US3765978A - Method of making a low-friction fabric bearing - Google Patents
Method of making a low-friction fabric bearing Download PDFInfo
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- US3765978A US3765978A US00160661A US3765978DA US3765978A US 3765978 A US3765978 A US 3765978A US 00160661 A US00160661 A US 00160661A US 3765978D A US3765978D A US 3765978DA US 3765978 A US3765978 A US 3765978A
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- fabric
- filaments
- yarn
- tfe
- synthetic resin
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- 239000004744 fabric Substances 0.000 title claims abstract description 79
- 238000004519 manufacturing process Methods 0.000 title claims description 11
- 229920003002 synthetic resin Polymers 0.000 claims abstract description 21
- 239000000057 synthetic resin Substances 0.000 claims abstract description 21
- 229920005989 resin Polymers 0.000 claims abstract description 18
- 239000011347 resin Substances 0.000 claims abstract description 18
- 229920001778 nylon Polymers 0.000 claims abstract description 17
- 238000004513 sizing Methods 0.000 claims abstract description 17
- 239000004677 Nylon Substances 0.000 claims abstract description 16
- 238000010276 construction Methods 0.000 claims abstract description 7
- 238000005470 impregnation Methods 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 claims description 33
- 239000003795 chemical substances by application Substances 0.000 claims description 17
- 238000005406 washing Methods 0.000 claims description 15
- 229920000728 polyester Polymers 0.000 claims description 7
- 239000002904 solvent Substances 0.000 claims description 7
- 239000004593 Epoxy Substances 0.000 claims description 4
- 238000009835 boiling Methods 0.000 claims description 4
- 238000009954 braiding Methods 0.000 claims description 4
- 238000009940 knitting Methods 0.000 claims description 4
- ISWSIDIOOBJBQZ-UHFFFAOYSA-N phenol group Chemical group C1(=CC=CC=C1)O ISWSIDIOOBJBQZ-UHFFFAOYSA-N 0.000 claims description 4
- 238000009941 weaving Methods 0.000 claims description 4
- 239000004642 Polyimide Substances 0.000 claims description 3
- 229920001721 polyimide Polymers 0.000 claims description 3
- 238000002791 soaking Methods 0.000 claims description 3
- 238000007596 consolidation process Methods 0.000 claims description 2
- BFKJFAAPBSQJPD-UHFFFAOYSA-N tetrafluoroethene Chemical compound FC(F)=C(F)F BFKJFAAPBSQJPD-UHFFFAOYSA-N 0.000 description 32
- 229920000784 Nomex Polymers 0.000 description 13
- 239000004763 nomex Substances 0.000 description 13
- 206010037660 Pyrexia Diseases 0.000 description 3
- 239000004809 Teflon Substances 0.000 description 3
- 229920006362 Teflon® Polymers 0.000 description 3
- 238000001035 drying Methods 0.000 description 3
- 239000000835 fiber Substances 0.000 description 3
- 239000000853 adhesive Substances 0.000 description 2
- 230000001070 adhesive effect Effects 0.000 description 2
- 230000015556 catabolic process Effects 0.000 description 2
- 230000006870 function Effects 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 238000003825 pressing Methods 0.000 description 2
- 238000005096 rolling process Methods 0.000 description 2
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 2
- 238000006243 chemical reaction Methods 0.000 description 1
- 239000011248 coating agent Substances 0.000 description 1
- 238000000576 coating method Methods 0.000 description 1
- 238000005520 cutting process Methods 0.000 description 1
- 238000006731 degradation reaction Methods 0.000 description 1
- 230000000593 degrading effect Effects 0.000 description 1
- 239000000945 filler Substances 0.000 description 1
- 239000003365 glass fiber Substances 0.000 description 1
- 238000010438 heat treatment Methods 0.000 description 1
- 239000011159 matrix material Substances 0.000 description 1
- 238000007431 microscopic evaluation Methods 0.000 description 1
- 239000006082 mold release agent Substances 0.000 description 1
- 238000000465 moulding Methods 0.000 description 1
- 230000035515 penetration Effects 0.000 description 1
- 230000000704 physical effect Effects 0.000 description 1
- 238000009877 rendering Methods 0.000 description 1
- 230000000717 retained effect Effects 0.000 description 1
- -1 vinyl alcohols Chemical class 0.000 description 1
- 229920002554 vinyl polymer Polymers 0.000 description 1
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C33/00—Parts of bearings; Special methods for making bearings or parts thereof
- F16C33/02—Parts of sliding-contact bearings
- F16C33/04—Brasses; Bushes; Linings
- F16C33/20—Sliding surface consisting mainly of plastics
- F16C33/201—Composition of the plastic
-
- D—TEXTILES; PAPER
- D02—YARNS; MECHANICAL FINISHING OF YARNS OR ROPES; WARPING OR BEAMING
- D02G—CRIMPING OR CURLING FIBRES, FILAMENTS, THREADS, OR YARNS; YARNS OR THREADS
- D02G3/00—Yarns or threads, e.g. fancy yarns; Processes or apparatus for the production thereof, not otherwise provided for
- D02G3/44—Yarns or threads characterised by the purpose for which they are designed
- D02G3/447—Yarns or threads for specific use in general industrial applications, e.g. as filters or reinforcement
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/249921—Web or sheet containing structurally defined element or component
- Y10T428/249922—Embodying intertwined or helical component[s]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2922—Nonlinear [e.g., crimped, coiled, etc.]
- Y10T428/2925—Helical or coiled
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/2936—Wound or wrapped core or coating [i.e., spiral or helical]
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/2964—Artificial fiber or filament
- Y10T428/2967—Synthetic resin or polymer
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/2964—Artificial fiber or filament
- Y10T428/2967—Synthetic resin or polymer
- Y10T428/2969—Polyamide, polyimide or polyester
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T428/00—Stock material or miscellaneous articles
- Y10T428/29—Coated or structually defined flake, particle, cell, strand, strand portion, rod, filament, macroscopic fiber or mass thereof
- Y10T428/2913—Rod, strand, filament or fiber
- Y10T428/2933—Coated or with bond, impregnation or core
- Y10T428/2971—Impregnation
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
- Y10T442/20—Coated or impregnated woven, knit, or nonwoven fabric which is not [a] associated with another preformed layer or fiber layer or, [b] with respect to woven and knit, characterized, respectively, by a particular or differential weave or knit, wherein the coating or impregnation is neither a foamed material nor a free metal or alloy layer
- Y10T442/2008—Fabric composed of a fiber or strand which is of specific structural definition
Definitions
- ABSTRACT Improved wear and load-carrying properties result for a resin-impregnated fabric bearing wherein the bearing surface includes, as the most significant fabric component, a yarn which is a compounded bundle of sized TFE filaments and sized filaments of hightemperature nylon, in the proportion of at least no more than 50 percent TFE by volume.
- the yarn is loosely twisted, to the extent that after construction of a fabric with said yarn, the yarn is fully washable, to remove the sizing, down to the innermost filaments. This enables full impregnation of the fabric with synthetic resin, and curing in substantially intimate and continuous and void-free relation of the resin to all filaments within the yarn of the fabric.
- TFE tetrafluoroethylene
- Another object is to provide an improved yarn for use as the low-friction component of a bearing of the character indicated.
- a further object is to provide a method and means whereby increased body density is provided in support material for low-friction fibers at the bearing surface.
- a still further object is to meet the above objects with greater load-bearing capacity, longer-wear performance and capability of operation at higher temperatures than heretofore.
- a specific object is to provide increased support for low-friction fibers at the bearing surface, whereby TFE filaments are better retained against rolling to the point of breakage.
- FIG. 1 is an enlarged simplified fragmentary view in perspective to illustrate a yarn of the invention
- FIGS. 2 and 3 are similar simplified and enlarged fragmentary sectional views through part of a bundle of filaments in yarn of the invention, at different stages of a method of the invention;
- FIG. 4 is an even more greatly enlarged sectional view through part of a bearing of the invention.
- FIG. 5 is a simplified longitudinal sectional view of a complete bearing embodying the invention.
- the invention contemplates major reliance upon filaments of high-temperature nylon to function with TFE filaments in the yarn which is compounded for use as the low-friction bearing surface in a fabric bearing, the bearing being completed and consolidated by a cured synthetic resin.
- the nylon provides high strength and stability at elevated temperatures and is present in the yarn to the extent of at least 50 percent by volume of all filamentary components (including the TFE); preferably, the TFE filaments are present to the extent of 20 to 30 percent by volume.
- the filaments of the yarn be relatively loose and that they be subjected to as little twist as possible, consistent with an ability to handle the yarn, as in the process of constructing a bearing fabric in which said yarn appears as the major component of the bearing-surface material, on at least one side of the fabric.
- the filaments to be compounded into the yarn are supplied with a very thin sizing agent or coating which simplifies handling in the construction of a fabric. It is difficult to show the dimensional significance of this coat, and in the past its presence has been neglected.
- the sizing coat on commercially available filaments e.g., of TFE, or of high-temperature nylon
- curing temperatures for the synthetic impregnating resin are such as to generate fine bubbles or otherwise to react with the sizing agent.
- the product of such reaction e.g., gas bubbles generated upon heating sizing agents containing vinyl alcohols, becomes a'permanent part of the cured resin in the immediate vicinity of the filament to be supported. Not only is the density of resin thereby reduced at and near the bearing surface, but filament support and entrapment by the resin are materially degraded.
- the first four figures illustrate the foregoing on a simplified basis, for the case of yarn made of a bundle 10 of continuous sized TFE filaments, loosely twisted with a bundle ll of continuous sized filaments of hightemperature nylon (FIG. 1). This is the yarn which becomes the significant bearing-surface component, whether the fabric is braided, knitted or woven.
- FIG. 2 illustrates, with great and obvious exaggeration, the sizing coat 12 for each filament 13 in a yarn bundle.
- the coated filaments are not drawn tight, thanks to the bare minimum of twist, thus rendering the bundle readily susceptable to washing in a solvent for the sizing agent. Washing thoroughly removes the sizing agent, allowing full synthetic-resin penetration, as suggested at 14 in FIG. 3.
- FIG. 4 such a relationship appears in greater detail, illustrating that TFE filaments (13') and high-temperature nylon filaments (13”) both appear at the bearing surface 15, the contour of which depends upon that of a contour-forming surface 16; surface 16 is seen as part of a molding element 17 to which the fabric is conformed in producing the desired bearing surface 15.
- a satin-weave fabric, with 4:1 face, is produced using a multi-component warp yarn of the invention, and a filling yarn of continuous-filament, type 430 Nomex, the latter being a designation by the EL duPont Company for a particular one of its high-temperature nylons.
- the filling yarn is strictly described, for each end, as 200/100/38, of the type 430 Nomex; i.e., ZOO-denier Nomex yarn, consisting of 100 filaments, said yarn being twisted three times per inch.
- the warp yarn is strictly described as one end of 400/60/0 Teflon* (du- Pont Company trademark for its TFE filament.) and two ends of 200/100/0 type 430 Nomex; in other words, the TFE end comprises 400-denier TFE yarn with 60 filaments, and with zero twist, while the two Nomex ends are each as described for the filler, but with zero twist.
- the components of the warp yarn are then twisted three turns per inch.
- the sectional areas of the TFE filaments and Nomex filaments in the warp yarn are chosen to present about 25 percent TFE at the bearing surface, the rest of the bearing-surface filaments being Nomex.
- the fabric After weaving, the fabric is thoroughly washed in boiling water to remove the sizing, should the sizing happen to be water-soluble. Then after appropriate rinsing, drying and pressing, the fabric is cut and applied as the liner 20 of a plane spherical bearing (see FIG.
- the inner ring 21 is a spherical ball which is first coated with a suitable moldrelease agent.
- the outer ring 22 is deformable and ultimately has a spherical bore as shown, but this is initially a straight cylindrical bore into which is inserted a cutting from the washed fabric, suitably coated with an uncured synthetic-resin adhesive; the adhesive may be a phenolic, epoxy, fluroethylene-propylenc (FEP), or polyimide. Ring deformation, bonding and curing may proceed generally as described in Litsky U.S. Pat. No. 3,303,557.
- the completed bearing exhibits superior performance, exceeding that of all-Teflon surfaced bearings in the important respects of maximum load, life (i.e., low wear) under load, and in general a higher upper temperature limit for satisfactory operation, the latter feature being a function of the synthetic resin and of the non Teflon yarns or yarn components.
- the bearing fabric is again a satin weave, differing from Example One only in the use of a polyester filling rather than a Nomex filling.
- the filling yarn for the back comprises one end, 60/2 cotton-count spun continuous-filament polyester, known as Kodel* (Kodel is a trademark of the Eastman Kodak Company for its polyester fiber.) No. IV, high tenacity, Type 421, 1 A denier.
- the fabric is washed thoroughly in boiling water to remove all size, and then dried and pressed before assembly into a bearing. Drying proceeds at 325F for minutes in an air-circulating oven, to accomplish a heat soak and fabric shrink, within the curing temperature of the synthetic resin (in this case, phenolic), so as to avoid or materially reduce shrinking during the resin cure.
- the synthetic resin in this case, phenolic
- EXAMPLE THREE The bearing fabric is again a satin weave, differing from the foregoing only in the use of glass-fiber yarn as the filling. This filling is described as one end ECE 450% Fiberglas yarn. Washing and finishing are as described for Example One.
- the bearing fabric is a tubular braid, of yarns constructed generally as described for the warp yarn of Example One, the same being cut to length and applied to a mandrel of desired contour, coated with a release agent, and the braid is backed by a Fiberglas-epoxy matrix, as described in greater detail in copending Matt, et al. application Ser. No. 94,091, filed Dec. 1, 1970, now US. Pat. No. 3,692,375. The size is removed after braiding and before application to the mandrel.
- the bearing fabric is a knitted tube, conventionally fabricated of yarns generally as described for the warp yarn of Example One, the same being cut to length, applied to a mandrel, and backed and consolidated as for Example Four. Again, size is removed after knitting and before application to the mandrel.
- the described yarns, fabrics and bearings will be seen to achieve all stated objects, with superior results. And, the particular examples are purely illustrative, in that other combinations may be used within the invention.
- the particular advantages are that the Nomex filaments substantially improve wear-resistance. The removal of sizing from the fabric assures enhanced resin density, for greater bonding to the Nomex and therefore better localized support of TFE filaments exposed at the bearing surface. If still further bonding to all filaments is desired, the TFE filaments should be etched.
- TFE filaments are realized by the time the proportion of TFE at the bearing surface has reached 50 percent; in fact, when the added strength of the combining Nomex is taken into account, the best results are achieved for a TFE proportion of 20 to 30 percent by volume, as in the examples presently given.
- the method of making a low-friction bearing surface which comprises selecting a loosely twisted yarn consisting of sized TFE filaments and of hightemperature nylon filaments, constructing a fabric with said yarn as the major component on at least one side,
- washing step is performed at a selected elevated temperature in the range up to the boiling condition of the washing agent, whereby washing is accompanied by a controlled degree of fabric shrinkage prior to resin-impregnation and cure.
- said yarn comprises a filament bundle twisted to an extent not substantially exceeding three twists per inch.
- TFE filaments and high-temperature nylon filaments are in the proportion of at least no more than 50 percent TFE by volume.
- TFE filaments and high-temperature nylon filaments are in the proportion of 20 to 30 percent TFE by volume.
- the method of making a low-friction fabric bearing surface which comprises selecting a loosely twisted yarn consisting of continuous TFE filaments and of continuous high-temperature nylon filaments, constructing a fabric with said yarn as the major component on at least one side, said fabric including a filamentary polyester as a component, preshrinking the fabric by heat-soaking the same under predetermined conditions of elevated temperature and time within substantially the manufacturers specified soak limits for the polyester, impregnating the fabric with an uncured synthetic resin selected for cure temperature within the predetermined elevated heat-soak temperature, conforming said one side to a desired bearingsurface contour, and curing the resin while the fabric is thus conformed.
- the method of making a low-friction bearing fabric which comprises selecting a loosely twisted yarn comprising sized TFE filaments and high-temperature nylon filaments as the most predominant components, constructing a fabric with said yarn as the major component on at least one side, and washing the fabric in sizing-agent solvent to remove sizing, whereby when said one side of said fabric is later embodied in a bearing surface potted with a synthetic resin, the resin is induced to flow into and throughout the cleaned and loose yarn bundles, for substantially intimate and continuous and void-free consolidation therewith.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Textile Engineering (AREA)
- Sliding-Contact Bearings (AREA)
- Treatments For Attaching Organic Compounds To Fibrous Goods (AREA)
- Laminated Bodies (AREA)
- Manufacture Of Macromolecular Shaped Articles (AREA)
- Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
- Woven Fabrics (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Improved wear and load-carrying properties result for a resinimpregnated fabric bearing wherein the bearing surface includes, as the most significant fabric component, a yarn which is a compounded bundle of sized TFE filaments and sized filaments of high-temperature nylon, in the proportion of at least no more than 50 percent TFE by volume. The yarn is loosely twisted, to the extent that after construction of a fabric with said yarn, the yarn is fully washable, to remove the sizing, down to the innermost filaments. This enables full impregnation of the fabric with synthetic resin, and curing in substantially intimate and continuous and void-free relation of the resin to all filaments within the yarn of the fabric.
Description
United States Patent [191 Matt [ METHOD OF MAKING A LOW-FRICTION FABRIC BEARING [75] Inventor: Richard J. Matt, Simsbury, Conn.
[73] Assignee: Textron Inc., Providence, R1.
22 Filed: July 8, 1971 21 Appl. No.: 160,661
[56] References Cited UNITED STATES PATENTS 2,953,418 9/1960 Runton et a]. 156/85 X 3,000,076 9/1961 Runton et a]. 308/238 2,525,476 10/1950 Chase et al. 28/75 X 3,093,504 6/1963 Bode 28/75 [451 Oct. 16, 1973 Primary Examiner-William A. Powell Attorney-Sandoe, Hopgood & Calimafde [57] ABSTRACT Improved wear and load-carrying properties result for a resin-impregnated fabric bearing wherein the bearing surface includes, as the most significant fabric component, a yarn which is a compounded bundle of sized TFE filaments and sized filaments of hightemperature nylon, in the proportion of at least no more than 50 percent TFE by volume. The yarn is loosely twisted, to the extent that after construction of a fabric with said yarn, the yarn is fully washable, to remove the sizing, down to the innermost filaments. This enables full impregnation of the fabric with synthetic resin, and curing in substantially intimate and continuous and void-free relation of the resin to all filaments within the yarn of the fabric.
18 Claims, 5 Drawing Figures METHOD OF MAKING A LOW-FRICTION FABRIC BEARING This invention relates to low-friction fabric bearings, to the method of making the same, and to the yarn from which the fabric is made.
Low-friction fabric bearings in use today employ tetrafluoroethylene (TFE) filaments as the low-friction component but are subject to certain limitations which curtail the range of use. For example, maximum or excessive loads are accompanied by undue wear and rapid breakdown. And maximum operating temperature is unduly limited, due to further mechanical degradation under load or at elevated temperature. It is believed that many of these undesirable limitations arise from the assumption that a preponderance of TFE is required at the bearing surface.
It is, accordingly, an object of the invention to provide an improved bearing construction of the character indicated, and an improved method of making the same.
Another object is to provide an improved yarn for use as the low-friction component of a bearing of the character indicated.
A further object is to provide a method and means whereby increased body density is provided in support material for low-friction fibers at the bearing surface.
A still further object is to meet the above objects with greater load-bearing capacity, longer-wear performance and capability of operation at higher temperatures than heretofore.
A specific object is to provide increased support for low-friction fibers at the bearing surface, whereby TFE filaments are better retained against rolling to the point of breakage.
It is a general object to achieve the foregoing objects with a structure which is inherently relatively economical to manufacture, which is at least equal to the performance of present high-quality bearings within their limited range of use, and which extends beyond present bearings the range of performance in regard to useful life, maximum load and maximum elevated operating temperature.
Other objects and various further features of novelty and invention will be pointed out or will occur to those skilled in the art from a reading of the following specification in conjunction with the accompanyiny drawing.
In said drawing, which shows, for illustrative purposes only, preferred features of the invention:
FIG. 1 is an enlarged simplified fragmentary view in perspective to illustrate a yarn of the invention;
FIGS. 2 and 3 are similar simplified and enlarged fragmentary sectional views through part of a bundle of filaments in yarn of the invention, at different stages of a method of the invention;
FIG. 4 is an even more greatly enlarged sectional view through part of a bearing of the invention; and
FIG. 5 is a simplified longitudinal sectional view of a complete bearing embodying the invention.
The invention contemplates major reliance upon filaments of high-temperature nylon to function with TFE filaments in the yarn which is compounded for use as the low-friction bearing surface in a fabric bearing, the bearing being completed and consolidated by a cured synthetic resin. The nylon provides high strength and stability at elevated temperatures and is present in the yarn to the extent of at least 50 percent by volume of all filamentary components (including the TFE); preferably, the TFE filaments are present to the extent of 20 to 30 percent by volume. It is of importance to the invention that the filaments of the yarn be relatively loose and that they be subjected to as little twist as possible, consistent with an ability to handle the yarn, as in the process of constructing a bearing fabric in which said yarn appears as the major component of the bearing-surface material, on at least one side of the fabric. conventionally, the filaments to be compounded into the yarn are supplied with a very thin sizing agent or coating which simplifies handling in the construction of a fabric. It is difficult to show the dimensional significance of this coat, and in the past its presence has been neglected. I have discovered, however, that the sizing coat on commercially available filaments, e.g., of TFE, or of high-temperature nylon, is an important factor to be reckoned with, in that curing temperatures for the synthetic impregnating resin are such as to generate fine bubbles or otherwise to react with the sizing agent. The product of such reaction, e.g., gas bubbles generated upon heating sizing agents containing vinyl alcohols, becomes a'permanent part of the cured resin in the immediate vicinity of the filament to be supported. Not only is the density of resin thereby reduced at and near the bearing surface, but filament support and entrapment by the resin are materially degraded.
Now, by providing such yarn as a loose combination, i.e., with little or no twist, e.g., one to three twists per inch, I assure that the innermost filaments of the yarn are loose and accessible, even after performing the braiding, knitting or weaving operations by which the bearing fabric is constructed. Due to the loose nature of the yarn, even after fabric construction, I find that it is possible to thoroughly wash off the sizing agents, using a suitable solvent for the sizing agent. Washing produces a limp fabric, with even more voids within the yarn strands, and cleansed down to the very walls of the individual filaments. I have found a vastly greater affinity of the yarn filaments for liquid synthetic resin, after such washing, drying and also pressing the fabric. 1 can only surmise that the cleansed filaments establish plural capillary paths which, due to the small degree of twist, readily wick or induce the flow of liquid resin to the very core of the yarn, in intimate, continuous and voidfree relation with all filaments thereof; at least, this is my observation, using high-power microscopic analysis. Such analysis confirms unusual resin-rich support for all filaments, providing unusually high density at and near the bearing surface.
The first four figures illustrate the foregoing on a simplified basis, for the case of yarn made of a bundle 10 of continuous sized TFE filaments, loosely twisted with a bundle ll of continuous sized filaments of hightemperature nylon (FIG. 1). This is the yarn which becomes the significant bearing-surface component, whether the fabric is braided, knitted or woven.
FIG. 2 illustrates, with great and obvious exaggeration, the sizing coat 12 for each filament 13 in a yarn bundle. The coated filaments are not drawn tight, thanks to the bare minimum of twist, thus rendering the bundle readily susceptable to washing in a solvent for the sizing agent. Washing thoroughly removes the sizing agent, allowing full synthetic-resin penetration, as suggested at 14 in FIG. 3. In FIG. 4, such a relationship appears in greater detail, illustrating that TFE filaments (13') and high-temperature nylon filaments (13") both appear at the bearing surface 15, the contour of which depends upon that of a contour-forming surface 16; surface 16 is seen as part of a molding element 17 to which the fabric is conformed in producing the desired bearing surface 15.
Several illustrative examples of the use of my invention will be given.
EXAMPLE ONE A satin-weave fabric, with 4:1 face, is produced using a multi-component warp yarn of the invention, and a filling yarn of continuous-filament, type 430 Nomex, the latter being a designation by the EL duPont Company for a particular one of its high-temperature nylons. The filling yarn is strictly described, for each end, as 200/100/38, of the type 430 Nomex; i.e., ZOO-denier Nomex yarn, consisting of 100 filaments, said yarn being twisted three times per inch. The warp yarn is strictly described as one end of 400/60/0 Teflon* (du- Pont Company trademark for its TFE filament.) and two ends of 200/100/0 type 430 Nomex; in other words, the TFE end comprises 400-denier TFE yarn with 60 filaments, and with zero twist, while the two Nomex ends are each as described for the filler, but with zero twist. The components of the warp yarn are then twisted three turns per inch. The sectional areas of the TFE filaments and Nomex filaments in the warp yarn are chosen to present about 25 percent TFE at the bearing surface, the rest of the bearing-surface filaments being Nomex.
After weaving, the fabric is thoroughly washed in boiling water to remove the sizing, should the sizing happen to be water-soluble. Then after appropriate rinsing, drying and pressing, the fabric is cut and applied as the liner 20 of a plane spherical bearing (see FIG.
In making the bearing of FIG. 5, the inner ring 21 is a spherical ball which is first coated with a suitable moldrelease agent. The outer ring 22 is deformable and ultimately has a spherical bore as shown, but this is initially a straight cylindrical bore into which is inserted a cutting from the washed fabric, suitably coated with an uncured synthetic-resin adhesive; the adhesive may be a phenolic, epoxy, fluroethylene-propylenc (FEP), or polyimide. Ring deformation, bonding and curing may proceed generally as described in Litsky U.S. Pat. No. 3,303,557.
The completed bearing exhibits superior performance, exceeding that of all-Teflon surfaced bearings in the important respects of maximum load, life (i.e., low wear) under load, and in general a higher upper temperature limit for satisfactory operation, the latter feature being a function of the synthetic resin and of the non Teflon yarns or yarn components.
EXAMPLE TWO The bearing fabric is again a satin weave, differing from Example One only in the use of a polyester filling rather than a Nomex filling. The filling yarn for the back comprises one end, 60/2 cotton-count spun continuous-filament polyester, known as Kodel* (Kodel is a trademark of the Eastman Kodak Company for its polyester fiber.) No. IV, high tenacity, Type 421, 1 A denier. The fabric is washed thoroughly in boiling water to remove all size, and then dried and pressed before assembly into a bearing. Drying proceeds at 325F for minutes in an air-circulating oven, to accomplish a heat soak and fabric shrink, within the curing temperature of the synthetic resin (in this case, phenolic), so as to avoid or materially reduce shrinking during the resin cure.
EXAMPLE THREE The bearing fabric is again a satin weave, differing from the foregoing only in the use of glass-fiber yarn as the filling. This filling is described as one end ECE 450% Fiberglas yarn. Washing and finishing are as described for Example One.
EXAMPLE FOUR The bearing fabric is a tubular braid, of yarns constructed generally as described for the warp yarn of Example One, the same being cut to length and applied to a mandrel of desired contour, coated with a release agent, and the braid is backed by a Fiberglas-epoxy matrix, as described in greater detail in copending Matt, et al. application Ser. No. 94,091, filed Dec. 1, 1970, now US. Pat. No. 3,692,375. The size is removed after braiding and before application to the mandrel.
EXAMPLE FIVE The bearing fabric is a knitted tube, conventionally fabricated of yarns generally as described for the warp yarn of Example One, the same being cut to length, applied to a mandrel, and backed and consolidated as for Example Four. Again, size is removed after knitting and before application to the mandrel.
The described yarns, fabrics and bearings will be seen to achieve all stated objects, with superior results. And, the particular examples are purely illustrative, in that other combinations may be used within the invention. The particular advantages are that the Nomex filaments substantially improve wear-resistance. The removal of sizing from the fabric assures enhanced resin density, for greater bonding to the Nomex and therefore better localized support of TFE filaments exposed at the bearing surface. If still further bonding to all filaments is desired, the TFE filaments should be etched.
In spite of the predominant use of Nomex at the hearing surface, the presence of TFE enables a low coefficient of friction (0.02 to 0.08). Low wear is attributed to ability of the support resin to prevent TFE filaments from rolling and necking down to a pointwhere they might otherwise break or crumble. And the indicated loose twist enables full washing of all filaments, for highly effective resin impregnation. The substantial use of Nomex enables high strength and bondability, without noticeably degrading the friction coefficient, with good physical properties at elevated temperatures up to 450F.
Stated in other words, I have found that the best of the low-friction properties of TFE filaments are realized by the time the proportion of TFE at the bearing surface has reached 50 percent; in fact, when the added strength of the combining Nomex is taken into account, the best results are achieved for a TFE proportion of 20 to 30 percent by volume, as in the examples presently given.
What is claimed is:
1. The method of making a low-friction bearing surface, which comprises selecting a loosely twisted yarn consisting of sized TFE filaments and of hightemperature nylon filaments, constructing a fabric with said yarn as the major component on at least one side,
washing the fabric in sizing-agent solvent to remove sizing, impregnating the fabric with an uncured synthetic resin, whereby the resin is induced to flow into and throughout the loose and clean yarn bundles of the fabric, conforming said one side to a desired bearingsurface contour, and curing the resin while the fabric is thus conformed.
2. The method of claim 1 in which the synthetic resin is FEP.
3. The method of claim 1 in which the synthetic resin is a phenolic.
4. The method of claim 1 in which the synthetic resin is an epoxy.
5. The method of claim 1 in which the synthetic resin is a polyimide.
6. The method of claim 1 in which the washing step is performed at a selected elevated temperature in the range up to the boiling condition of the washing agent, whereby washing is accompanied by a controlled degree of fabric shrinkage prior to resin-impregnation and cure.
7. The method according to claim 1 in which a mold element is selected with a mold surface of said contour, to which said fabric side is applied for contour conformance, said mold surface being coated with a release agent prior to fabric application thereto.
8. The method of claim 1 wherein said filaments are substantially continuous.
9. The method of claim 1 wherein said yarn comprises a filament bundle twisted to an extent not substantially exceeding three twists per inch.
10. The method of claim 1 wherein said TFE filaments are etched filaments.
l l. The method of claim 1 wherein said fabric is constructed by braiding.
12. The method of claim 1 wherein said fabric is constructed by knitting.
13. The method of claim 1 wherein said fabric is constructed by weaving.
14. The method of claim 1 in which the TFE filaments and high-temperature nylon filaments are in the proportion of at least no more than 50 percent TFE by volume.
15. The method of claim 14 in which the TFE filaments and high-temperature nylon filaments are in the proportion of 20 to 30 percent TFE by volume.
16. The method of making a low-friction fabric bearing surface, which comprises selecting a loosely twisted yarn consisting of continuous TFE filaments and of continuous high-temperature nylon filaments, constructing a fabric with said yarn as the major component on at least one side, said fabric including a filamentary polyester as a component, preshrinking the fabric by heat-soaking the same under predetermined conditions of elevated temperature and time within substantially the manufacturers specified soak limits for the polyester, impregnating the fabric with an uncured synthetic resin selected for cure temperature within the predetermined elevated heat-soak temperature, conforming said one side to a desired bearingsurface contour, and curing the resin while the fabric is thus conformed.
17. The method of claim 16 in which said filaments are sized prior to fabric construction, and in which the fabric is washed in sizing-agent solvent prior to heatsoaking.
18. The method of making a low-friction bearing fabric, which comprises selecting a loosely twisted yarn comprising sized TFE filaments and high-temperature nylon filaments as the most predominant components, constructing a fabric with said yarn as the major component on at least one side, and washing the fabric in sizing-agent solvent to remove sizing, whereby when said one side of said fabric is later embodied in a bearing surface potted with a synthetic resin, the resin is induced to flow into and throughout the cleaned and loose yarn bundles, for substantially intimate and continuous and void-free consolidation therewith.
Claims (17)
- 2. The method of claim 1 in which the synthetic resin is FEP.
- 3. The method of claim 1, in which the synthetic resin is a phenolic.
- 4. The method of claim 1, in which the synthetic resin is an epoxy.
- 5. The method of claim 1, in which the synthetic resin is a polyimide.
- 6. The method of claim 1, in which the washing step is performed at a selected eleVated temperature in the range up to the boiling condition of the washing agent, whereby washing is accompanied by a controlled degree of fabric shrinkage prior to resin-impregnation and cure.
- 7. The method according to claim 1, in which a mold element is selected with a mold surface of said contour, to which said fabric side is applied for contour conformance, said mold surface being coated with a release agent prior to fabric application thereto.
- 8. The method of claim 1, wherein said filaments are substantially continuous.
- 9. The method of claim 1, wherein said yarn comprises a filament bundle twisted to an extent not substantially exceeding three twists per inch.
- 10. The method of claim 1, wherein said TFE filaments are etched filaments.
- 11. The method of claim 1, wherein said fabric is constructed by braiding.
- 12. The method of claim 1, wherein said fabric is constructed by knitting.
- 13. The method of claim 1, wherein said fabric is constructed by weaving.
- 14. The method of claim 1, in which the TFE filaments and high-temperature nylon filaments are in the proportion of at least no more than 50 percent TFE by volume.
- 15. The method of claim 14 in which the TFE filaments and high-temperature nylon filaments are in the proportion of 20 to 30 percent TFE by volume.
- 16. The method of making a low-friction fabric bearing surface, which comprises selecting a loosely twisted yarn consisting of continuous TFE filaments and of continuous high-temperature nylon filaments, constructing a fabric with said yarn as the major component on at least one side, said fabric including a filamentary polyester as a component, preshrinking the fabric by heat-soaking the same under predetermined conditions of elevated temperature and time within substantially the manufacturer''s specified soak limits for the polyester, impregnating the fabric with an uncured synthetic resin selected for cure temperature within the predetermined elevated heat-soak temperature, conforming said one side to a desired bearing-surface contour, and curing the resin while the fabric is thus conformed.
- 17. The method of claim 16 in which said filaments are sized prior to fabric construction, and in which the fabric is washed in sizing-agent solvent prior to heat-soaking.
- 18. The method of making a low-friction bearing fabric, which comprises selecting a loosely twisted yarn comprising sized TFE filaments and high-temperature nylon filaments as the most predominant components, constructing a fabric with said yarn as the major component on at least one side, and washing the fabric in sizing-agent solvent to remove sizing, whereby when said one side of said fabric is later embodied in a bearing surface potted with a synthetic resin, the resin is induced to flow into and throughout the cleaned and loose yarn bundles, for substantially intimate and continuous and void-free consolidation therewith.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US16066171A | 1971-07-08 | 1971-07-08 |
Publications (1)
| Publication Number | Publication Date |
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| US3765978A true US3765978A (en) | 1973-10-16 |
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| US00160661A Expired - Lifetime US3765978A (en) | 1971-07-08 | 1971-07-08 | Method of making a low-friction fabric bearing |
| US05/376,235 Expired - Lifetime US4074512A (en) | 1971-07-08 | 1973-07-03 | Low-friction fabric bearing |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US05/376,235 Expired - Lifetime US4074512A (en) | 1971-07-08 | 1973-07-03 | Low-friction fabric bearing |
Country Status (6)
| Country | Link |
|---|---|
| US (2) | US3765978A (en) |
| JP (3) | JPS5838650B1 (en) |
| CA (1) | CA950520A (en) |
| DE (1) | DE2150847C3 (en) |
| FR (1) | FR2145130A5 (en) |
| GB (1) | GB1352755A (en) |
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| US3815468A (en) * | 1972-01-20 | 1974-06-11 | Textron Inc | Braided fabric bearing liner |
| US3844195A (en) * | 1972-05-26 | 1974-10-29 | Du Pont | Products |
| US4062989A (en) * | 1976-06-14 | 1977-12-13 | M. Lowenstein & Sons, Inc. | Method and apparatus for coating moving webs and products produced thereby |
| US4157788A (en) * | 1977-08-01 | 1979-06-12 | Thiokol Corporation | Low friction, movable, rocket nozzle |
| US4456653A (en) * | 1980-05-09 | 1984-06-26 | Ciba-Geigy Corporation | Pin for connecting machine elements with each other |
| US4997067A (en) * | 1989-06-26 | 1991-03-05 | Fenner America, Inc. | Friction apparatus |
| US5387300A (en) * | 1991-09-04 | 1995-02-07 | Kitamura; Atsushi | Method of manufacturing a seamless tubular woven article including polytetrafluoroethylene yarn |
| US5631085A (en) * | 1992-09-04 | 1997-05-20 | Hoechst Aktiengesellschaft | Compound yarn producing the sliding layer of plain bearings made of fiber-reinforced thermoplastics |
| US5952067A (en) * | 1996-12-02 | 1999-09-14 | A&P Technology, Inc. | Braided structure having uncrimped strands |
| DE19845442A1 (en) * | 1998-10-02 | 2000-04-20 | Cyril Xavier Latty | Packing |
| EP1234989A1 (en) * | 2001-02-22 | 2002-08-28 | New Hampshire Ball Bearings, Inc. | Self-lubricating bearing liner using poly(p-phenylene-2,6-benzobisoxazole) |
| WO2002072325A1 (en) * | 2001-03-12 | 2002-09-19 | E.S. Originals Inc. | Shoe having a fabric outsole and manufacturing process thereof |
| US20030009919A1 (en) * | 2000-07-20 | 2003-01-16 | E.S. Originals, Inc. | Process for making a shoe outsole |
| US6571491B2 (en) | 2001-03-12 | 2003-06-03 | E.S. Originals, Inc. | Shoe having a fabric outsole and manufacturing process thereof |
| US6696000B2 (en) | 2000-07-20 | 2004-02-24 | E.S. Originals, Inc. | Method of making a shoe and an outsole |
| US20040213492A1 (en) * | 2003-04-23 | 2004-10-28 | Michael Kim | Composite bearings |
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| CA1031024A (en) * | 1974-10-01 | 1978-05-09 | Textron Inc. | Low-friction fabric bearing and method of making the same |
| US4272950A (en) * | 1978-12-07 | 1981-06-16 | Commissariat A L'energie Atomique | Filiform textile material |
| US4381639A (en) * | 1980-06-19 | 1983-05-03 | Record Industrial Company | Sheath-core yarn for severe thermal protecting fabrics and method therefor |
| US4500593A (en) * | 1980-12-01 | 1985-02-19 | Weber John W | Protective fabric and fire curtain with a metallic laminate |
| US4358167A (en) * | 1981-05-26 | 1982-11-09 | The Torrington Company | Bearing element |
| USRE38136E1 (en) * | 1985-08-16 | 2003-06-10 | Supreme Elastic Corporation | Cut resistant support yarn suitable for wrapping with an additional yarn covering |
| US5655358A (en) * | 1985-08-16 | 1997-08-12 | Kolmes; Nathaniel H. | Cut resistant support yarn suitable for wrapping with an additional yarn covering |
| US4720943A (en) * | 1986-11-03 | 1988-01-26 | Monsanto Company | Cord structure |
| DK8289A (en) * | 1988-01-12 | 1989-07-13 | Raychem Ltd | COMPOSITE |
| US4893665A (en) * | 1988-02-17 | 1990-01-16 | The Goodyear Tire & Rubber Company | Cables for reinforcing deformable articles and articles reinforced by said cables |
| US4832101A (en) * | 1988-02-17 | 1989-05-23 | The Goodyear Tire & Rubber Company | Pneumatic tires |
| US5809861A (en) * | 1988-02-18 | 1998-09-22 | Whizard Protective Wear Corp. | Yarn having a braided covering thereon and safety apparel knitted therefrom |
| DE4330565C1 (en) * | 1993-09-09 | 1994-08-18 | Porsche Ag | Crankshaft bearing |
| US5590420A (en) * | 1994-03-24 | 1997-01-07 | Gunn; Robert T. | Low friction apparel |
| US5829057A (en) * | 1994-03-24 | 1998-11-03 | Robert T. Gunn | Low friction outer apparel |
| US5628172A (en) * | 1994-08-31 | 1997-05-13 | Nathaniel H. Kolmes | Composite yarns for protective garments |
| GB2320934A (en) * | 1997-01-06 | 1998-07-08 | Palencia Ltd | Yarn for use in tufted fabrics |
| RU2216612C2 (en) * | 1998-01-28 | 2003-11-20 | Е.И.Дюпон Де Немур Энд Компани | Mixed yarn for frictional use |
| US6143368A (en) | 1998-02-10 | 2000-11-07 | Gunn; Robert T. | Low coefficient of friction fibers |
| US7100246B1 (en) * | 1999-06-14 | 2006-09-05 | E. I. Du Pont De Nemours And Company | Stretch break method and product |
| AU5333000A (en) * | 1999-06-14 | 2001-01-02 | E.I. Du Pont De Nemours And Company | Stretch break method and product |
| DE19950621A1 (en) * | 1999-10-20 | 2001-04-26 | Schuler Kunststofftechnik Gmbh | Sliding bearing plate for molding tool parts, especially in vehicle tire molds, comprises multi-layer structure with self-lubricating bearing surface |
| WO2001044306A2 (en) * | 1999-11-15 | 2001-06-21 | Gunn Robert T | Compositions with low coefficients of friction and methods for their preparation |
| US20060204753A1 (en) * | 2001-11-21 | 2006-09-14 | Glen Simmonds | Stretch Break Method and Product |
| US20050191474A1 (en) * | 2003-10-09 | 2005-09-01 | Gunn Robert T. | Compositions with low coefficients of friction and methods for their preparation |
| US7345215B2 (en) * | 2003-12-22 | 2008-03-18 | Sca Hygiene Products Ab | Absorbent product with low friction zone |
| US7147378B2 (en) * | 2004-02-19 | 2006-12-12 | Gore Enterprise Holdings, Inc. | Low friction, abrasion-resistant bearing materials |
| US20050186367A1 (en) * | 2004-02-19 | 2005-08-25 | Hanrahan James R. | Low friction, abrasion-resistant materials and articles made therefrom |
| US7296394B2 (en) * | 2005-02-11 | 2007-11-20 | Gore Enterprise Holdings, Inc. | Fluoropolymer fiber composite bundle |
| US20060182962A1 (en) * | 2005-02-11 | 2006-08-17 | Bucher Richard A | Fluoropolymer fiber composite bundle |
| US9334587B2 (en) | 2005-02-11 | 2016-05-10 | W. L. Gore & Associates, Inc. | Fluoropolymer fiber composite bundle |
| US8152380B2 (en) * | 2006-07-07 | 2012-04-10 | Federal-Mogul World Wide, Inc. | Sleeve bearing assembly and method of construction |
| CN102870300A (en) | 2010-04-16 | 2013-01-09 | 瑞拉特斯有限公司 | Protective tube |
| DE102016014816B4 (en) * | 2016-12-13 | 2019-02-28 | Robert Lorenz | Bearing arrangement with maintenance-free fiber sliding layer |
| CN116497491B (en) * | 2023-06-20 | 2023-09-08 | 克州润华纺织科技有限公司 | Blended yarn production equipment and production technology |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3815468A (en) * | 1972-01-20 | 1974-06-11 | Textron Inc | Braided fabric bearing liner |
| US3844195A (en) * | 1972-05-26 | 1974-10-29 | Du Pont | Products |
| US4062989A (en) * | 1976-06-14 | 1977-12-13 | M. Lowenstein & Sons, Inc. | Method and apparatus for coating moving webs and products produced thereby |
| US4157788A (en) * | 1977-08-01 | 1979-06-12 | Thiokol Corporation | Low friction, movable, rocket nozzle |
| US4456653A (en) * | 1980-05-09 | 1984-06-26 | Ciba-Geigy Corporation | Pin for connecting machine elements with each other |
| US4997067A (en) * | 1989-06-26 | 1991-03-05 | Fenner America, Inc. | Friction apparatus |
| US5387300A (en) * | 1991-09-04 | 1995-02-07 | Kitamura; Atsushi | Method of manufacturing a seamless tubular woven article including polytetrafluoroethylene yarn |
| US5631085A (en) * | 1992-09-04 | 1997-05-20 | Hoechst Aktiengesellschaft | Compound yarn producing the sliding layer of plain bearings made of fiber-reinforced thermoplastics |
| US5952067A (en) * | 1996-12-02 | 1999-09-14 | A&P Technology, Inc. | Braided structure having uncrimped strands |
| DE19845442A1 (en) * | 1998-10-02 | 2000-04-20 | Cyril Xavier Latty | Packing |
| US7353626B2 (en) | 2000-07-20 | 2008-04-08 | E.S. Originals, Inc. | Shoe with slip-resistant, shape-retaining fabric outsole |
| US6823611B2 (en) | 2000-07-20 | 2004-11-30 | E. S. Originals, Inc. | Shoe with slip-resistant, shape-retaining fabric outsole |
| US20030009919A1 (en) * | 2000-07-20 | 2003-01-16 | E.S. Originals, Inc. | Process for making a shoe outsole |
| US20060143946A1 (en) * | 2000-07-20 | 2006-07-06 | Jon Otis | Shoe with slip-resistant, shape-retaining fabric outsole |
| US6696000B2 (en) | 2000-07-20 | 2004-02-24 | E.S. Originals, Inc. | Method of making a shoe and an outsole |
| US6698109B2 (en) | 2000-07-20 | 2004-03-02 | E.S. Originals, Inc. | Shoe with slip-resistant, shape-retaining fabric outsole |
| US7036246B2 (en) | 2000-07-20 | 2006-05-02 | E.S. Origianals, Inc. | Shoe with slip-resistant, shape-retaining fabric outsole |
| US20050241182A1 (en) * | 2000-07-20 | 2005-11-03 | Jon Otis | Shoe with slip-resistant, shape-retaining fabric outsole |
| EP1234989A1 (en) * | 2001-02-22 | 2002-08-28 | New Hampshire Ball Bearings, Inc. | Self-lubricating bearing liner using poly(p-phenylene-2,6-benzobisoxazole) |
| US20020152638A1 (en) * | 2001-03-12 | 2002-10-24 | E. S. Originals, Inc. | Shoe having a fabric outsole and manufacturing process thereof and system for customized ordering thereof |
| US6944975B2 (en) | 2001-03-12 | 2005-09-20 | E.S. Originals, Inc. | Shoe having a fabric outsole and manufacturing process thereof |
| US6571491B2 (en) | 2001-03-12 | 2003-06-03 | E.S. Originals, Inc. | Shoe having a fabric outsole and manufacturing process thereof |
| US7179414B2 (en) | 2001-03-12 | 2007-02-20 | E.S. Originals, Inc. | Shoe manufacturing method |
| WO2002072325A1 (en) * | 2001-03-12 | 2002-09-19 | E.S. Originals Inc. | Shoe having a fabric outsole and manufacturing process thereof |
| CN1471453B (en) * | 2001-03-12 | 2010-12-22 | 爱思先创有限公司 | Shoe with textile outsole and method of making same |
| WO2004094850A1 (en) * | 2003-04-23 | 2004-11-04 | Glacier Garlock Bearings, Inc. | Composite bearings |
| US20040213492A1 (en) * | 2003-04-23 | 2004-10-28 | Michael Kim | Composite bearings |
Also Published As
| Publication number | Publication date |
|---|---|
| CA950520A (en) | 1974-07-02 |
| JPS552888A (en) | 1980-01-10 |
| US4074512A (en) | 1978-02-21 |
| JPS57176924U (en) | 1982-11-09 |
| DE2150847A1 (en) | 1973-01-18 |
| DE2150847B2 (en) | 1981-01-15 |
| JPS5838650B1 (en) | 1983-08-24 |
| GB1352755A (en) | 1974-05-08 |
| FR2145130A5 (en) | 1973-02-16 |
| DE2150847C3 (en) | 1981-11-05 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| AS | Assignment |
Owner name: TORRINGTON COMPANY, THE, CONNECTICUT Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:TEXTRON INC.;REEL/FRAME:004548/0536 Effective date: 19851026 Owner name: TORRINGTON COMPANY, THE, 59 FIELD STREET, TORRINGT Free format text: ASSIGNMENT OF ASSIGNORS INTEREST.;ASSIGNOR:TEXTRON INC.;REEL/FRAME:004548/0536 Effective date: 19851026 |