US2478037A - Method of applying a silver layer to a steel bearing blank - Google Patents

Method of applying a silver layer to a steel bearing blank Download PDF

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US2478037A
US2478037A US552501A US55250144A US2478037A US 2478037 A US2478037 A US 2478037A US 552501 A US552501 A US 552501A US 55250144 A US55250144 A US 55250144A US 2478037 A US2478037 A US 2478037A
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silver
blank
applying
steel
pressure
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Joseph B Brennan
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    • BPERFORMING OPERATIONS; TRANSPORTING
    • B23MACHINE TOOLS; METAL-WORKING NOT OTHERWISE PROVIDED FOR
    • B23KSOLDERING OR UNSOLDERING; WELDING; CLADDING OR PLATING BY SOLDERING OR WELDING; CUTTING BY APPLYING HEAT LOCALLY, e.g. FLAME CUTTING; WORKING BY LASER BEAM
    • B23K20/00Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating
    • B23K20/22Non-electric welding by applying impact or other pressure, with or without the application of heat, e.g. cladding or plating taking account of the properties of the materials to be welded
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/936Chemical deposition, e.g. electroless plating
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/937Sprayed 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/939Molten or fused coating
    • 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
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S428/00Stock material or miscellaneous articles
    • Y10S428/922Static electricity metal bleed-off metallic stock
    • Y10S428/9335Product by special process
    • Y10S428/94Pressure bonding, e.g. explosive
    • 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
    • Y10T29/49805Shaping by direct application of fluent pressure
    • 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
    • Y10T428/00Stock material or miscellaneous articles
    • Y10T428/12All metal or with adjacent metals
    • Y10T428/12493Composite; i.e., plural, adjacent, spatially distinct metal components [e.g., layers, joint, etc.]
    • Y10T428/12771Transition metal-base component
    • Y10T428/12861Group VIII or IB metal-base component
    • Y10T428/12896Ag-base component

Definitions

  • This invention relates to the manufacture of laminated articles of metals or alloys, or metals and non-metals in combination.
  • the purpose of this invention is to secure improved adhesion between laminations in laminated articles and especially between layers of material or bodies of material and adjacent metallic layers, and even more particularly to secure an improved adhesion in coatings or overlays of metals onto metallic bodies, sheets or articles.
  • an electrodeposited coating on the outside of a metallic article may be, by my invention, given enhanced adhesion to the inner metal article and strength to the unit.
  • Im'pregnation of metals with metals may also be accomplished by my invention, especially where porosity in the inner body exists and the melting point of the outside metal is lower than that of the inside metal and there is a complete sheath or seal and coverage of non-porous metal over the porous inner body or layer.
  • tungsten carbide shapes or briquets may be impregnated with nickel or silver or other alloying binders to produce a hard material unusually dense and superior for tools to cut metals.
  • Fig. 1 represents a silver plated flanged steel backed bearing now in common use on aircraft engines after plating and prior to final machining;
  • Fig. 2 is a vertical sectional view of a pressure vessel such as suitable for use in the treatin process.
  • the steel blank or shell I is provided with a surface layer 2 of silver, such as by plating thereon.
  • a suitable form of apparatus may involve a pressure vessel 3, of generally cylindrical shape and having a gas-tight removable cover 4.
  • Suitable cooling means for the wall of the vessel such as water cooling coils, not shown, may be arranged about the wall.
  • heatin means such as electric heating means 5, may be provided, and such as to be spaced from the walls by porous insulation 6.
  • the source of this high pressure gas may be a gas cylinder, not shown, connected to the pipe 1;
  • a pyrometer 8 indicates the temperature in the chamber 9, and thus the treating temperature may be controlled as required.
  • the coated bearing is placed in the chamber 9, and the cover 4 is fastened in place, and electric current is fed to the heating coil 5 to a temperature sufficient to soften or render the silver plastic, and the gas is fed into line I at a pressure of, for instance, 1,000 to 3,000 lbs. per square inch for a suitable time, for instance 5 to 15 minutes.
  • the coating is softened under the heat and by the high pressure is compacted intimately into the interstices of the face of the steel blank, alloying therewith in a contact or boundary layer.
  • the gas pressure by line 1 is now shut off, and the vent i0 is opened.
  • the cover 4 may then be removed and the bearing taken out and cooled and finished as desired; as, for instance, by a final machining.
  • the coating is completely adherent at all points to the steel shell.
  • An alternate method of securing improved adherence of laminated metals is to take the steel blank I and place on the inside and outside of same a silver stamping of sheet silver in close fittin relationship.
  • the close fit between the sheet silver stampings and the steel blank may be accomplished in a hydraulic press or by spinning as is well known.
  • Raw edges of the silver shell will remain after such an assembly however, and it is necessary to seal these raw edges to the steel blank so that gas will not leak behind the silver shells or overlays.
  • I weld or solder these edges to the steel blank or/and to each other.
  • a sintered blank of powdered steel is used instead of a machined from solid steel blank, the silver outside the blank being applied in a press to the outside of said powdered metal blank after it has been sintered to make a close fitting assembly.
  • the exposed portion, if any, of the powdered metal blank may then be coated with a sealing metal such as a high melting solder and this may also be used to seal the raw edges of the silver shells to the powdered metal blank and then this assembly may be treated in the pressure furnace similarly to the above described procedure with the machined from solid steel blank.
  • the pressure furnace has an inner chamber for silvered steel bearings which is preferably spaced and insulated from the wall of the pressure furnace so that heat loss will be minimized. It is also desirable to maintain the temperature of the pressure vessel enclosing the furnace as with water coils so that it retains its strength.
  • Vacuum treatment of the assemblies prior to pressure heat treatment may also be used according to my invention and may be most desirable when individual units are treated with high frequency permitting the rapid change of atmosphere from vacuum to pressure.
  • a paste of powdered silver with a binder of camphor and a volatile solvent may be applied to the steel blank by spreading evenly as by the use of' a woven screen and squeegee, i. e., by the so-called silk screen process after which the coated blank is baked to dry and sintered, then subjected to the pressure furnace treatment.
  • a method of the character described which comprises silver plating a steel bearing blank, and subjecting such plated article to heat to soften the silver while applying gaseous pressure at least 1000 pounds per square inch for at least five minutes.
  • a method of the character described which comprises applying a thin surfacing of silver to a steel bearing blank, and heating and softening the silver under pressure of at least 1000 pounds per square inch for at least five minutes.
  • a method of the character described which comprises applying silver to a steel bearing blank and heating to softening of the silver under pressure of an inert gas of at least 1000 pounds per square inch for at least five minutes.
  • a method of the character described which comprises nickel plating a steel bearing blank, applying silver to the plated surface, and then heat-softening the silver and forcing it into the adjacent surface by applying high pressure by a gas for at least five minutes.
  • a method of the character described which comprises applying a layer of fusible metal to a blank of higher melting point, and heat-softening the fusible metal while applying elastic pressure of at least 1000 pounds per square inch equally on all sides for at least five minutes.
  • a method of the character described which comprises applying a thin surface sheet of fusible metal to a blank of higher melting point, sealing the raw edges of the fusible sheet, and heatsoftening the fusible metal under elastic pressure of at least 1000 pounds per square inch equally on all sides for at least five minutes.
  • a method of the character described which comprises uniting a. gas-impenetrable fusible metal layer on a layer of metal of higher melting point by heat-softening the fusible metal while, in unobstructed contact equally on both layers, forcing gas at high pressure to elastically compact the metals together, for at least a few minutes.

Description

Aug. 2, 1949. J B. BRENNAN METHOD OF AI PLYING A SILVER LAYER TO A STEEL BEARING BLANK Filed Sept. 2, 1944 FIGJI l/oszpy d Bgewvmv Patented Aug. 2, 1949 -UNITED STATES PATENT OFFICE METHOD OF APPLYING A SILVER LAYER TO A STEEL BEARING BLANK Joseph B. Brennan, Bratenahl, Ohio Application September 2, 1944, Serial No. 552,501
7 Claims. 1
This invention relates to the manufacture of laminated articles of metals or alloys, or metals and non-metals in combination.
The purpose of this invention is to secure improved adhesion between laminations in laminated articles and especially between layers of material or bodies of material and adjacent metallic layers, and even more particularly to secure an improved adhesion in coatings or overlays of metals onto metallic bodies, sheets or articles.
Thus, an electrodeposited coating on the outside of a metallic article may be, by my invention, given enhanced adhesion to the inner metal article and strength to the unit.
Im'pregnation of metals with metals may also be accomplished by my invention, especially where porosity in the inner body exists and the melting point of the outside metal is lower than that of the inside metal and there is a complete sheath or seal and coverage of non-porous metal over the porous inner body or layer.
Thus, tungsten carbide shapes or briquets may be impregnated with nickel or silver or other alloying binders to produce a hard material unusually dense and superior for tools to cut metals.
There is a pronounced need at present for the use of my invention in the manufacture of silver plated airplane engine bearings. At present from one to ten per cent of all silver plated bearings are rejected due to poor adherence of the plating to the steel body.
As an example of a method of carrying out my invention referring to the drawings which accompany this application and are a part thereof:
Fig. 1 represents a silver plated flanged steel backed bearing now in common use on aircraft engines after plating and prior to final machining; and
Fig. 2 is a vertical sectional view of a pressure vessel such as suitable for use in the treatin process.
Referring to Fig. 1 of the drawing, the steel blank or shell I is provided with a surface layer 2 of silver, such as by plating thereon. For heating and uniting the surface layer with the body of such structure, one suitable form of apparatus may involve a pressure vessel 3, of generally cylindrical shape and having a gas-tight removable cover 4. Suitable cooling means for the wall of the vessel, such as water cooling coils, not shown, may be arranged about the wall. Inside, heatin means, such as electric heating means 5, may be provided, and such as to be spaced from the walls by porous insulation 6.
A high pressure gas line 1 to supply inert gas, such as CO or N, is connected to the pressure vessel and is provided with suitable control valve means. The source of this high pressure gas may be a gas cylinder, not shown, connected to the pipe 1; A pyrometer 8 indicates the temperature in the chamber 9, and thus the treating temperature may be controlled as required.
The coated bearing is placed in the chamber 9, and the cover 4 is fastened in place, and electric current is fed to the heating coil 5 to a temperature sufficient to soften or render the silver plastic, and the gas is fed into line I at a pressure of, for instance, 1,000 to 3,000 lbs. per square inch for a suitable time, for instance 5 to 15 minutes. The coating is softened under the heat and by the high pressure is compacted intimately into the interstices of the face of the steel blank, alloying therewith in a contact or boundary layer. The gas pressure by line 1 is now shut off, and the vent i0 is opened. The cover 4 may then be removed and the bearing taken out and cooled and finished as desired; as, for instance, by a final machining. The coating is completely adherent at all points to the steel shell.
An alternate method of securing improved adherence of laminated metals is to take the steel blank I and place on the inside and outside of same a silver stamping of sheet silver in close fittin relationship. The close fit between the sheet silver stampings and the steel blank may be accomplished in a hydraulic press or by spinning as is well known. Raw edges of the silver shell will remain after such an assembly however, and it is necessary to seal these raw edges to the steel blank so that gas will not leak behind the silver shells or overlays. In order to prevent this gas infiltration, according to my invention, I weld or solder these edges to the steel blank or/and to each other.
As a further example, a sintered blank of powdered steel is used instead of a machined from solid steel blank, the silver outside the blank being applied in a press to the outside of said powdered metal blank after it has been sintered to make a close fitting assembly. The exposed portion, if any, of the powdered metal blank may then be coated with a sealing metal such as a high melting solder and this may also be used to seal the raw edges of the silver shells to the powdered metal blank and then this assembly may be treated in the pressure furnace similarly to the above described procedure with the machined from solid steel blank.
The limiting factors with reference to adhesion furnace.
The pressure furnace has an inner chamber for silvered steel bearings which is preferably spaced and insulated from the wall of the pressure furnace so that heat loss will be minimized. It is also desirable to maintain the temperature of the pressure vessel enclosing the furnace as with water coils so that it retains its strength.
The use of high frequency currents to accelerate heating may be desirable in some applictions and is contemplated as a part of my invention. It is also contemplated by my invention that a thin plate of a metal, such as nickel, may be applied to the steel blank prior to the application of the silver plate or shell.
Vacuum treatment of the assemblies prior to pressure heat treatment may also be used according to my invention and may be most desirable when individual units are treated with high frequency permitting the rapid change of atmosphere from vacuum to pressure.
It is also contemplated, according to my invention, that other methods of applying the silver coating may be used, for example, a paste of powdered silver with a binder of camphor and a volatile solvent may be applied to the steel blank by spreading evenly as by the use of' a woven screen and squeegee, i. e., by the so-called silk screen process after which the coated blank is baked to dry and sintered, then subjected to the pressure furnace treatment.
Another method of carrying out my invention is to spray silver onto a heated steel blank with a metal spray gun and then heat to fuse all the particles of silver together and eliminate porosity and then subject this spray coated blank to the pressure furnace treatment.
Having described my invention, what I claim is:
1. A method of the character described, which comprises silver plating a steel bearing blank, and subjecting such plated article to heat to soften the silver while applying gaseous pressure at least 1000 pounds per square inch for at least five minutes.
2. A method of the character described, which comprises applying a thin surfacing of silver to a steel bearing blank, and heating and softening the silver under pressure of at least 1000 pounds per square inch for at least five minutes.
3. A method of the character described, which comprises applying silver to a steel bearing blank and heating to softening of the silver under pressure of an inert gas of at least 1000 pounds per square inch for at least five minutes.
4. A method of the character described, which comprises nickel plating a steel bearing blank, applying silver to the plated surface, and then heat-softening the silver and forcing it into the adjacent surface by applying high pressure by a gas for at least five minutes.
5. A method of the character described, which comprises applying a layer of fusible metal to a blank of higher melting point, and heat-softening the fusible metal while applying elastic pressure of at least 1000 pounds per square inch equally on all sides for at least five minutes.
6. A method of the character described, which comprises applying a thin surface sheet of fusible metal to a blank of higher melting point, sealing the raw edges of the fusible sheet, and heatsoftening the fusible metal under elastic pressure of at least 1000 pounds per square inch equally on all sides for at least five minutes.
7. A method of the character described, which comprises uniting a. gas-impenetrable fusible metal layer on a layer of metal of higher melting point by heat-softening the fusible metal while, in unobstructed contact equally on both layers, forcing gas at high pressure to elastically compact the metals together, for at least a few minutes.
JOSEPH B. BRENNAN.
REFERENCES CITED UNITED STATES PATENTS Number Name Date 1,019,532 Salm Mar. 5, 1912 1,226,470 Coolidge May 5, 1917 1,522,676 Gerleman Jan. 13, 1925 1,550,157 Gillette Aug. 18, 1925 1,556,758 Clark Oct. 13, 1925 2,074,352 Armstrong Mar. 23, 1937 2,160,559 Orr, Jr. May 30, 1939 2,178,527 Wellman Oct. 31, 1939 2,181,083 Payette Nov. 21, 1939 2,266,276 Schluchtes et a1. Dec. 16, 1941 2,283,219 McCullough May 19, 1942 2,294,404 Hensel Sept. 1, 1942 2,298,908 Wentworth Oct. 13, 1942 2,364,713 Hensel Dec. 12, 1944 2,372,202 Hensel Mar. 27, 1945 2,373,116 Hobrock Apr. 10, 1945 2,386,951 Howe Oct. 16, 1945 Guinea Jan. 15, 1946
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Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2657298A (en) * 1951-10-29 1953-10-27 Smith Corp A O Method and apparatus for manufacturing composite plates
US2664326A (en) * 1947-02-11 1953-12-29 Ekstrand & Tholand Inc Plated bearing and the manufacture thereof
US2912551A (en) * 1957-07-31 1959-11-10 Smith Corp A O Method and apparatus for bonding laminated structures
US2932885A (en) * 1960-04-19 Method and pack for making zirconium-clad steel plate
US2932882A (en) * 1954-02-25 1960-04-19 Jr John C R Kelly Method of preparing powdered refractory metals for mechanical working
US3000755A (en) * 1956-10-11 1961-09-19 Gen Motors Corp Oxidation-resistant turbine blades
US3116548A (en) * 1958-01-03 1964-01-07 Smith Corp A O Method of bonding metal members
US3131459A (en) * 1959-11-09 1964-05-05 Corning Glass Works Method of bonding absorbing material to a delay line
US3163500A (en) * 1962-08-03 1964-12-29 Engelhard Ind Inc Sandwich composite brazing alloy
US3165823A (en) * 1959-06-26 1965-01-19 Eaton Mfg Co Metallic surface coating and method for making the same
US4492021A (en) * 1979-12-24 1985-01-08 Chloride Silent Power Limited Method of making cathode current collectors for sodium sulphur cells
US4709848A (en) * 1957-10-02 1987-12-01 The United States Of America As Represented By The United States Department Of Energy Method of bonding
US5846610A (en) * 1993-10-01 1998-12-08 Clinical Diagnostic Systems Production of carriers for surface plasmon resonance
US10087984B2 (en) 2015-06-30 2018-10-02 Saint-Gobain Performance Plastics Corporation Plain bearing

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1019532A (en) * 1911-02-20 1912-03-05 Sali Salm Apparatus for making tight the pores of castings.
US1226470A (en) * 1915-02-20 1917-05-15 Gen Electric Refractory-metal tube.
US1522676A (en) * 1923-11-03 1925-01-13 Oscar W Gerleman Piston-ring and cylinder testing and treating device
US1550157A (en) * 1924-01-02 1925-08-18 Gen Electric Progressive system of brazing
US1556758A (en) * 1924-08-23 1925-10-13 Caribonum Ltd Inking device
US2074352A (en) * 1936-07-11 1937-03-23 Percy A E Armstrong Method of making composite metal articles
US2160559A (en) * 1936-10-17 1939-05-30 Jr John B Orr Manufacture of composite metal members
US2178527A (en) * 1938-05-28 1939-10-31 Sk Wellman Co Composite machine element and method of making same
US2181083A (en) * 1936-01-02 1939-11-21 Metals & Controls Corp Laminated contact
US2266276A (en) * 1939-06-23 1941-12-16 Gen Motors Corp Combined heat treatment and bending method
US2283219A (en) * 1939-11-24 1942-05-19 Bohn Aluminium & Brass Corp Bearing
US2294404A (en) * 1940-08-22 1942-09-01 Mallory & Co Inc P R Silver bearing
US2298908A (en) * 1940-12-31 1942-10-13 Rca Corp Powdered metal
US2364713A (en) * 1943-06-22 1944-12-12 Mallory & Co Inc P R Bearing
US2372202A (en) * 1940-05-08 1945-03-27 Mallory & Co Inc P R Bearing
US2373116A (en) * 1941-10-31 1945-04-10 Bundy Tubing Co Method of uniting metals
US2386951A (en) * 1942-04-23 1945-10-16 Gen Motors Corp Method of making bearings
US2392917A (en) * 1944-01-26 1946-01-15 Wilson H A Co Silver cladding

Patent Citations (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1019532A (en) * 1911-02-20 1912-03-05 Sali Salm Apparatus for making tight the pores of castings.
US1226470A (en) * 1915-02-20 1917-05-15 Gen Electric Refractory-metal tube.
US1522676A (en) * 1923-11-03 1925-01-13 Oscar W Gerleman Piston-ring and cylinder testing and treating device
US1550157A (en) * 1924-01-02 1925-08-18 Gen Electric Progressive system of brazing
US1556758A (en) * 1924-08-23 1925-10-13 Caribonum Ltd Inking device
US2181083A (en) * 1936-01-02 1939-11-21 Metals & Controls Corp Laminated contact
US2074352A (en) * 1936-07-11 1937-03-23 Percy A E Armstrong Method of making composite metal articles
US2160559A (en) * 1936-10-17 1939-05-30 Jr John B Orr Manufacture of composite metal members
US2178527A (en) * 1938-05-28 1939-10-31 Sk Wellman Co Composite machine element and method of making same
US2266276A (en) * 1939-06-23 1941-12-16 Gen Motors Corp Combined heat treatment and bending method
US2283219A (en) * 1939-11-24 1942-05-19 Bohn Aluminium & Brass Corp Bearing
US2372202A (en) * 1940-05-08 1945-03-27 Mallory & Co Inc P R Bearing
US2294404A (en) * 1940-08-22 1942-09-01 Mallory & Co Inc P R Silver bearing
US2298908A (en) * 1940-12-31 1942-10-13 Rca Corp Powdered metal
US2373116A (en) * 1941-10-31 1945-04-10 Bundy Tubing Co Method of uniting metals
US2386951A (en) * 1942-04-23 1945-10-16 Gen Motors Corp Method of making bearings
US2364713A (en) * 1943-06-22 1944-12-12 Mallory & Co Inc P R Bearing
US2392917A (en) * 1944-01-26 1946-01-15 Wilson H A Co Silver cladding

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2932885A (en) * 1960-04-19 Method and pack for making zirconium-clad steel plate
US2664326A (en) * 1947-02-11 1953-12-29 Ekstrand & Tholand Inc Plated bearing and the manufacture thereof
US2657298A (en) * 1951-10-29 1953-10-27 Smith Corp A O Method and apparatus for manufacturing composite plates
US2932882A (en) * 1954-02-25 1960-04-19 Jr John C R Kelly Method of preparing powdered refractory metals for mechanical working
US3000755A (en) * 1956-10-11 1961-09-19 Gen Motors Corp Oxidation-resistant turbine blades
US2912551A (en) * 1957-07-31 1959-11-10 Smith Corp A O Method and apparatus for bonding laminated structures
US4709848A (en) * 1957-10-02 1987-12-01 The United States Of America As Represented By The United States Department Of Energy Method of bonding
US3116548A (en) * 1958-01-03 1964-01-07 Smith Corp A O Method of bonding metal members
US3165823A (en) * 1959-06-26 1965-01-19 Eaton Mfg Co Metallic surface coating and method for making the same
US3131459A (en) * 1959-11-09 1964-05-05 Corning Glass Works Method of bonding absorbing material to a delay line
US3163500A (en) * 1962-08-03 1964-12-29 Engelhard Ind Inc Sandwich composite brazing alloy
US4492021A (en) * 1979-12-24 1985-01-08 Chloride Silent Power Limited Method of making cathode current collectors for sodium sulphur cells
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US10087984B2 (en) 2015-06-30 2018-10-02 Saint-Gobain Performance Plastics Corporation Plain bearing

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