US1923075A - Composite metal article and method of forming the same - Google Patents

Composite metal article and method of forming the same Download PDF

Info

Publication number
US1923075A
US1923075A US366467A US36646729A US1923075A US 1923075 A US1923075 A US 1923075A US 366467 A US366467 A US 366467A US 36646729 A US36646729 A US 36646729A US 1923075 A US1923075 A US 1923075A
Authority
US
United States
Prior art keywords
tube
metal
alloy
lining
forming
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
Application number
US366467A
Inventor
Brown Walter
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US366467A priority Critical patent/US1923075A/en
Application granted granted Critical
Publication of US1923075A publication Critical patent/US1923075A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • CCHEMISTRY; METALLURGY
    • C23COATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; CHEMICAL SURFACE TREATMENT; DIFFUSION TREATMENT OF METALLIC MATERIAL; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL; INHIBITING CORROSION OF METALLIC MATERIAL OR INCRUSTATION IN GENERAL
    • C23CCOATING METALLIC MATERIAL; COATING MATERIAL WITH METALLIC MATERIAL; SURFACE TREATMENT OF METALLIC MATERIAL BY DIFFUSION INTO THE SURFACE, BY CHEMICAL CONVERSION OR SUBSTITUTION; COATING BY VACUUM EVAPORATION, BY SPUTTERING, BY ION IMPLANTATION OR BY CHEMICAL VAPOUR DEPOSITION, IN GENERAL
    • C23C24/00Coating starting from inorganic powder
    • C23C24/08Coating starting from inorganic powder by application of heat or pressure and heat
    • C23C24/10Coating starting from inorganic powder by application of heat or pressure and heat with intermediate formation of a liquid phase in the layer
    • C23C24/103Coating with metallic material, i.e. metals or metal alloys, optionally comprising hard particles, e.g. oxides, carbides or nitrides
    • C23C24/106Coating with metal alloys or metal elements only
    • 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
    • Y10T29/49643Rotary bearing
    • Y10T29/49647Plain bearing
    • Y10T29/49668Sleeve or bushing making
    • Y10T29/49677Sleeve or bushing making having liner
    • 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
    • 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
    • Y10T29/49709Specific metallic composition

Definitions

  • the invention relates to the manufacture of composite metal articles composed of two or more different metals or alloys which are integrally bonded together. More particularly the invention relates to tubing or tubular'articles having an inner lining of a different composition from the outer material.
  • the object of the invention is to provide an improved process for obtaining the inner metallic lining in good condition and well bonded to the outer material.
  • a further object is to provide a process adapted for readily producing certain articles of commerce where it is desirable to have in a single article properties which can only be obtained by using twoor more different metals or alloys.
  • Figure 1 is a sectional view of an apparatus in which my improved method may be carried out
  • Figure 2 is a transverse section through the tubular article during the process
  • Figure 3 is a cross section of the article at the end of the process
  • Figure 4 is an axial section through a valve seat bushing made in accordance with my invention.
  • the metal or alloy forming the inner lining shall have a lower melting point than the metal or alloy constituting the outer' portion.
  • My invention is applicable to various metals and alloys but there are certain particularly advantageous combinations, one of which consists of an outer steel shell provided with a brass or bronze inner lining and another consists of an outer steel or alloy shell with an inner lining of a hard non-machinable alloy of the cobalt chromium type such, for example, as Stellite or other metals having similar properties and normally used for cutting tools.
  • I provide a tube within which is placed the quantity of metal or alloy necessary to provide an inner coating of the desired thickness.
  • the alloy is preferably introduced into the tube in the form of small pieces 13 and after it is placed therein the ends of the tube are closed in a suitable manner.
  • - 14 and 15 represent end plugs made of steel, graphlie or other suitable material and designed to i! fit in the ends of the tubes to close the same extween centers 11 and 12 which engage countersinks in the respective end plugs.
  • the plug 15 has a vent 16 extending through the same and the center 30 engaging the plug has flattened sides 31 forming edges for driving the tube and also providing clearance for venting the inside of the tube.
  • the tube may be rotated in any suitable manner but, as shown, it is connected to a sprocket wheel 25 and driven from an electric motor 26 by means of a chain 2'7.
  • the tube In carrying out the process the tube is rotated and the current to the induction furnace turned on, thereby developing heat in the tube and alloy while they are being rotated.
  • the temperature reaches the melting point of the alloy it is reduced to a molten condition and forms a pool 28 at-the bottom of thetube with which the side walls are continuously washed-during the rotation.
  • the washing of the side walls removes any dirt or other foreign substance adhering to the walls and permits the molten metal to come into actual contact with the metal of the outer tube 10.
  • the tubing is then removed from the furnace and the rotation of the same continued 95 while allowing the molten metal to cool off and gradually lose its fluidity.
  • the fluid is bonded to the outer tube and as solidiflcation takes place the alloy becomes formed into a circular ring, all portions of which are equally 1 spaced from the surface ofrotation.
  • the tube and maintains the molten metal under a non-oxidizing condition.
  • the process as above described may be usedin the manufacture of various articles such as copper lined tubing, bronze lined steel pipe, bronze lined bearings, etc.
  • Another use for the process is in the manufacture of oil well valve seat bushings wherein the outside shell is formed of steel or other tough metal or alloy and the inside lining is composed of a cobalt chromium alloy of the Stellite type.
  • a suitable cobalt chromium alloy the following composition is given:
  • Figure 4 shows an oil well valve seat bushing comprising an outer ring 10 formed of steel or other tough alloy having an annular rib 11 on the periphery thereof.
  • the inner ring l2 is of uniform diameter and has the beveled seats 13.
  • valve seat bushing when constructed in accordance with the method hereinbefore set forth is of great utility and is far superior to an all-steel bushing or the all-alloy bushing whether or not the same has been heat treated to secure hardness in the valve seat.
  • the bushing is capable of standing up for long periods of time in actual service and the bond between the inner and outer metals is excellent due to the method of uniting the two metals.
  • the invention is not limited to the particular articles above described, but may be used generally in the formation of an inner lining of one metal on another metal, and more particularly for the purpose of lining a tubular outer shell with a metal or alloy of relatively high fusing point.
  • a process of forming composite articles which consists in forming a tube with inwardly projecting flanges at both outer ends thereof, introducing a solid metal into said tube, heating said tube to the melting point of said solid metal while maintaining said tube substantially sealed, rotating said tube while maintaining the seal to distribute the molten metal into intimate contact with the walls of 'said tube and the walls of said flanges. cooling said tube while maintaining the rotation thereof until the inner metal is solidified thereby forming a. solid lining integrally united to said tube and said flanges.
  • a process for lining tubing which consists in introducing solid metal into a tube, said metal having a melting point of at least 1000 F.,
  • a process for lining tubing with metal or alloy having a melting point of at least 1000 R, which consists in introducing the lining metal in a solid state into a tube, closing the ends of said tube with end pieces, welding said end pieces to said tube to provide a tight seal, heating said tube to the melting point of the inner metal, rotating said tube to distribute the molten metal into contact with the walls of said tube and cooling said tube while maintaining the rotation thereof until the inner metal is solidified thereby forming a solid lining integrally united to said tube and said end pieces.
  • a proces'sfor lining tubing with metal or alloy having a melting point of at least 1000 F. which consists in introducing the lining metal in a solid state into a tube, closing the ends of said tube to provide a tight seal sufficient to resist the penetration of the molten lining metal, heating said tube to the melting point of the inner metal, rotating said tube to distribute the molten metal into contact with the walls of said tube and cooling said tube while maintaining the rotation thereof until the inner metal is solidified thereby forming a solid lining integrally united to said tube and the closed end portions thereof.
  • a process for lining tubing with metal or alloy having a melting point of at least 1000" F. which consists in introducing the lining metal in a solid state into a tube, sealing the ends of said tube to prevent the inflow of oxidizing gases and permit relief of internal gaseous pressure, heating said tube to the melting point of the inner metal thereby causing an outflow of the expanded gas within said tube, rotating said tube while cooling the same to centrifugally cast the molten metal and removing the closed tube from the rotating means after the solidification of said inner metal.
  • a process for lining tubing with a copper alloy having a melting point of at least 1000 -F. which consists in introducing the copper alloy in a solid state into a tube, sealing the ends of said tube to prevent the inflow of oxidizing gases and permit relief of internal gaseouspressure, heating said tube to the melting point of the copper alloy thereby causing an outflow of the expanded gas within said tube, rotating said tube while cooling the same to centrifugally cast the copper alloy and removing the closed tube from the rotating means after the solidification of said copper alloy.
  • a process for lining tubing with a cobaltchromium alloy having a melting point of at least 1000 F. which consists in introducing the cobaltchromium alloy in a solid state into a tube, sealing the ends of said tube to prevent the inflow of oxidizing gases and permit relief of internal gaseous pressure, heating said tube to the melting point of the cobalt-chromium alloy thereby causing an outflow of the expanded gas within said tube, rotating said tube while cooling the same to centrifugally cast the cobalt-chromium alloy and removing the closed tube from the rotating means after the solidification of said cobaltchromium alloy.

Description

Aug. 22, 1933. w BROWN 1,923,075
COMPOSITE METAL ARTICLE AND METHOD OF FORMING THE SAME Filed May 27, 1929 v INVENTOR ATTORNEYs Patented Aug. 22, 1933 PATENT OFFICE COMPOSITE METAL ARTICLE AND METHOD, OF FORMING THE SAME Walter Brown, Toledo, Ohio Application May 27, 1929. Serial No. 366,467
8 Claims.
The invention relates to the manufacture of composite metal articles composed of two or more different metals or alloys which are integrally bonded together. More particularly the invention relates to tubing or tubular'articles having an inner lining of a different composition from the outer material.
The object of the invention is to provide an improved process for obtaining the inner metallic lining in good condition and well bonded to the outer material. A further object is to provide a process adapted for readily producing certain articles of commerce where it is desirable to have in a single article properties which can only be obtained by using twoor more different metals or alloys.
These and other objects are attained in the manner hereinafter more fully described and illustrated in the accompanying drawing, wherein Figure 1 is a sectional view of an apparatus in which my improved method may be carried out;
Figure 2 is a transverse section through the tubular article during the process;
Figure 3 is a cross section of the article at the end of the process;
Figure 4 is an axial section through a valve seat bushing made in accordance with my invention.
In order to carry out my invention, whichis hereinafter more fully set forth, it is necessary that the metal or alloy forming the inner lining shall have a lower melting point than the metal or alloy constituting the outer' portion. My invention is applicable to various metals and alloys but there are certain particularly advantageous combinations, one of which consists of an outer steel shell provided with a brass or bronze inner lining and another consists of an outer steel or alloy shell with an inner lining of a hard non-machinable alloy of the cobalt chromium type such, for example, as Stellite or other metals having similar properties and normally used for cutting tools.
In ca y g out the process for obtaining the composite metal article, I provide a tube within which is placed the quantity of metal or alloy necessary to provide an inner coating of the desired thickness. The alloy is preferably introduced into the tube in the form of small pieces 13 and after it is placed therein the ends of the tube are closed in a suitable manner.- 14 and 15 represent end plugs made of steel, graphlie or other suitable material and designed to i! fit in the ends of the tubes to close the same extween centers 11 and 12 which engage countersinks in the respective end plugs. The plug 15 has a vent 16 extending through the same and the center 30 engaging the plug has flattened sides 31 forming edges for driving the tube and also providing clearance for venting the inside of the tube.
While any suitable type of furnace may be used, it has been found particularly advantageous to employ a high frequency induction furnace, as in this type of furnace the hottest part is the metal itself. Thus, as illustrated in the drawing, thereis the quartz tube 21, outside of which is the induction coil 22 for supplying the power to the furnace, this being placed within a protective housing 23. I
The tube may be rotated in any suitable manner but, as shown, it is connected to a sprocket wheel 25 and driven from an electric motor 26 by means of a chain 2'7.
In carrying out the process the tube is rotated and the current to the induction furnace turned on, thereby developing heat in the tube and alloy while they are being rotated. When the temperature reaches the melting point of the alloy it is reduced to a molten condition and forms a pool 28 at-the bottom of thetube with which the side walls are continuously washed-during the rotation. The washing of the side walls removes any dirt or other foreign substance adhering to the walls and permits the molten metal to come into actual contact with the metal of the outer tube 10. The tubing is then removed from the furnace and the rotation of the same continued 95 while allowing the molten metal to cool off and gradually lose its fluidity. During this operation the fluid is bonded to the outer tube and as solidiflcation takes place the alloy becomes formed into a circular ring, all portions of which are equally 1 spaced from the surface ofrotation.
With some metals it is advantageous to increase the speed of the tubing, after the metal has given the walls the washing action, and
the tube and maintains the molten metal under a non-oxidizing condition.
The process as above described may be usedin the manufacture of various articles such as copper lined tubing, bronze lined steel pipe, bronze lined bearings, etc. Another use for the process is in the manufacture of oil well valve seat bushings wherein the outside shell is formed of steel or other tough metal or alloy and the inside lining is composed of a cobalt chromium alloy of the Stellite type. As an example of a suitable cobalt chromium alloy, the following composition is given:
APPIOXiIllIlii' perccniuge Cobalt 50 Chromium 32 Tungsten 16 Molybdenum 2 Figure 4 shows an oil well valve seat bushing comprising an outer ring 10 formed of steel or other tough alloy having an annular rib 11 on the periphery thereof. The inner ring l2 is of uniform diameter and has the beveled seats 13.
The valve seat bushing, above described, when constructed in accordance with the method hereinbefore set forth is of great utility and is far superior to an all-steel bushing or the all-alloy bushing whether or not the same has been heat treated to secure hardness in the valve seat. The bushing is capable of standing up for long periods of time in actual service and the bond between the inner and outer metals is excellent due to the method of uniting the two metals.
It is to be understood that the invention is not limited to the particular articles above described, but may be used generally in the formation of an inner lining of one metal on another metal, and more particularly for the purpose of lining a tubular outer shell with a metal or alloy of relatively high fusing point.
What I claim as my invention is:
1. The process of forming composite articles of two metals of different composition having melting points above 1000 F. which consists in placing one metal in a solid state within a tube of dissimilar metal, sealing the opening at both ends of the tube, heating the tube to a temperature sufficient to melt the first mentioned metal, rotating the tube to cause the molten metal to adhere to the inner walls of said tube by centrifugal force cooling the tube'while maintaining said rotation until said molten metal is solidified and removing from the rotating means the sealed tube line with the first named metal.
2. A process of forming composite articles which consists in forming a tube with inwardly projecting flanges at both outer ends thereof, introducing a solid metal into said tube, heating said tube to the melting point of said solid metal while maintaining said tube substantially sealed, rotating said tube while maintaining the seal to distribute the molten metal into intimate contact with the walls of 'said tube and the walls of said flanges. cooling said tube while maintaining the rotation thereof until the inner metal is solidified thereby forming a. solid lining integrally united to said tube and said flanges.
3. A process for lining tubing which consists in introducing solid metal into a tube, said metal having a melting point of at least 1000 F.,
hermetically sealing the ends of the tube except for a small vent, heating said tubing to above the melting point of said metal and rotating said tubing to distribute the molten metal into intimate conact with the walls of said tube.
4. A process for lining tubing with metal or alloy, having a melting point of at least 1000 R, which consists in introducing the lining metal in a solid state into a tube, closing the ends of said tube with end pieces, welding said end pieces to said tube to provide a tight seal, heating said tube to the melting point of the inner metal, rotating said tube to distribute the molten metal into contact with the walls of said tube and cooling said tube while maintaining the rotation thereof until the inner metal is solidified thereby forming a solid lining integrally united to said tube and said end pieces.
5. A proces'sfor lining tubing with metal or alloy having a melting point of at least 1000 F. which consists in introducing the lining metal in a solid state into a tube, closing the ends of said tube to provide a tight seal sufficient to resist the penetration of the molten lining metal, heating said tube to the melting point of the inner metal, rotating said tube to distribute the molten metal into contact with the walls of said tube and cooling said tube while maintaining the rotation thereof until the inner metal is solidified thereby forming a solid lining integrally united to said tube and the closed end portions thereof.
6. A process for lining tubing with metal or alloy having a melting point of at least 1000" F. which consists in introducing the lining metal in a solid state into a tube, sealing the ends of said tube to prevent the inflow of oxidizing gases and permit relief of internal gaseous pressure, heating said tube to the melting point of the inner metal thereby causing an outflow of the expanded gas within said tube, rotating said tube while cooling the same to centrifugally cast the molten metal and removing the closed tube from the rotating means after the solidification of said inner metal.
7. A process for lining tubing with a copper alloy having a melting point of at least 1000 -F. which consists in introducing the copper alloy in a solid state into a tube, sealing the ends of said tube to prevent the inflow of oxidizing gases and permit relief of internal gaseouspressure, heating said tube to the melting point of the copper alloy thereby causing an outflow of the expanded gas within said tube, rotating said tube while cooling the same to centrifugally cast the copper alloy and removing the closed tube from the rotating means after the solidification of said copper alloy.
8. A process for lining tubing with a cobaltchromium alloy having a melting point of at least 1000 F. which consists in introducing the cobaltchromium alloy in a solid state into a tube, sealing the ends of said tube to prevent the inflow of oxidizing gases and permit relief of internal gaseous pressure, heating said tube to the melting point of the cobalt-chromium alloy thereby causing an outflow of the expanded gas within said tube, rotating said tube while cooling the same to centrifugally cast the cobalt-chromium alloy and removing the closed tube from the rotating means after the solidification of said cobaltchromium alloy.
WALTER BROWN.
US366467A 1929-05-27 1929-05-27 Composite metal article and method of forming the same Expired - Lifetime US1923075A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US366467A US1923075A (en) 1929-05-27 1929-05-27 Composite metal article and method of forming the same

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US366467A US1923075A (en) 1929-05-27 1929-05-27 Composite metal article and method of forming the same

Publications (1)

Publication Number Publication Date
US1923075A true US1923075A (en) 1933-08-22

Family

ID=23443123

Family Applications (1)

Application Number Title Priority Date Filing Date
US366467A Expired - Lifetime US1923075A (en) 1929-05-27 1929-05-27 Composite metal article and method of forming the same

Country Status (1)

Country Link
US (1) US1923075A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE748566C (en) * 1939-05-09 1944-11-04 Method and device for the production of composite cast bodies
DE764274C (en) * 1937-07-08 1953-01-26 Gen Motors Corp Procedure for ejecting bearings
US2670509A (en) * 1950-08-24 1954-03-02 Benjamin H Hadley Apparatus for lining bearings
US2670511A (en) * 1953-04-20 1954-03-02 Benjamin H Hadley Method of lining bearings
US4117580A (en) * 1975-04-07 1978-10-03 Friedrich Heck Manufacture of bearings
US4150182A (en) * 1977-05-02 1979-04-17 United States Steel Corporation Method of producing a refractory lining in a cylinder or tube and resultant article
FR2444088A1 (en) * 1978-12-13 1980-07-11 Uk I Spetialnykh Applying protective coating to metal pipe surfaces - simultaneously using metal evaporator and metallisation element for external and internal surfaces.
US4664609A (en) * 1983-12-14 1987-05-12 Honda Giken Kogyo Kabushiki Kaisha Vane holder for vane pump and method of making same
US4679294A (en) * 1982-07-09 1987-07-14 Lomax Donald P Method for making a trimetallic cylinder

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE764274C (en) * 1937-07-08 1953-01-26 Gen Motors Corp Procedure for ejecting bearings
DE748566C (en) * 1939-05-09 1944-11-04 Method and device for the production of composite cast bodies
US2670509A (en) * 1950-08-24 1954-03-02 Benjamin H Hadley Apparatus for lining bearings
US2670511A (en) * 1953-04-20 1954-03-02 Benjamin H Hadley Method of lining bearings
US4117580A (en) * 1975-04-07 1978-10-03 Friedrich Heck Manufacture of bearings
US4150182A (en) * 1977-05-02 1979-04-17 United States Steel Corporation Method of producing a refractory lining in a cylinder or tube and resultant article
FR2444088A1 (en) * 1978-12-13 1980-07-11 Uk I Spetialnykh Applying protective coating to metal pipe surfaces - simultaneously using metal evaporator and metallisation element for external and internal surfaces.
US4679294A (en) * 1982-07-09 1987-07-14 Lomax Donald P Method for making a trimetallic cylinder
US4664609A (en) * 1983-12-14 1987-05-12 Honda Giken Kogyo Kabushiki Kaisha Vane holder for vane pump and method of making same

Similar Documents

Publication Publication Date Title
US1923075A (en) Composite metal article and method of forming the same
US2193088A (en) Poppet valve blank and method of making same
EP1858660A2 (en) Glass-forming die and method
US2964251A (en) Roll structure
US2275503A (en) Process for making composite metal articles and apparatus therefor
US2119042A (en) Valve
US4497358A (en) Process for the manufacture of a steel body with a borehole protected against abrasion
US1005736A (en) Process for manufacturing turbine bucket-wheels.
US1313387A (en) Welded steel barbel and method of making sake
US3461944A (en) Method of manufacturing a lined iron-base article
US1434047A (en) Method of uniting hard steel alloys to softer steel bars
US2207150A (en) Centrifugally cast plunger and tube
US1333337A (en) Method of making bearings
US2289703A (en) Method of making bearings
US627293A (en) Douglas george brighton
US1153197A (en) Art of casting and uniting metals.
US2809407A (en) Method of making a composite metal article
US1920022A (en) Bearing manufcture
US2326730A (en) Mold and method of making the same
US2503533A (en) Process of making bearings
US2670511A (en) Method of lining bearings
US3225400A (en) Method for casting transition couplings
US2033814A (en) Composite metal article
US536184A (en) Method of
US3019512A (en) Joint construction