simultaneously spraying the entire outer face of the back.
Before being applied to the mandrel, the bearing back l0 has a liquid flux applied to its concave surface and is then immersed in a kettle of molten solder (heated to approximately 600 F.) and allowed to come up to that temperature which is well above the melting temperature of the solder (approximately 370 FJ. The bearing back is then quickly placed against the mandrel and. the clamping screw I tightened to thrust the bearing back edges Ii against the mandrel lips I2. The space between the arcuate portions of the mandrel and the bearing back forms a mold for the liner metal 2l which is poured promptly after the application of the bearing back to the mandrel, the liner metal and the thin coating 22 of solder uniting to form a bond between the liner 2l and the bearing back.
During or immediately following the pouring of the liner metal, valve I8 is opened and water or other cooling liquid is discharged against the rear face of the bearing back Ill, which is cooled rapidly, thus quickly solidifying the solder bond 22 and the portion of the liner metal 2i adiav cent to the bearing back Il) while a substantial portion of the remaining lining metal 2l is still molten.
As is well understood in the casting art, the metal will be most dense and consequently stronger where it is cooled quickly and less dense where it cools slowly. Any shrinkage occurring during the latter portion of the cooling operation will be along the surface which is closer to the mandrel and not along the surface which is ad jacent to the solder bond and bearing back. Hence the bond between the bearing back and the liner will be stronger than if the liner metal were cooled from the mandrel towards the bearing back and there will be less likelihood of minute shrinkage cavities o1' spongy metal between the bearing back and the liner, which weakens the metal and facilitates loosening of the liner from the bearing back after the iinished bearing is put in service and the liner is subject to thrusts and impacts under heavy loads.
Figures 5 and 6 of the drawings illustrate the difference in physical characteristics of bearings produced by methods used heretofore and the method of the present invention. In Figure 5, illustrating a bearing with liner cast in the usual manner, the metal 2| adjacent the mandrel will freeze before the metal adjacent back It freezes and the bonding alloy 22 and lining metal 2| adjacent thereto will remain liquid for to 10t` seconds. During this time, the bonding alloy, which is chemically similar to the lining metal, is drawn away from the bearing back and diused into the lining metal, as illustrated at 2E, thus weakening bond 22 and the adjacent lining metal by forming a spongy, weak structure with large voids, as illustrated at 2d, adjacent to the bearing back.
In Figure 6, illustrating a bearing cast according to the present disclosure the bonding alloy 22 and adjacent lining metal 2l is solidied within 5 to 8 seconds after the lining metal is poured. The quick solidication of the bonding alloy solder 2 2 retains the solder against the solid bearing back lil and the quick solidification of the adjacent lining metal 2l and the rapid solidiiication of the remaining lining metal forms a close, uniformly grained, strong dense structure of the lining metal throughout its thickness.
These statements are not merely theories but have been demonstrated by photo-micrographs oi sections through A. A. R. standard bearings and bearings made according to the present invention and Figures 5 and 6 are intended to illustrate the grain structure shown in such photomicrographs.
Promptly upon completion of the pouring and solidification of the liner metal, clamping screw l is released and holding member fl is swung to bring the clamping screw opposite to the right hand mandrel 2 and another bearing is applied to mandrel 2 and the pouring operation duplicated. By using the mandrels alternately, their temperature may be held below a point where cooling and hardening oi the liner would be impeded. Also, this alternate use of the mandreis will provide for leaving the cooling liner in a position long enough to permit it to harden so that it may be handled without deformation of its journal-engaging surface 23.
To avoid cooling of the liner metal at the tcp of the bearing before the metal cools at the center oi the bearing (and thus causing the liner metal to shrink and pull away from the bearing back at its center), the discharge portion VI of the conduit is placed closer to the bottom oi the mandrel than to the top so that cooling and solidiication begins at the lower end of the bearing (Figure 3) and proceeds upwardly, particularly in view of the fact that the metal is poured from the top, and the lower portion of the liner metal will be cooling while the upper portion is still being poured into the mold. Thus there is always a supply of molten metal just above the point of solidiiication which moves upwardly as the molten metal flows into the mold, and the last point of solidication is at the upper end oi the bearing.
Since bearing backs of the type under consideration are usually formed of copper alloys having a high degree of conductivity, the conduction of heat from the soldered surface of the liner metal will be readily eiected when the outer face of the bearing is cooled by the discharge of cooling liquid from the conduit. Obviously the diierential between the rate of cooling or the liner metal at the bearing back and at the mandrei may be increased by using a closed mandrel or by applying heat to the inner face of the mandrel by a gas burner 26 or other suitable means.- Prcierably the temperature of the mandrel is maintained below the solidication temperature of the liner metal.
It will be understood that other liquids may be used in place of the water for cooling the outer face of the bearing back and that other details may be varied without departing from the spirit of the invention, and the exclusive use of those modications coming within the scope of the cla-im is` contemplated.
What is claimed is:
The method of applying a metallic lead-base liner of 1/8 inch or greater thickness to the face of a railway axle journal bea-ring baci; of conper-base metal and having a concave arcuate contour in cross section in a manner to pre-- Vent development of voids in the line-r by ecntrolling the density thereof, which comprises anplying a liquid flux to the inner face of the back, immersing the back in bath of molten solder having a temperature approximately 600 F. and far below they melting temperature of the back to form a, layer of solder on. the inner face of the bac-k, maintaining the back in immersion until it has attained the temperature of the bath, then immediately placing the back with said face in concentric relation to a convex mold member so that a mold cavity is created between the solder-clad inner face of the back and the mold member, and heating the moid member without exceeding the freezing' temperature of the liner metal, lling the mold cavity so created with molted liner metal at a temperature far below the melting tempera-ture or" the back, continuing to apply heat to the mold member to maintain its temperature near but below the freezing temperature of the liner metal, and simultaneously with the pouring of the molten liner metal applying cooling means to the outer face of the back to: cool the back to a relatively low ternperature for effecting a marked differential rate* of freezing of the liner metal whereby the portion thereof against the back is rapidly solidified, together with the solder, in advance of the freezing ci the portion of the liner metal adjacent the heated mold member, and thereby produce a liner with maximum deneity adjacent the back and with less density where spaced from the back.
References Cited in the file of this patent UNITED STATES PATENTS Number Name Date 730,828 Woodman June 9, 1903 777,507 Hewitt Dec. 13, 1904 1,180,728 Klocke Apr. 25, 1916 1,258,702 Pearman Mar. 12, 1918 1,321,478 Russler Nov. l1, 1919 1,399,252 Eggenweiler Dec. 6, 1921 1,529,034 Page Mar. 10, 1925 2,058,621 Pike Oct. 27, 1986 2,108,590 Boegehold et al Jan. 25, 1938 2,107,978 Croucher Feb. S, 1938 2,127,937 Pike Aug. 23, 1938 2,245,578 Enderich et al June 17, 1941 2,248,693 Bartscherer July 8, 1941 2,364,503 Zink Dec. 5, 1944 FOREIGN APATENTS Number Country Date 577,685 Great Britain May 28, 1946 884,498 France Apr. 27, 1943
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Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2842818A (en) * 1954-08-23 1958-07-15 Meredith Publishing Company Apparatus for pressure casting of printing plates
US3485290A (en) * 1966-09-14 1969-12-23 United Aircraft Corp Method of making a rocket nozzle
US3500526A (en) * 1967-01-03 1970-03-17 Vertical Seal Co Production of large bearings
US4117580A (en) * 1975-04-07 1978-10-03 Friedrich Heck Manufacture of bearings

Citations (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US730328A (en) * 1902-05-26 1903-06-09 August J Weil Journal-bearing.
US777507A (en) * 1904-01-18 1904-12-13 James E Hewitt Car-axle bearing.
US1180728A (en) * 1915-05-08 1916-04-25 Pressed Bearing Company Method of making lined bearings.
US1258702A (en) * 1915-02-08 1918-03-12 Ervin J Hanson Babbitting-jig.
US1321478A (en) * 1919-11-11 of new castle
US1399252A (en) * 1920-04-15 1921-12-06 Gen Aluminum & Brass Mfg Compa Method of lining bearing-backs
US1529034A (en) * 1919-10-10 1925-03-10 Gen Motors Corp Method of forming bearings from cast metal
US2058621A (en) * 1934-02-05 1936-10-27 Kalif Corp Making bearings
US2106590A (en) * 1935-04-29 1938-01-25 Gen Motors Corp Bearing and method
US2107978A (en) * 1935-08-02 1938-02-08 Croucher Harry James Sainsbury Jig for use in metaling bearings
US2127937A (en) * 1935-04-17 1938-08-23 Kalif Corp Making bearings
US2246578A (en) * 1939-02-24 1941-06-24 Salardi Albert Bernhard De Trussed structural member and method of and means for its manufacture
US2248693A (en) * 1937-04-02 1941-07-08 Bartscherer Franz Method for producing hollow bodies in centrifugal casting molds rotatable about the vertical axis
FR884498A (en) * 1940-09-02 1943-08-18 Kloeckner Humboldt Deutz Ag Method and apparatus for lining bearings and other cylindrical members with anti-friction metals
US2364503A (en) * 1939-05-17 1944-12-05 Gen Motors Corp Bearing and method of making same
GB577685A (en) * 1944-05-10 1946-05-28 Robert Douglas Cheyne Method of and apparatus for production of lined bearing members

Patent Citations (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1321478A (en) * 1919-11-11 of new castle
US730328A (en) * 1902-05-26 1903-06-09 August J Weil Journal-bearing.
US777507A (en) * 1904-01-18 1904-12-13 James E Hewitt Car-axle bearing.
US1258702A (en) * 1915-02-08 1918-03-12 Ervin J Hanson Babbitting-jig.
US1180728A (en) * 1915-05-08 1916-04-25 Pressed Bearing Company Method of making lined bearings.
US1529034A (en) * 1919-10-10 1925-03-10 Gen Motors Corp Method of forming bearings from cast metal
US1399252A (en) * 1920-04-15 1921-12-06 Gen Aluminum & Brass Mfg Compa Method of lining bearing-backs
US2058621A (en) * 1934-02-05 1936-10-27 Kalif Corp Making bearings
US2127937A (en) * 1935-04-17 1938-08-23 Kalif Corp Making bearings
US2106590A (en) * 1935-04-29 1938-01-25 Gen Motors Corp Bearing and method
US2107978A (en) * 1935-08-02 1938-02-08 Croucher Harry James Sainsbury Jig for use in metaling bearings
US2248693A (en) * 1937-04-02 1941-07-08 Bartscherer Franz Method for producing hollow bodies in centrifugal casting molds rotatable about the vertical axis
US2246578A (en) * 1939-02-24 1941-06-24 Salardi Albert Bernhard De Trussed structural member and method of and means for its manufacture
US2364503A (en) * 1939-05-17 1944-12-05 Gen Motors Corp Bearing and method of making same
FR884498A (en) * 1940-09-02 1943-08-18 Kloeckner Humboldt Deutz Ag Method and apparatus for lining bearings and other cylindrical members with anti-friction metals
GB577685A (en) * 1944-05-10 1946-05-28 Robert Douglas Cheyne Method of and apparatus for production of lined bearing members

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2842818A (en) * 1954-08-23 1958-07-15 Meredith Publishing Company Apparatus for pressure casting of printing plates
US3485290A (en) * 1966-09-14 1969-12-23 United Aircraft Corp Method of making a rocket nozzle
US3500526A (en) * 1967-01-03 1970-03-17 Vertical Seal Co Production of large bearings
US4117580A (en) * 1975-04-07 1978-10-03 Friedrich Heck Manufacture of bearings

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