US20090087126A1 - Bearings - Google Patents

Bearings Download PDF

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Publication number
US20090087126A1
US20090087126A1 US11/865,250 US86525007A US2009087126A1 US 20090087126 A1 US20090087126 A1 US 20090087126A1 US 86525007 A US86525007 A US 86525007A US 2009087126 A1 US2009087126 A1 US 2009087126A1
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US
United States
Prior art keywords
bearing
substrate
layer
lobes
portions
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.)
Abandoned
Application number
US11/865,250
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English (en)
Inventor
Timothy J. Hagan
Vincent J. DiMartino
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.)
Saint Gobain Performance Plastics Corp
Original Assignee
Saint Gobain Performance Plastics Corp
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 Saint Gobain Performance Plastics Corp filed Critical Saint Gobain Performance Plastics Corp
Priority to US11/865,250 priority Critical patent/US20090087126A1/en
Assigned to SAINT-GOBAIN PERFORMANCE PLASTICS CORPORATION reassignment SAINT-GOBAIN PERFORMANCE PLASTICS CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: DIMARTINO, VINCENT J., HAGAN, TIMOTHY J.
Priority to PCT/US2008/078105 priority patent/WO2009045953A1/en
Priority to CA2700405A priority patent/CA2700405A1/en
Priority to EP08836299.1A priority patent/EP2201256B1/en
Priority to MX2010003626A priority patent/MX2010003626A/es
Priority to CN2008801095694A priority patent/CN101809302B/zh
Priority to TW097137784A priority patent/TWI393824B/zh
Publication of US20090087126A1 publication Critical patent/US20090087126A1/en
Priority to US13/105,660 priority patent/US8491194B2/en
Abandoned legal-status Critical Current

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Classifications

    • 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
    • F16C33/20—Sliding surface consisting mainly of plastics
    • F16C33/201—Composition of the plastic
    • 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
    • F16C17/00—Sliding-contact bearings for exclusively rotary movement
    • F16C17/02—Sliding-contact bearings for exclusively rotary movement for radial load only
    • 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
    • F16C37/00—Cooling of bearings
    • F16C37/002—Cooling of bearings of fluid bearings

Definitions

  • the invention relates to bearings.
  • Bearings can provide convenient means for rotatably, pivotably or slidably fastening multiple members to one another in a low maintenance manner.
  • Applications for bearings include those that have continuous rotational movement, such as journals for supporting a driven shaft.
  • Bearings can also be used for applications that have repeated pivotal movement, such as automotive door hinges, door checks, brake and accelerator pedals. Additional applications include those that have repeated reciprocal movement, such as automotive shock absorbers and struts.
  • Bearings can also be used in lighter duty applications, such as multiple bar linkages used in the automotive industry for trunk deck lid and hood hinges.
  • Low maintenance bearings can include a variety of configurations, such as, for example, bushes or journal bearings, thrust bearings or washers, locating pads, valve port plates, and wearing components for a variety of mechanisms.
  • An example of a low maintenance a sliding bearing includes a metal support and a plastic layer.
  • the invention relates to bearings, such as those that can be used in high speed applications.
  • the invention features a bearing including a substrate having a first portion and a second portion thicker than the first portion, the second portion having a curved outer contour; and a first layer on an inner contour of the substrate.
  • the first layer can include a lubricious material, such as grease.
  • the invention features a bearing including a substrate having a first portion and a second portion thicker than the first portion, the second portion having a curved outer contour; and a first layer on the outer contour of the substrate.
  • the invention features a bearing including a substrate having an inner surface, a first portion and a second portion thicker than the first portion, the second portion extending linearly for at least 25% of a length of the substrate; and a first layer on the inner surface of the substrate.
  • FIG. 1 is a perspective view of an embodiment of a bearing.
  • FIG. 2 is a cross-sectional view of the bearing of FIG. 1 , taken along line 2 - 2 .
  • FIG. 3 is a diagram of an embodiment of a substrate.
  • FIG. 4 is a cross-sectional view of an embodiment of a bearing.
  • FIG. 5 is a cross-sectional view of an embodiment of a bearing.
  • FIG. 6 is a diagram of a system including a bearing and a motor.
  • a plain bearing 20 includes a cylindrical body 22 that defines a lumen 24 extending coaxially with a longitudinal axis (L) of the bearing.
  • bearing 20 can be placed in a housing, and lumen 24 can be used to receive, for example, a rotating shaft of a motor.
  • Body 22 includes (e.g., is formed of) multiple (as shown, three) unitarily formed layers that enhance the performance of bearing 20 .
  • body 22 includes a thermally conductive outer layer 26 that forms a cylindrical outer surface of bearing 20 , a substrate 28 , and a lubricious inner layer 30 that forms a cylindrical inner surface of the bearing.
  • the lubricious material reduces friction and allows bearing 20 to be used for high speed applications (such as electric motors, transmissions, and reciprocating pumps).
  • Thermally conductive outer layer 26 can reduce generation of heat during use.
  • Substrate 28 includes a plurality of lobes 32 that extend circumferentially and coaxially around longitudinal axis L. Substrate 28 provides bearing 20 with a mechanically strong support, and lobes 28 allow more thermally conductive material from outer layer 26 to be included in bearing 20 . As shown, lobes 32 are curved projections that extend radially outward away from longitudinal axis L. Referring to FIG. 3 , adjacent lobes 32 are spaced from each other and separated by a trough portion 33 . Each trough portion 33 has a thickness (T l ) that is less than a thickness (T l ) of a lobe adjacent to the trough portion 33 .
  • Each lobe 32 has an outer contour 34 having at least one curved portion or segment (such as a curved outermost portion, e.g., the outermost 25%, 10%, 5%, 2% of a maximum thickness of a lobe), and an inner contour 36 whose curvature tracks the curvature of lumen 24 .
  • outer contour 34 can include one or more curved portions that matches or substantially matches a portion of a circle, an ellipse, an oval, a parabola, or a non-linear and non-angular curve.
  • outer contour 34 includes one or more continuously curved portions in which two line segments (if any) on the outer contour cannot intersect at a point that is on the curved portion.
  • outer contour 34 has a radius of curvature ranging from approximately 0.5 mm to approximately 2.0 mm.
  • each trough portion 33 has a curved outer contour 35 .
  • outer contour 35 is concave, while outer contour 34 of lobe 32 is convex.
  • Outer contour 35 can include one or more curved portions that matches or substantially matches a portion of a circle, an ellipse, an oval, a parabola, or a non-linear and non-angular curve.
  • outer contour 35 includes one or more continuously curved portions in which two line segments (if any) on the outer contour cannot intersect at a point that is on the curved portion.
  • Outer contour 35 can have a radius of curvature that is less than, substantially equal to, or greater than a radius of curvature of outer contour 34 .
  • lobes 32 and substrate 28 can vary, depending on the intended application of bearing 20 .
  • a substrate can include one or more lobes, such as two to more than twelve lobes.
  • the number of lobes can be a function of, for example, the intended application for bearing 20 , the thicknesses of the layers in the bearing, the materials included in the bearing, the geometry and size of the bearing, and/or the geometry and size of the member (e.g., spinning shaft) to be used with the bearing.
  • Increasing the number of lobes can, for example, increase the surface area of the substrate that interacts with a housing and allow a higher load to be used with the bearing.
  • the number of lobes is determined by balancing the load requirements of the intended application and the reduction (e.g., minimization) of friction and heat generation.
  • the lobes can be equally or unequally distributed around longitudinal axis L. As shown in FIG. 1 , the lobes extend linearly and longitudinally parallel to longitudinal axis L for the entire length of substrate 28 , which, as shown, matches the longitudinal length (l) of bearing 20 .
  • the lobes extend for less than the entire longitudinal length (l) of bearing 20 , for example, from approximately 25% to approximately 100% of length (l), from approximately 50% to approximately 100% of length (l), or from approximately 75% to approximately 100% of length (l).
  • One or more lobes can extend continuously or discontinuously along length (l).
  • a bearing 20 ′ includes lobes 32 ′ of different dimensions. As shown, substrate 28 ′ includes four lobes 32 ′ and four thinner lobes 32 ′′.
  • Substrate 28 can include (e.g., be formed of) any material capable of providing bearing 20 with the mechanical and physical properties for the bearing to be used in its intended application.
  • substrate 28 can include one or more metals (such as aluminum), one or more alloys (such as steel, cold-rolled steel, stainless steel, conventional drawing quality sheet steel, and brass), one or more plastics, one or more ceramics, and/or one or more composites (such as one including glass and/or carbon fibers).
  • Substrate 28 can include only one homogeneous composition (such as an alloy or a composite), or two or more discrete portions of different compositions. For example, referring to FIG.
  • substrate 28 ′′ includes an inner layer 40 having a first composition (such as a steel), and an outer layer 42 having a second composition (such as a porous bronze) different from the first composition.
  • a substrate include composites from a family of materials known as NORGLIDE® (e.g., NORGLIDE® PRO XL, available from Saint-Gobain Performance Plastics). These composites can include, for example, a steel backing and/or a reinforced mesh, and a layer of filled or compounded PTFE.
  • the portions having different compositions can be arranged radially ( FIG. 5 ) or circumferentially (e.g., adjacent lobes or portions thereof can have different compositions).
  • the inner and outer surfaces of substrate 28 can be untreated or treated to enhance the physical and/or chemical properties of the substrate.
  • the surface(s) can be treated using techniques such as galvanizing, chromate or phosphate treatments, anodizing (e.g., for an aluminum substrate), laser melting or ablation, mechanical sandblasting and/or chemical pickling.
  • a surface can be modified using a discontinuous laser beam that selectively hits the surface and melts it over a relatively small area to create spaced craters.
  • the craters can enhance adhesion between substrate 28 and lubricious layer 30 .
  • Thermally conductive layer 26 can include (e.g., is formed of) one or more materials having a thermal conductivity equal to and/or greater than a thermal conductivity of a material included in substrate 28 .
  • the thermally conductive materials can have properties that allow layer 26 to be applied (e.g., laminated) to the material(s) included in substrate 28 .
  • thermally conductive layer 26 can include only one homogeneous composition, or two or more discrete portions of different compositions. The portions having different compositions can be arranged radially (e.g., FIG. 5 ) or circumferentially.
  • thermally conductive materials include compressed powdered metal (e.g., copper), compressed powdered alloys, and compressed composites having thermally conductive fibers (e.g., metal fibers).
  • bearing 20 does not include thermally conductive layer 26 or any material disposed on the outer surface (e.g., outer contour 34 or outer contour 35 ) of substrate 28 .
  • Lubricious layer 30 can include (e.g., be formed of) one or more lubricious materials, such as a material having a lower coefficient of friction than a material included in substrate 28 .
  • the lubricious materials can allow bearing 20 to be bored, broached or burnished to size after installation without reducing the performance of the bearing.
  • the lubricious materials can have properties that allow layer 30 to be applied (e.g., laminated) to the material(s) included in substrate 28 .
  • lubricious layer 30 can include only one homogeneous composition, or two or more discrete portions of different compositions. The portions having different compositions can be arranged radially (e.g., FIG. 5 ) or circumferentially.
  • Examples of materials in lubricious layer 30 include polymers or plastic materials, such as temperature tolerant polymer systems containing high melt temperature polymers.
  • Examples of polymeric materials include fluoropolymers (e.g., polytetrafluoroethylene (PTFE), fluorinated ethylene-propylene (FEP), polyvinylidene flouride (PVDF), polychlorotrifluoroethylene (PCTFE), ethylene-chlorotrifluoroethylene (ECTFE), perfluoroalkoxy polymer (PFA), and other materials disclosed in U.S. Pat. No.
  • PTFE polytetrafluoroethylene
  • FEP fluorinated ethylene-propylene
  • PVDF polyvinylidene flouride
  • PCTFE polychlorotrifluoroethylene
  • ECTFE ethylene-chlorotrifluoroethylene
  • PFA perfluoroalkoxy polymer
  • acetals polycarbonates, polyimides, polyetherimides, polyether ether ketones (PEEK), polyethylenes, polypropylenes, polysulfones (e.g., polyethersulfone), polyamides (Nylon), polyphenylene sulfides, polyurethanes, polyesters, polyphenylene oxides, PPS, PPS 0 2 , aromatic or aliphatic polyketone/ethers, PEI and blends and alloys thereof.
  • PEEK polyetherimides
  • PEEK polyether ether ketones
  • Polyethylenes polypropylenes
  • polysulfones e.g., polyethersulfone
  • polyamides Nylon
  • polyphenylene sulfides polyurethanes
  • polyesters polyphenylene oxides
  • PPS polyphenylene oxides
  • PPS PPS 0 2
  • aromatic or aliphatic polyketone/ethers PEI and blends and alloys thereof.
  • one or more additives are included in layer 30 .
  • the additives can affect characteristics of the material(s) in layer 30 , such as lubricity, mechanical strength, wear resistance thermal conductivity and electrical conductivity.
  • examples of additives include glass and/or carbon fiber, silicone, graphite, molybdenum disulfide, aromatic polyester, carbon particles, bronze, fluoropolymer and combinations thereof.
  • the additives can be present in from approximately 0.5 to approximately 49.5 volume percent.
  • materials in lubricious layers 30 include solid state materials (e.g., inorganic materials such as graphite and/or molybdenum disulfide) and viscous fluids (e.g., grease).
  • solid state materials e.g., inorganic materials such as graphite and/or molybdenum disulfide
  • viscous fluids e.g., grease
  • Bearing 20 can be fabricated using cladding and lamination techniques.
  • the substrate can be formed using cladding techniques in which heat and pressure are applied to form a unitary structure (e.g., a sheet).
  • Substrate 28 once formed, can be passed through a conventional calender roll having the negative of the selected pattern of lobes 32 , or through a series of gears.
  • Lubricious layer 30 and thermally conductive layer 26 can be subsequently applied to substrate 28 by laminating sheets of the selected material(s), such as PTFE.
  • the entire laminate can then be inserted into a conventional press under heat and pressure to form a unitary body (e.g., a sheet).
  • the body can then be formed into various application specific configurations using conventional techniques to yield bearing 20 .
  • the body can be formed into any number of bearing types, such as bushes or journal bearings, thrust washers, and skid plates.
  • Bushes or journal bearings can be formed by cutting the unitary body into strips. Each of these strips, in turn, can be formed (e.g., rolled) into hollow cylinders.
  • Certain bearings, such as cylindrical bearings, can be flanged using conventional techniques.
  • a bearing can be fabricated by forming a substrate into a selected configuration, such as, for example, a cylinder, prior to applying of the lubricious layer.
  • the substrate can be provided with lobes as described herein, and then fabricated into a cylinder.
  • the lubricious layer can be applied to the cylinder, such as, for example, by spray coating, painting or dipping.
  • Application of the lubricious layer can be performed before or after flanging one or both ends of the cylinder.
  • the substrate can be fabricated into a cylinder, by a conventional method such as hot or cold forming operations, including roll forming, piercing, drawing or extrusion processes to produce either seamed or seamless cylinders.
  • the lobes can be provided using, for example, a chemical etching process or laser treatment.
  • the lubricious layer can be applied to the cylinder as previously described.
  • a system 50 includes a housing 52 , a motor 54 having a rotatable rotor 54 in the housing, and bearing 20 in the housing.
  • bearing 20 is positioned between rotor 54 and housing 52 , specifically, with the rotor in lumen 24 of the bearing.
  • Bearing 20 is capable of reducing motor vibrations, which can result in quieter motor operation and increased motor life.
  • bearing 20 is used to replace bushings and ball bearings in electric motors, e.g., those under one horsepower.
  • the bearings described herein are used in applications in which a pivotable member (e.g., a shaft) is placed in a lumen of a bearing.
  • a bearing includes one or more intermediate layers between substrate 28 and inner layer 30 .
  • the intermediate layer can, for example, enhance adhesion or bonding between substrate 28 and layer 30 .
  • the intermediate layer can include, for example, an adhesive such as fluoropolymers such as PFA, MFA, ETFE, FEP, PCTFE, and PVDF, curing adhesives such as epoxy, polyimide adhesives, and lower temperature hot melts such as ethylene vinylacetate (EVA) and polyether/polyamide copolymer (Pebax®).
  • an adhesive such as fluoropolymers such as PFA, MFA, ETFE, FEP, PCTFE, and PVDF
  • curing adhesives such as epoxy, polyimide adhesives
  • lower temperature hot melts such as ethylene vinylacetate (EVA) and polyether/polyamide copolymer (Pebax®).
  • the curved lobes described herein can be used in combination with structures that are not curved, such as raised structures described in Woelki, U.S. Pat. No. 5,971,617.
  • the raised structures can include linear segments that intersect at a point on the outer contour of the structures.
  • lubricious layer 30 is perforated for additional lubrication by grease pockets disposed therein.

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Sliding-Contact Bearings (AREA)
  • Laminated Bodies (AREA)
US11/865,250 2007-10-01 2007-10-01 Bearings Abandoned US20090087126A1 (en)

Priority Applications (8)

Application Number Priority Date Filing Date Title
US11/865,250 US20090087126A1 (en) 2007-10-01 2007-10-01 Bearings
PCT/US2008/078105 WO2009045953A1 (en) 2007-10-01 2008-09-29 Bearings
CA2700405A CA2700405A1 (en) 2007-10-01 2008-09-29 Bearing with externally contoured cylindrical insert having lubricious inner surface
EP08836299.1A EP2201256B1 (en) 2007-10-01 2008-09-29 Bearing
MX2010003626A MX2010003626A (es) 2007-10-01 2008-09-29 Cojinetes.
CN2008801095694A CN101809302B (zh) 2007-10-01 2008-09-29 轴承及具有该轴承的系统
TW097137784A TWI393824B (zh) 2007-10-01 2008-10-01 軸承
US13/105,660 US8491194B2 (en) 2007-10-01 2011-05-11 Bearings

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US11/865,250 US20090087126A1 (en) 2007-10-01 2007-10-01 Bearings

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US13/105,660 Continuation US8491194B2 (en) 2007-10-01 2011-05-11 Bearings

Publications (1)

Publication Number Publication Date
US20090087126A1 true US20090087126A1 (en) 2009-04-02

Family

ID=40508488

Family Applications (2)

Application Number Title Priority Date Filing Date
US11/865,250 Abandoned US20090087126A1 (en) 2007-10-01 2007-10-01 Bearings
US13/105,660 Expired - Fee Related US8491194B2 (en) 2007-10-01 2011-05-11 Bearings

Family Applications After (1)

Application Number Title Priority Date Filing Date
US13/105,660 Expired - Fee Related US8491194B2 (en) 2007-10-01 2011-05-11 Bearings

Country Status (7)

Country Link
US (2) US20090087126A1 (zh)
EP (1) EP2201256B1 (zh)
CN (1) CN101809302B (zh)
CA (1) CA2700405A1 (zh)
MX (1) MX2010003626A (zh)
TW (1) TWI393824B (zh)
WO (1) WO2009045953A1 (zh)

Cited By (8)

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US20070234839A1 (en) * 2006-03-22 2007-10-11 Saint-Gobain Performance Plastics Corporation Bearing assemblies
US20110135232A1 (en) * 2009-11-10 2011-06-09 Saint-Gobain Performance Plastics Corporation Closed end bearing cup
US20110219907A1 (en) * 2008-10-01 2011-09-15 Thyssenkrupp Presta Ag Sliding sleeve
US8491194B2 (en) 2007-10-01 2013-07-23 Saint-Gobain Performance Plastics Corporation Bearings
CN105020267A (zh) * 2015-08-10 2015-11-04 大连三环复合材料技术开发有限公司 核主泵水润滑复合材料推力轴承
WO2017013192A1 (de) * 2015-07-21 2017-01-26 Deutsches Zentrum für Luft- und Raumfahrt e.V. Gleitlagervorrichtung
EP3343053A1 (en) * 2016-12-16 2018-07-04 General Electric Company Joint-less continuous plain journal bearing
US20180306240A1 (en) * 2017-04-19 2018-10-25 Seiko Instruments Inc. Enveloping layer-coated slide bearing and drive module

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CN203348081U (zh) * 2012-04-30 2013-12-18 伊顿公司 正排量泵组件
EP3188907B1 (en) 2014-09-02 2022-05-04 Saint-Gobain Performance Plastics Pampus GmbH Corrosion resistant bushing
DE102015209495A1 (de) * 2015-05-22 2016-11-24 Volkswagen Aktiengesellschaft Anordnung zum Dämpfen einer akustischen Kopplung und Lageranordnung mit einer solchen
CN106015315A (zh) * 2016-08-04 2016-10-12 江苏亚星波纹管有限公司 一种波纹管轴承装置
DE102017103940B4 (de) * 2017-02-24 2020-06-18 Vibracoustic Gmbh Gleitlager für ein Stützlager
US11209065B2 (en) 2017-08-09 2021-12-28 Vibracoustic Usa, Inc. Low torsion bushing and assembly
US11174895B2 (en) * 2019-04-30 2021-11-16 General Electric Company Bearing for a wind turbine drivetrain having an elastomer support

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WO2009045953A1 (en) 2009-04-09
EP2201256A1 (en) 2010-06-30
TWI393824B (zh) 2013-04-21
MX2010003626A (es) 2010-04-21
CA2700405A1 (en) 2009-04-09
CN101809302B (zh) 2012-11-28
EP2201256B1 (en) 2014-01-08
CN101809302A (zh) 2010-08-18
EP2201256A4 (en) 2011-12-28
US20110211780A1 (en) 2011-09-01
US8491194B2 (en) 2013-07-23

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