US2130461A - Method of making bearings - Google Patents
Method of making bearings Download PDFInfo
- Publication number
- US2130461A US2130461A US360899A US36089929A US2130461A US 2130461 A US2130461 A US 2130461A US 360899 A US360899 A US 360899A US 36089929 A US36089929 A US 36089929A US 2130461 A US2130461 A US 2130461A
- Authority
- US
- United States
- Prior art keywords
- bronze
- bearing
- metals
- metal
- lining
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Lifetime
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Classifications
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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
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/06—Sliding surface mainly made of metal
- F16C33/14—Special methods of manufacture; Running-in
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B22—CASTING; POWDER METALLURGY
- B22D—CASTING OF METALS; CASTING OF OTHER SUBSTANCES BY THE SAME PROCESSES OR DEVICES
- B22D19/00—Casting in, on, or around objects which form part of the product
- B22D19/08—Casting in, on, or around objects which form part of the product for building-up linings or coverings, e.g. of anti-frictional metal
- B22D19/085—Casting 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
-
- 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
- F16C2223/00—Surface treatments; Hardening; Coating
- F16C2223/30—Coating surfaces
- F16C2223/44—Coating surfaces by casting molten material on the substrate
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49643—Rotary bearing
- Y10T29/49647—Plain bearing
- Y10T29/49668—Sleeve or bushing making
- Y10T29/49677—Sleeve or bushing making having liner
-
- 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49705—Coating or 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
- Y10T29/00—Metal working
- Y10T29/49—Method of mechanical manufacture
- Y10T29/49636—Process for making bearing or component thereof
- Y10T29/49709—Specific metallic composition
Definitions
- the object of my said invention is to provide a bearing and a method of making the same composed of metals which will provide a bearing of the necessary strength and rigidity and a bearing surface which will be of comparatively soft wearing quality but at the same time capable of resisting much higher temperature and withstanding much greater strain or "pounding" in servicefords the best foundation for a bearing such asrequired for the purpose indicated for the reason that it may be of lighter weight for the samedegree of strength than any other metal which I have found suitable for the purpose.
- so-called "plastic bronze” makes a most desirable metal for the lining or wearing surface for the bearing.
- plastic bronze I mean a compositioncomposed of copper and lead the proportions of which may be varied to suit difierent conditions and different requirements, a
- Plastic bronze is generally understood to also include, if desired, copper alloys of from 4% to 7% tin with 20% to 30% lead and with or without small quantities of nickel. It will be understood that in using the term "plastic bronze herein it is intended to include all such suitable compositions and variations thereof.
- the melting point of steel is considerably higher than the melting pointof the bronze but the melting point of bronze is very much higher than the melting point of babbitt and the bronze of a composition such as above indicated while afiording a most excellent surface for the bearings of high speed
- I employ a method by which the steel shell and the bronze lining or bearing surface are united by fusing the two metals to unite them by a bond that makes them practically integral and permanent so that separation under any strein,.load or flexing imposed'by the duty of the motor is impossible.
- Figure 1 illustrates a bearing such as contemplated by my invention, the bearing housing usually of aluminum or any other appropriate metal being indicated by the reference letter A, the steel shell by the reference letter B, and the bronze lining by the reference letter C.
- Figure 2 I illustrate a method the bearing which consists in mounting a cylinder D with. a bottom 12 within the shell B and pouring the molten bronze from a ladle E into the space between the cylinder and the inner .surface of the shell, It will be understood of l course that the ends of the bearing are me.- chined ofi' appropriately after the bearing is finished. The bottom d of the cylinder D is large enough to cover the end of the shell B as clearly indicated. c i
- the steelshell and lining metal may be heated together to a temperature where the lining metal will be a sub stantial degree above its melting point and the steel shell a substantial degree below its melting point or the parts may be heated separately to different temperatures so long as the steel shell is a substantial degree below its melting point and, the lining metal a substantial degree above its melting point.
- the two metals may be united or applied to each other in any manner found practicable, the particular method illustrated and described. being one that I have found suitable for the purpose.
- the steel back and the lining metal may be united in flat sheet form if desired and then rolled or otherwise shaped to form a bearin of the shape desired.
- the steel shell of appropriate thickness is heated to a temperature which is approximately the temperature required for melting the bronze metal which is to' be used to the steel of a temperature substantially the same as that of such bronze metal the two metals fuse and unite firmly together forming a bond that makes the two metals practically integral and incapable of separation regardless of strain, flexing or other duty imposedin use.
- the bronze metal After the bronze metal is poured or otherwise applied to the steel shell it is allowed to cool for a short period suflicient to allow the two metals to fuse together but before the lead in the composition of the bronze can settle and separate from the copper by reason of its greater gravity the bearing is immersed in a cold bath and cooled quickly so that the copper and lead content of the bronze composition are held in the metal properly mixed and of the same relative proportions throughout.
- the method of forming bearings which consists in heating a steel shell to approximately the melting point of the bronze lining metal, heating the bronze lining metal to a temperature higher than its melting point, depositing said lining metal while so heated upon the surface of the heated shell, permitting the two metals to fuse and. then rapidly cooling the same.
- bearings which consists in providing a steel shell of relatively light' flexible character, heating said shell to approximately the melting point of a plastic bronze lining metal, heating said plastic bronze lining metal to a temperature higher than its melting point, depositing said lining metal while in its molten state upon the surface of the heated steel shell, pausing for a short space of time to permit the two metals to fuse and then rapidly cooling the same.
- bearings which consists in combining'a steel shell of relatively flexible character with a liningbf plastic bronze by heating the two metals to a temperature that will not melt the steel but will melt the lining metal,' permitting the two metals to fuse and then rapidly cooling the same.
- bearings which consists in combining a steel shell with a lining of plastic bronze" by heating the two metals to a temperature that will not melt the steel, but will melt the lining metal, permitting the two metals to fuse and then rapidly cooling the same.
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Sliding-Contact Bearings (AREA)
Description
Sept. 20, 1938. GlLMAN 2,130,461
- METHOD OF MAKING BEARINGS Fild may 6' 2 Fig-l; A
B EIEE BRONZE,
\f i ammo I v v H I H 127mm 1 Patented- Sept. 20, 193% UNITE sires METHOD OF MAKING- BEGS Norman E. Gilman, Indianapolis, Ind, assignor, by mesne assignments, to General Motors Corporation, Detroit, Mich,
were
a corporation of Dela- Application my 6, 1929, Serial No. 36(i,899
In the development of motors designed for high speed and heavy loads it is important that they be of the lightest weight possible in order that the least amount of power may be required to propel their own weight and, therefore, that metal oi. the lightest weight possible be employed. This has resulted in the improvement of metals used for such purposes so that the weight has been decreased without impairing the strength and endurance qualities but more flexibility has resulted, such improved metals being capable of withstanding more or less'flexing. Such flexing of the metals as well as the speed of or the load carried by the motor causes a strain upon the bearings used which breaks down lining of such material as Babbitt metal, which has heretofore been generally employedfor such purposes, and also results inthe loosening of the bond between the Babbitt lining and the metal of which the shell is composed,"thereby materially decreasing the life of the bearing and impairing its emciency in use. Inasmuch as the value of the motor in service can equal only the life of the bearing it becomes more and more important in the development of this art that bearings be provided which will stand up under the flexing and the great speed and the great load imposed without danger of destruction in the performance of such duty and particularly without separation are composed.
The object of my said invention is to provide a bearing and a method of making the same composed of metals which will provide a bearing of the necessary strength and rigidity and a bearing surface which will be of comparatively soft wearing quality but at the same time capable of resisting much higher temperature and withstanding much greater strain or "pounding" in servicefords the best foundation for a bearing such asrequired for the purpose indicated for the reason that it may be of lighter weight for the samedegree of strength than any other metal which I have found suitable for the purpose. I have so also found that so-called "plastic bronze" makes a most desirable metal for the lining or wearing surface for the bearing. By "plastic bronze" I mean a compositioncomposed of copper and lead the proportions of which may be varied to suit difierent conditions and different requirements, a
of the metals of which the shell and the lining (UL 22-68) I suitable composition being thirty (30) parts of lead and seventy parts oflcopper. Plastic bronze is generally understood to also include, if desired, copper alloys of from 4% to 7% tin with 20% to 30% lead and with or without small quantities of nickel. It will be understood that in using the term "plastic bronze herein it is intended to include all such suitable compositions and variations thereof. As is we'll known the melting point of steel is considerably higher than the melting pointof the bronze but the melting point of bronze is very much higher than the melting point of babbitt and the bronze of a composition such as above indicated while afiording a most excellent surface for the bearings of high speed In the manufacture of bearings of my said invention I employ a method by which the steel shell and the bronze lining or bearing surface are united by fusing the two metals to unite them by a bond that makes them practically integral and permanent so that separation under any strein,.load or flexing imposed'by the duty of the motor is impossible.
In the accompanying drawing, Figure 1 illustrates a bearing such as contemplated by my invention, the bearing housing usually of aluminum or any other appropriate metal being indicated by the reference letter A, the steel shell by the reference letter B, and the bronze lining by the reference letter C.
In Figure 2 I illustrate a method the bearing which consists in mounting a cylinder D with. a bottom 12 within the shell B and pouring the molten bronze from a ladle E into the space between the cylinder and the inner .surface of the shell, It will be understood of l course that the ends of the bearing are me.- chined ofi' appropriately after the bearing is finished. The bottom d of the cylinder D is large enough to cover the end of the shell B as clearly indicated. c i
While I have illustrated this as a method by which the molten bronze may be appliedto the shell it will be understood, of course, that any other appropriate method may be employed, whether it be the method of pouring, the method of die casting, or the method of applying by centrifugal force or any other method now known or found appropriate. And I also want it understood that while I have specified steel' and plastic bronze" as the two metals preferable in use that these terms aroused as meaning any of forming metals that may be found capable of the use intended. Further, while the method described has been found particularly adapted for the purpose set forth it will be understood of course that it may be modified within the scope of the appended claims. For example, the steelshell and lining metal may be heated together to a temperature where the lining metal will be a sub stantial degree above its melting point and the steel shell a substantial degree below its melting point or the parts may be heated separately to different temperatures so long as the steel shell is a substantial degree below its melting point and, the lining metal a substantial degree above its melting point. The two metals may be united or applied to each other in any manner found practicable, the particular method illustrated and described. being one that I have found suitable for the purpose. As will be understood the steel back and the lining metal may be united in flat sheet form if desired and then rolled or otherwise shaped to form a bearin of the shape desired.
In the practice of the method by which these bearings are produced the steel shell of appropriate thickness is heated to a temperature which is approximately the temperature required for melting the bronze metal which is to' be used to the steel of a temperature substantially the same as that of such bronze metal the two metals fuse and unite firmly together forming a bond that makes the two metals practically integral and incapable of separation regardless of strain, flexing or other duty imposedin use.
After the bronze metal is poured or otherwise applied to the steel shell it is allowed to cool for a short period suflicient to allow the two metals to fuse together but before the lead in the composition of the bronze can settle and separate from the copper by reason of its greater gravity the bearing is immersed in a cold bath and cooled quickly so that the copper and lead content of the bronze composition are held in the metal properly mixed and of the same relative proportions throughout.
The bearing resulting from the practice of the method herein set forth is made the subject matter of another application No. 575,117, filed November 14, 1931, as a division of this application.
While I have illustrated a bearing with the shell lined on its inner surface with the bronze it will be understood of course that its outside may be in a like manner covered with a bronze bearing surface or the bearing surface may be applied to both sides of the steel shell, depending upon the character of use for which the bearing is intended.
By this method a bearingis providedwhich has been found capable of withstanding the severe requirements of motors designed for the highest speed in airplane and other service and by actual test and comparison such bearings have been able to far exceed in their efficiency in these respects any bearings made by any other processes heretofore known.
Having thus fully described my said invention, what I claim as new and desire to secure by Letters Patent, is:
l. The method of forming bearings which consists in heating a steel shell to approximately the melting point of the bronze lining metal, heating the bronze lining metal to a temperature higher than its melting point, depositing said lining metal while so heated upon the surface of the heated shell, permitting the two metals to fuse and. then rapidly cooling the same.
2. The method of forming bearings which consists in providing a steel shell of relatively light' flexible character, heating said shell to approximately the melting point of a plastic bronze lining metal, heating said plastic bronze lining metal to a temperature higher than its melting point, depositing said lining metal while in its molten state upon the surface of the heated steel shell, pausing for a short space of time to permit the two metals to fuse and then rapidly cooling the same.
3. The method of forming bearings which consists of heating a steel body to a temperature higher than the melting point of a composition metal for the bearing surface, mounting a cylindrical core concentrically within said heated steel body, then applying the composition lining metal heated to a temperature higher than its melting point in the space between said core and steel body, allowing time for the two metals to fuse.
and then immersing the bearing and core in a. cold bath to set the composition.
4. The method of forming bearings which consists in combining'a steel shell of relatively flexible character with a liningbf plastic bronze by heating the two metals to a temperature that will not melt the steel but will melt the lining metal,' permitting the two metals to fuse and then rapidly cooling the same.
5. The method of forming bearings which consists in combining a steel shell with a lining of plastic bronze" by heating the two metals to a temperature that will not melt the steel, but will melt the lining metal, permitting the two metals to fuse and then rapidly cooling the same.
6. The process of producing a bearing having an outer iron or steel layer, and an inner layer consisting primarily of copper and lead, said two layers being autogenously welded together at their meeting surfaces, whichprocess comprises contacting a molten mass of saidcopper and lead to form said inner layer, with said outer iron or steel layer heated to 'a temperature sufliciently high to produce an autogenous weld between the layers; permitting said bearing to stand for a time sufficient for an autogenous weld to form between the layers; andflnally drastically chilling said bearing.
NORMAN H. G1LMAN.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US360899A US2130461A (en) | 1929-05-06 | 1929-05-06 | Method of making bearings |
US575117A US2130462A (en) | 1929-05-06 | 1931-11-14 | Bearing |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US360899A US2130461A (en) | 1929-05-06 | 1929-05-06 | Method of making bearings |
Publications (1)
Publication Number | Publication Date |
---|---|
US2130461A true US2130461A (en) | 1938-09-20 |
Family
ID=23419848
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US360899A Expired - Lifetime US2130461A (en) | 1929-05-06 | 1929-05-06 | Method of making bearings |
Country Status (1)
Country | Link |
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US (1) | US2130461A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3304589A (en) * | 1963-07-22 | 1967-02-21 | Vologdin Vladisl Valentinovich | Method of casting a wear-resistant layer on cast-iron internal combustion engine cylinder liners |
US5398294A (en) * | 1993-12-10 | 1995-03-14 | Kamatics Corporation | Track roller bearing |
WO2007001826A2 (en) * | 2005-06-21 | 2007-01-04 | Ashmin, Lc | Bearing apparatus and process |
-
1929
- 1929-05-06 US US360899A patent/US2130461A/en not_active Expired - Lifetime
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3304589A (en) * | 1963-07-22 | 1967-02-21 | Vologdin Vladisl Valentinovich | Method of casting a wear-resistant layer on cast-iron internal combustion engine cylinder liners |
US5398294A (en) * | 1993-12-10 | 1995-03-14 | Kamatics Corporation | Track roller bearing |
US5537746A (en) * | 1993-12-10 | 1996-07-23 | Kamatics Corporation | Method of manufacture of improved track roller bearing |
WO2007001826A2 (en) * | 2005-06-21 | 2007-01-04 | Ashmin, Lc | Bearing apparatus and process |
WO2007001826A3 (en) * | 2005-06-21 | 2007-06-14 | Ashmin Lc | Bearing apparatus and process |
GB2444186A (en) * | 2005-06-21 | 2008-05-28 | Lc Ashmin | Bearing apparatus and process |
GB2444186B (en) * | 2005-06-21 | 2010-10-13 | Lc Ashmin | Bearing apparatus and process |
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