US3343362A - Bearing members having a plurality of coatings - Google Patents

Bearing members having a plurality of coatings Download PDF

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US3343362A
US3343362A US427741A US42774165A US3343362A US 3343362 A US3343362 A US 3343362A US 427741 A US427741 A US 427741A US 42774165 A US42774165 A US 42774165A US 3343362 A US3343362 A US 3343362A
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coating
oxide
spinning ring
friction
composite
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US427741A
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Dallas F Lunsford
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Dana Inc
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Dana Inc
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C33/00Parts of bearings; Special methods for making bearings or parts thereof
    • F16C33/02Parts of sliding-contact bearings
    • F16C33/04Brasses; Bushes; Linings
    • F16C33/06Sliding surface mainly made of metal
    • 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
    • C23C28/00Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D
    • C23C28/30Coatings combining at least one metallic layer and at least one inorganic non-metallic layer
    • C23C28/32Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer
    • C23C28/321Coatings combining at least one metallic layer and at least one inorganic non-metallic layer including at least one pure metallic layer with at least one metal alloy layer
    • 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
    • C23C8/00Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals
    • C23C8/06Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases
    • C23C8/08Solid state diffusion of only non-metal elements into metallic material surfaces; Chemical surface treatment of metallic material by reaction of the surface with a reactive gas, leaving reaction products of surface material in the coating, e.g. conversion coatings, passivation of metals using gases only one element being applied
    • C23C8/10Oxidising
    • C23C8/16Oxidising using oxygen-containing compounds, e.g. water, carbon dioxide
    • C23C8/18Oxidising of ferrous surfaces
    • DTEXTILES; PAPER
    • D01NATURAL OR MAN-MADE THREADS OR FIBRES; SPINNING
    • D01HSPINNING OR TWISTING
    • D01H7/00Spinning or twisting arrangements
    • D01H7/02Spinning or twisting arrangements for imparting permanent twist
    • D01H7/52Ring-and-traveller arrangements
    • D01H7/60Rings or travellers; Manufacture thereof not otherwise provided for ; Cleaning means for rings
    • D01H7/602Rings
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16CSHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2340/00Apparatus for treating textiles
    • F16C2340/18Apparatus for spinning or twisting

Definitions

  • a ferrous bearing member having a wear surface formed by an inner intimate coating of ferrous oxide and an outer intimate coating of tin or the like so that the bearing members wear surface is hard, durable and scuff resistant.
  • This invention relates to rapidly seating bearing members which are characterized by long life. More particularly, this invention relates to new and novel spinning and the break-in period of spinning rings which will be described forthwith.
  • spinning or twisting rings are used to guide a body of fibers being twisted into yarn or thread from feed rollers through a rotating spindle by means of a traveler which is freely mounted for rotation about the circumference of each ring.
  • Each spinning ring is mounted coaxially with a spindle and reciprocates between the ends of such spindle in a direction of a longitudinal axis of the same to give desired distribution of the spun material thereon,
  • the traveler is usually made from carburized steel and rotates circumferentially about the uppermost flange of the spinning ring.
  • Spinning rings have commonly been madeof steel which has been hardened, ground and polished. In spite of such treatment, these rings possess minutely pitted external surfaces having a relatively high coeflicient of friction, thereby leading to frequent traveler changes and reduced rate of production until the external surfaces are rendered smooth.
  • Various attempts have been made to overcome these defects in spinning rings by coating such surfaces with nickel, nylon, plastics, and the like. Although some of these materials in general tend to alleviate the breakin problem, they have not proven completely satisfactory in other respects.
  • Another object of this invention is to provide an article formed from ferrous metal with an initial coating having a crystalline structure and a second overlaying coating of anti-friction metal.
  • FIG. 1 is an isometric view of a spinning ring incorporating this invention and having a traveler attached thereto;
  • FIG. 2 is a radial cross-section view of the spinning ring of FIG. 1 taken along the line 2-2 in FIG. 1.
  • metals and metal alloys which are known for their lubricating and anti friction properties.
  • This class includes, among others, lead, copper, tin, cadmium, and alloys thereof.
  • Metal alloys which are intended for anti-friction use are sometimes referred to as Babbit'metals, such as alloys containing lead:5% tin and 65% tin:35% nickel.
  • the face plating but is impregnated with the anti-friction metal as well.
  • the anti-friction metal is not completely removed during initial operation.
  • a bearing member is shown in the form of a spinning ring 10 formed from ferrous metal and comprising a central annular rib portion 12 and having a pair of axially spaced flanges 14 and 16 formed integrally therewith.
  • Each of the flanges 14 and 16 extends both radially inward and outward from the rib portion 12 and is adapted to support a traveler 18 for rotation about the circumference of the ring 10.
  • the surface thereof is first finish machined and then subjected to a treatment which provides a layer of iron oxide 22 over the base ferrous metal indicated at 20.
  • the iron oxide layer 22 may be ferric oxide (Fe O ferrosoferric oxide (Fe O sub-layers of Fe O and Fe O or a composite of ferrous oxide (FeO) and Pe O
  • the preferred layers 22 for this invention is a layer of Fe O or a composite layer of FeO and Fe O because of the long wearing characteristics of the same.
  • the Fe O may be formed according to the teachings in United States Patent No. 2,236,728 to F. H. Given; wherein, a ferrous article is held in a superheated steam atmosphere at a temperature between 1,020 F.
  • the composite layer of FeO and Pe o may be deposited by the method taught in the inventors copending United States patent application Ser. No. 420,- 883, filed Dec. 24, 1964; wherein, a ferrous article is heated to a temperature between 1050* F. and 1800 F. in a steam atmosphere and held at that temperature for a period of approximately twenty seconds, after which time the article is quenched.
  • This deposition may be by any conventional method such as electro-plating.
  • a tin layer has been deposited over an iron oxide coating by placing the coated article, which serves as the cathode, and a tin anode in a bath containing one ounce of soliurn hydroxide per gal lon of water at a temperature of 150 F.
  • a power source such as a motor generator, was then utilized to generate a current density of 40 amps/ft
  • a current density of 40 amps/ft Unusually good results have been obtained when an anti-friction metal is applied to an iron oxide surface of a spinning ring in that the need for travel change during initial operation has been eliminated.
  • the elimination of the adverse effects of the break-in period was demonstrated in a test utilizing a Saco-Lowell frame.
  • the recommended break-in period using this type of frame involves five traveler changes; that is, a traveler change after 30 minutes, 24 hours, 48 hours, 72 hours, and 96 hours.
  • Spinning rings formed from cast iron with a ferric oxide-ferrosoferric oxide first coating and an outer layer of tin were installed on a Saco-Lowell frame. Each of the rings supported a carburized steel traveler. After the spinning frames were operated for 24 hours the rings were removed and inspected. No Wear was observed on the original travelers and they were placed back on the ring. The life of these travelers proved equal to the life of travelers subsequently installed. In addition, the spinning rings themselves provided long periods of use. In short, the effect of the break-in period was eliminated without adverse effect on the durability of the spinning ring.
  • the double coating system comprising an iron oxide with an anti-friction metal overlay has been applied to piston rings as well.
  • iron piston rings were given Fe O coatings by the process taught by Givens in United States Patent No. 2,23 6,728. Some of these oxide coated piston rings were plated with cadmium and others with tin. Both soft metals formed an itnegral bond with the oxide surfaces. Some of the double coated piston rings were installed in a test engine and rendered good performance.
  • the thickness of the double coating applied to a member will be determined, mainly, by the size of the article being coated and the application of such member. For example, 2" x 1" x /8 rings having an iron oxide coating varying from 0.00005"-0.0001 and an anti-friction metal overlay of 0.0002"-0.0003" have proven very satisfactory.
  • the thickness of the iron oxide coating is controlled at least by the reaction temperature and time at such reaction temperature.
  • the thickness of the anti-friction metal overlay is controlled at least by the current density of the bath and by the period of coating.
  • a bearing member comprising a base portion formed from ferrous metal and having a wearing surface, a first coating intimately secured to at least a portion of said wearing surface and having a porous crystalline structure selected from the group consisting of ferric oxide, ferrosoferric oxide, a composite of ferric and ferrosoferric oxide and a composite of ferrous oxide and ferrosoferric oxide and a second anti-friction metallic coating intimately secured to said first coating at least at said portion of said wear surface selected from a group consisting of lead, copper, tin, cadmium and alloys thereof, whereby said anti-friction metallic coating is incompletely removed during initial operation of said bearing member.
  • a spinning ring comprising a base portion formed from ferrous metal and having an annular body portion and an annular flange formed coaxially and integrally with said spinning ring, said flange forming a wearing surface, a first coating intimately attached to said flange selected from a group consisting of ferric oxide, ferroso ferric oxide, a composite of ferric and ferrosoferric oxide and a composite of ferrous oxide and ferrosoferric oxide, a second anti-friction metallic coating deposited on said first coating to form an external surface on said spinning ring and covering the first coating on at least said flange, said second coating selected from a group consisting of lead, copper, tin, cadmium and alloys thereof, whereby said anti-friction metallic coating is incompletely removed during initial operation of said spinning ring.

Description

Sept. 26, 1967 D. F. LUNSFORD BEARING MEMBERS HAVING A PLURALITY 0F COATINGS Filed Jan. 25, 1965 FIG. I
FIG.- 2
v INVENTOR- DALLAS- F. LUNSFORD ,LQ M
ATTORNEYS United States Patent Ofiiice 3,343,362 Patented Sept. 26, 1967 3,343,362 BEARING MEMBERS HAVING A PLURALITY F COATINGS Dallas F. Lunsford, Cambridge City, Ind., assignor to Dana Corporation, Toledo, Ohio, a corporation of irginia Filed Jan. 25, 1965, Ser. No. 427,741 2 Claims. (Cl. 57-119) ABSTRACT OF THE DISCLOSURE A ferrous bearing member is disclosed having a wear surface formed by an inner intimate coating of ferrous oxide and an outer intimate coating of tin or the like so that the bearing members wear surface is hard, durable and scuff resistant.
This invention relates to rapidly seating bearing members which are characterized by long life. More particularly, this invention relates to new and novel spinning and the break-in period of spinning rings which will be described forthwith.
In conventional spinning and twisting mechanisms used in the textile industry, spinning or twisting rings are used to guide a body of fibers being twisted into yarn or thread from feed rollers through a rotating spindle by means of a traveler which is freely mounted for rotation about the circumference of each ring. Each spinning ring is mounted coaxially with a spindle and reciprocates between the ends of such spindle in a direction of a longitudinal axis of the same to give desired distribution of the spun material thereon, The traveler is usually made from carburized steel and rotates circumferentially about the uppermost flange of the spinning ring.
A great expense associated with spinning rings involves the changing of travelers when a spinning ring is first used, in addition to a reduced production rate. An appreciation of the expense involved may be obtained by reference to the Mar. 6, 1964, edition of The Textile Weekly, page 381, wherein it is stated, fthat the recommended procedure for running in ordinaryrings involves 36 traveler changes during the first 65 hours and that the spindle speeds must be reduced by about 25% during such period. Although this article gives an'indication of the problem, it should be noted that the number of traveler changes during the break-in of the spinning ring will vary, among other things, with the count of the thread, the speed of the traveler,-and the diameter of the spinning ring.
Spinning rings have commonly been madeof steel which has been hardened, ground and polished. In spite of such treatment, these rings possess minutely pitted external surfaces having a relatively high coeflicient of friction, thereby leading to frequent traveler changes and reduced rate of production until the external surfaces are rendered smooth. Various attempts have been made to overcome these defects in spinning rings by coating such surfaces with nickel, nylon, plastics, and the like. Although some of these materials in general tend to alleviate the breakin problem, they have not proven completely satisfactory in other respects.
It is, therefore, an object of this invention to provide a novel bearing member which is capable of operating at high efiiciency from its initial operation and which has a low rate of wear.
It is another object of this invention to provide a ferrous bearing member having a plurality of coatings.
Another object of this invention is to provide an article formed from ferrous metal with an initial coating having a crystalline structure and a second overlaying coating of anti-friction metal.
It is yet another object of this invention to provide a spinning ring having a low friction surface which substantially eliminates the need for break-in and which has a long period of use.
It is still another object of this invention to provide a bearing member with a porous, long wearing first coating and with a softer, anti-friction second coating formed within the pores and upon the surface of the first coatlng.
Other and further objects of this invention will be ap parent from the following description and claims, and may be understood by reference to the accompanying FIG. 1 is an isometric view of a spinning ring incorporating this invention and having a traveler attached thereto; and
FIG. 2 is a radial cross-section view of the spinning ring of FIG. 1 taken along the line 2-2 in FIG. 1.
There is aclass of metals and metal alloys, hereinafter referred to collectively in the specification and claims as metals, which are known for their lubricating and anti friction properties. This class includes, among others, lead, copper, tin, cadmium, and alloys thereof. Metal alloys which are intended for anti-friction use are sometimes referred to as Babbit'metals, such as alloys containing lead:5% tin and 65% tin:35% nickel.
It has been found that the break-in problem associatedwith ferrous metal bearing members is somewhat relieved when the body of such member is provided with an external layer of anti-friction metal. Unfortunately, the anti-friction metal wears quickly and the exposed ferrous metal tends to gall, seize or score. An unique bearing member has been obtained by initially forming a first coating of an iron oxide, such as Fe O or FeOFe O intimately on the surface of the bearing member and then placing an overlying coating of anti-friction metal on such oxide coated surface. The iron oxides have low wear rates and do not exhibit galling, seizing or scoring tendencies. Consequently, 'such a double coating results in fast break-in and maximum subsequent performance. More particu-.
face plating but is impregnated with the anti-friction metal as well. Thus, the anti-friction metal is not completely removed during initial operation.
Referring to FIGS. 1 and 2, a bearing member is shown in the form of a spinning ring 10 formed from ferrous metal and comprising a central annular rib portion 12 and having a pair of axially spaced flanges 14 and 16 formed integrally therewith. Each of the flanges 14 and 16 extends both radially inward and outward from the rib portion 12 and is adapted to support a traveler 18 for rotation about the circumference of the ring 10.
In preparing the preferred embodiment of the spinning ring 10, the surface thereof is first finish machined and then subjected to a treatment which provides a layer of iron oxide 22 over the base ferrous metal indicated at 20. The iron oxide layer 22 may be ferric oxide (Fe O ferrosoferric oxide (Fe O sub-layers of Fe O and Fe O or a composite of ferrous oxide (FeO) and Pe O The preferred layers 22 for this invention is a layer of Fe O or a composite layer of FeO and Fe O because of the long wearing characteristics of the same. The Fe O may be formed according to the teachings in United States Patent No. 2,236,728 to F. H. Given; wherein, a ferrous article is held in a superheated steam atmosphere at a temperature between 1,020 F. to 1300 F. for a period of one-half hour. The composite layer of FeO and Pe o, may be deposited by the method taught in the inventors copending United States patent application Ser. No. 420,- 883, filed Dec. 24, 1964; wherein, a ferrous article is heated to a temperature between 1050* F. and 1800 F. in a steam atmosphere and held at that temperature for a period of approximately twenty seconds, after which time the article is quenched.
After the oxide coated article is thoroughly cleaned, an anti-friction metal layer 24, such as tin, lead, cadmium or alloys therefrom, is deposited over the iron oxide layer 22 to form the external surface of the bearing member. This deposition may be by any conventional method such as electro-plating. For example, a tin layer has been deposited over an iron oxide coating by placing the coated article, which serves as the cathode, and a tin anode in a bath containing one ounce of soliurn hydroxide per gal lon of water at a temperature of 150 F. A power source, such as a motor generator, was then utilized to generate a current density of 40 amps/ft Unusually good results have been obtained when an anti-friction metal is applied to an iron oxide surface of a spinning ring in that the need for travel change during initial operation has been eliminated. The elimination of the adverse effects of the break-in period was demonstrated in a test utilizing a Saco-Lowell frame. The recommended break-in period using this type of frame involves five traveler changes; that is, a traveler change after 30 minutes, 24 hours, 48 hours, 72 hours, and 96 hours. By using the spinning ring of this invention with a Saco-Lowell frame, the traveler changes during the break-in were completely eliminated. Spinning rings formed from cast iron with a ferric oxide-ferrosoferric oxide first coating and an outer layer of tin were installed on a Saco-Lowell frame. Each of the rings supported a carburized steel traveler. After the spinning frames were operated for 24 hours the rings were removed and inspected. No Wear was observed on the original travelers and they were placed back on the ring. The life of these travelers proved equal to the life of travelers subsequently installed. In addition, the spinning rings themselves provided long periods of use. In short, the effect of the break-in period was eliminated without adverse effect on the durability of the spinning ring.
The double coating system comprising an iron oxide with an anti-friction metal overlay has been applied to piston rings as well. In this instance, iron piston rings were given Fe O coatings by the process taught by Givens in United States Patent No. 2,23 6,728. Some of these oxide coated piston rings were plated with cadmium and others with tin. Both soft metals formed an itnegral bond with the oxide surfaces. Some of the double coated piston rings were installed in a test engine and rendered good performance.
The thickness of the double coating applied to a member will be determined, mainly, by the size of the article being coated and the application of such member. For example, 2" x 1" x /8 rings having an iron oxide coating varying from 0.00005"-0.0001 and an anti-friction metal overlay of 0.0002"-0.0003" have proven very satisfactory. The thickness of the iron oxide coating is controlled at least by the reaction temperature and time at such reaction temperature. The thickness of the anti-friction metal overlay is controlled at least by the current density of the bath and by the period of coating.
Although the preferred embodiment of this invention has been shown and described, changes and modifications can be made therein without departing from the scope of this invention and it is understood that the preceding description is illustrative only and not for the purpose of rendering this invention limited to the details illustrated or described except insofar as they are limited by the terms of the following claims.
What is claimed is:
1. A bearing member comprising a base portion formed from ferrous metal and having a wearing surface, a first coating intimately secured to at least a portion of said wearing surface and having a porous crystalline structure selected from the group consisting of ferric oxide, ferrosoferric oxide, a composite of ferric and ferrosoferric oxide and a composite of ferrous oxide and ferrosoferric oxide and a second anti-friction metallic coating intimately secured to said first coating at least at said portion of said wear surface selected from a group consisting of lead, copper, tin, cadmium and alloys thereof, whereby said anti-friction metallic coating is incompletely removed during initial operation of said bearing member.
2. A spinning ring comprising a base portion formed from ferrous metal and having an annular body portion and an annular flange formed coaxially and integrally with said spinning ring, said flange forming a wearing surface, a first coating intimately attached to said flange selected from a group consisting of ferric oxide, ferroso ferric oxide, a composite of ferric and ferrosoferric oxide and a composite of ferrous oxide and ferrosoferric oxide, a second anti-friction metallic coating deposited on said first coating to form an external surface on said spinning ring and covering the first coating on at least said flange, said second coating selected from a group consisting of lead, copper, tin, cadmium and alloys thereof, whereby said anti-friction metallic coating is incompletely removed during initial operation of said spinning ring.
References Cited UNITED STATES PATENTS 1,745,835 2/ 1930 Merrill 57-119 2,099,340 11/1937 Kautz 148-6.35 2,236,728 4/1941 Given 1486.35 2,268,868 1/1942 Given 1486.35 X 2,798,357 7/1957 Stahli 57-119 2,970,425 2/ 1961 Foard 57-119 2,983,563 5/1961 McLean et al 308-241 X 2,987,871 6/1961 -Foard 57120 3,118,272 1/1964 Clapp 57120 3,226,924 1/1966 Dalpiaz 57119 X FRANK J. COHEN, Primary Examiner.

Claims (2)

1. A BEARING MEMBER COMPRISING A BASE PORTION FORMED FROM FERROUS METAL AND HAVING A WEARING SURFACE, A FIRST COATING INTIMATELY SECURED TO AT LEAST A PORTION OF SAID WEARING SURFACE AND HAVING A POROUS CRYSTALINE STRUCTURE SELECTED FROM THE GROUP CONSISTING OF FERRIC OXIDE, FERROSOFERRIC OXIDE, A COMPOSITE OF FERRIC AND FERROSOFERRIC OXIDE AND A COMPOSITE OF FERROUS OXIDE AND FERROSOFERRIC OXIDE AND A SECOND ANTI-FRICTION METALLIC COATING INTIMATELY SECURED TO SAID FIRST COATING AT LEAST AT SAID PORTION OF SAID WEAR SURFACE SELECTED FROM A GROUP CONSISTING OF LEAD, COPPER, TIN, CADMIUM AND ALLOYS THEREOF, WHEREBY SAID ANTI-FRICTION METALLIC COATING IS INCOMPLETELY REMOVED DURING INITIAL OPERATION OF SAID BEARING MEMBER.
2. A SPINNING RING COMPRISING A BASE PORTION FORMED FROM FERROUS METAL AND HAVING AN ANNULAR BODY PORTION AND AN ANNULAR FLANGE FORMED COAXIALLY AND INTEGRALLY WITH SAID SPINNING RING, SAID FLANGE FORMING A WEARING SURFACE, A FIRST COATING INTIMATELY ATTACHED TO SAID FLANGE SELECTED FROM A GROUP CONSISTING OF FERRIC OXIDE, FERROSOFERRIC OXIDE, A COMPOSITE OF FERRIC AND FERROSOFERRIC OXIDE AND A COMPOSITE OF FERROUS OXIDE AND FERROSOFERRIC OXIDE A SECOND ANTI-FRICTION METALLIC COATING DEPOSITED ON SAID FIRST COATING TO FORM AN EXTERNAL SURFACE ON SAID SPINNING RING AND COVERING THE FIRST COATING ON AT LEAST SAID FLANGE, SAID SECOND COATING SELECTED FROM A GROUP CONSISTING OF LEAD, COPPER, TIN, CADMIUM AND ALLOYS THEREOF, WHEREBY SAID ANTI-FRICTION METALLIC COATING IS INCOMPLETELY REMOVED DURING INITIAL OPERATION OF SAID SPINNING RING.
US427741A 1964-12-24 1965-01-25 Bearing members having a plurality of coatings Expired - Lifetime US3343362A (en)

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US420883A US3421307A (en) 1964-12-24 1964-12-24 Bearing member having a composite coating
US427741A US3343362A (en) 1964-12-24 1965-01-25 Bearing members having a plurality of coatings
FR40689A FR1457861A (en) 1964-12-24 1965-12-02 Ferrous metal bearing member with an integrated layer of ferrous oxide and ferrosoferric oxide, particularly for rings on a spinning machine

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US420883A US3421307A (en) 1964-12-24 1964-12-24 Bearing member having a composite coating
US427741A US3343362A (en) 1964-12-24 1965-01-25 Bearing members having a plurality of coatings

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Cited By (10)

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US3922444A (en) * 1972-08-30 1975-11-25 Nippon Piston Ring Co Ltd Sliding member
US4072368A (en) * 1975-09-24 1978-02-07 Miba Gleitlager Aktiengesellschaft Sliding-surface bearing and process of manufacturing the same
US4110512A (en) * 1971-12-27 1978-08-29 Chrysler Corporation Iron oxide material and members for dry lubricated systems including the method of preparation therefor
US4308715A (en) * 1980-05-25 1982-01-05 Rieter Machine Works Ltd. Spinning ring made from steel for ring spinning and ring twisting machine
US4362012A (en) * 1979-08-24 1982-12-07 Societe Alsacienne De Constructions Mecaniques De Mulhouse Anti-balloon devices of spinning frames
US4683010A (en) * 1985-10-01 1987-07-28 Acs Industries, Inc. Compacted wire seal and method of forming same
US4698958A (en) * 1984-09-27 1987-10-13 Kanai Juyo Kogyo Co., Ltd. Ring for spinning and twisting machines
US5829240A (en) * 1997-03-17 1998-11-03 A. B. Carter, Inc. Spinning ring having improved traveler bearing surface
US5970698A (en) * 1996-11-14 1999-10-26 Howa Machinery, Ltd. Rotary spinning ring structure
US6360520B2 (en) 2000-01-14 2002-03-26 Ab Carter, Inc. Spinning ring having amorphous chromium bearing surface

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0811848B2 (en) * 1987-12-28 1996-02-07 金井 宏之 Ring for spinning machine
US6277214B1 (en) 1999-07-09 2001-08-21 Powertech Labs Inc. Protective iron oxide scale on heat-treated irons and steels
CN107420286B (en) * 2012-02-20 2019-10-08 松下电器产业株式会社 Slide unit and coolant compressor and freezer and air conditioner using it

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US2987871A (en) * 1958-02-17 1961-06-13 Kluttz Machine & Foundry Compa Spinning ring and method of making same
US3118272A (en) * 1962-06-08 1964-01-21 Powdered metal bearings
US3226924A (en) * 1964-02-04 1966-01-04 Carter Inc Ab Electrolessly plated textile ring traveler

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US2099340A (en) * 1934-06-28 1937-11-16 Republic Steel Corp Process of enameling
US2268868A (en) * 1940-04-06 1942-01-06 Perfect Cirele Company Bearing member
US2236728A (en) * 1940-05-01 1941-04-01 Perfect Circle Co Process of treating bearing members
US2798357A (en) * 1951-09-29 1957-07-09 Rieter Joh Jacob & Cie Ag Spinning ring
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US4110512A (en) * 1971-12-27 1978-08-29 Chrysler Corporation Iron oxide material and members for dry lubricated systems including the method of preparation therefor
US3922444A (en) * 1972-08-30 1975-11-25 Nippon Piston Ring Co Ltd Sliding member
US4072368A (en) * 1975-09-24 1978-02-07 Miba Gleitlager Aktiengesellschaft Sliding-surface bearing and process of manufacturing the same
US4362012A (en) * 1979-08-24 1982-12-07 Societe Alsacienne De Constructions Mecaniques De Mulhouse Anti-balloon devices of spinning frames
US4308715A (en) * 1980-05-25 1982-01-05 Rieter Machine Works Ltd. Spinning ring made from steel for ring spinning and ring twisting machine
US4698958A (en) * 1984-09-27 1987-10-13 Kanai Juyo Kogyo Co., Ltd. Ring for spinning and twisting machines
US4683010A (en) * 1985-10-01 1987-07-28 Acs Industries, Inc. Compacted wire seal and method of forming same
US5970698A (en) * 1996-11-14 1999-10-26 Howa Machinery, Ltd. Rotary spinning ring structure
US5829240A (en) * 1997-03-17 1998-11-03 A. B. Carter, Inc. Spinning ring having improved traveler bearing surface
US6360520B2 (en) 2000-01-14 2002-03-26 Ab Carter, Inc. Spinning ring having amorphous chromium bearing surface

Also Published As

Publication number Publication date
FR1457861A (en) 1966-11-04
US3421307A (en) 1969-01-14

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