US20090263181A1 - Joint assembly with centering flange - Google Patents
Joint assembly with centering flange Download PDFInfo
- Publication number
- US20090263181A1 US20090263181A1 US12/491,931 US49193109A US2009263181A1 US 20090263181 A1 US20090263181 A1 US 20090263181A1 US 49193109 A US49193109 A US 49193109A US 2009263181 A1 US2009263181 A1 US 2009263181A1
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- US
- United States
- Prior art keywords
- rotating part
- contact section
- centering flange
- joint assembly
- axis
- 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
Links
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- 230000013011 mating Effects 0.000 description 6
- 230000000712 assembly Effects 0.000 description 3
- 238000000429 assembly Methods 0.000 description 3
- 230000004323 axial length Effects 0.000 description 2
- 230000008901 benefit Effects 0.000 description 2
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- 238000006073 displacement reaction Methods 0.000 description 1
- -1 ferrous metals Chemical class 0.000 description 1
- 238000005461 lubrication Methods 0.000 description 1
- 229910052751 metal Inorganic materials 0.000 description 1
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- 229920001169 thermoplastic Polymers 0.000 description 1
- 239000004416 thermosoftening plastic Substances 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
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D1/00—Couplings for rigidly connecting two coaxial shafts or other movable machine elements
- F16D1/06—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end
- F16D1/076—Couplings for rigidly connecting two coaxial shafts or other movable machine elements for attachment of a member on a shaft or on a shaft-end by clamping together two faces perpendicular to the axis of rotation, e.g. with bolted flanges
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
- F16B2200/50—Flanged connections
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B2200/00—Constructional details of connections not covered for in other groups of this subclass
- F16B2200/50—Flanged connections
- F16B2200/506—Flanged connections bolted or riveted
-
- 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
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D3/00—Yielding couplings, i.e. with means permitting movement between the connected parts during the drive
- F16D3/16—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts
- F16D3/20—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts one coupling part entering a sleeve of the other coupling part and connected thereto by sliding or rolling members
- F16D3/22—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts one coupling part entering a sleeve of the other coupling part and connected thereto by sliding or rolling members the rolling members being balls, rollers, or the like, guided in grooves or sockets in both coupling parts
- F16D3/223—Universal joints in which flexibility is produced by means of pivots or sliding or rolling connecting parts one coupling part entering a sleeve of the other coupling part and connected thereto by sliding or rolling members the rolling members being balls, rollers, or the like, guided in grooves or sockets in both coupling parts the rolling members being guided in grooves in both coupling parts
- F16D2003/22326—Attachments to the outer joint member, i.e. attachments to the exterior of the outer joint member or to the shaft of the outer joint member
-
- 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
- Y10T403/00—Joints and connections
- Y10T403/32—Articulated members
- Y10T403/32114—Articulated members including static joint
- Y10T403/32196—Articulate joint is ball and socket
- Y10T403/32204—Articulate joint is ball and socket with threaded joint
Definitions
- the present invention relates generally to joint assemblies for operatively coupling rotating parts. More specifically, the present invention relates to joint assemblies comprising multiple joint members with one of the joint members having a centering flange for mounting to one of the rotating parts.
- Joint assemblies for operatively coupling first and second rotating parts are well known in the art.
- One particularly well known joint assembly is that formed between one end of what is referred to as a constant velocity or CV joint that is included in the first rotating part, and the second rotating part.
- a typical CV joint of a first rotating part comprises a first CV joint member and a second CV joint member, the second CV joint member having an end adapted for mounting to a second rotating part as part of a joint assembly.
- a plurality of torque-transmitting elements are disposed between the first and second CV joint members to operatively couple the first and second CV joint members.
- the first CV joint member can be fixed to other portions of the first rotating part in any number of fashions, such as by splined fits and the like.
- the second CV joint member often includes a centering flange for mating with the second rotating part.
- the centering flange 10 of second CV joint member 12 of the first rotating part has an overall length L 1 .
- the centering flange 10 also has a contact section 14 configured for being in a substantially interference fit with an inner cylindrical surface 16 of the second rotating part 18 .
- the contact section 14 has a second length L 2 that extends a substantial portion of the overall length L 1 .
- the volume of material in the contact section 14 must be displaced when mounting the centering flange 10 of second CV joint member 12 to the second rotating part 18 , either by forces deflecting the centering flange 10 radially inwardly or by forces deforming the centering flange 10 .
- the larger the volume of material to be displaced the larger the force required to mount the centering flange 10 to the second rotating part 18 , and likewise, the larger the force required to remove the centering flange 10 from the second rotating part 18 to repair or replace the joint assembly.
- this prior art centering flange which is cylindrical so as to present a straight pilot, requires a precision fit and is susceptible to binding.
- a centering flange that has a contact section configured in a way such that the substantially interference fit between the centering flange and the second rotating part provides alignment between the centering flange and the second rotating part while minimizing the forces necessary to mount the centering flange to the second rotating part.
- the present invention provides a joint assembly for operatively coupling first and second rotating parts.
- the first rotating part includes a CV joint that has a first CV joint member and a second CV joint member, the second CV joint member adapted for mounting to the second rotating part.
- At least one torque-transmitting element is disposed between the first and second CV joint members for operatively coupling the first and second CV joint members.
- the second CV joint member includes a centering flange disposed about an axis and having a first length for mounting to the second rotating part.
- the centering flange has a contact section configured for being in a substantially interference fit with the second rotating part when mounting the centering flange to the second rotating part.
- the contact section has a second length substantially smaller than the first length of the centering flange such that the substantially interference fit between the centering flange and the second rotating part provides alignment between the centering flange and the second rotating part while minimizing forces necessary to mount the centering flange to the second rotating part.
- the substantially interference fit requires displacement of less material than the prior art centering flange shown in FIG. 1 with the same outer dimensions.
- tolerances between the centering flange and the second rotating part can be increased.
- variations in dimensions of the centering flange of the present invention can be higher than the prior art centering flange since the contact section of the centering flange of the present invention is much smaller than that of the prior art centering flange.
- FIG. 1 is a partial, cross-sectional, exploded view of a prior art joint assembly, showing its centering flange;
- FIG. 2 is a cross-sectional, exploded view of a joint assembly of the present invention, showing its centering flange on a CV joint member;
- FIG. 3 is an end view of the portion of the joint assembly of FIG. 2 that includes the CV joint of the first rotating part, with the cover enclosing the CV joint closed end removed;
- FIGS. 4 and 5 respectively show a partial, cross-sectional, exploded view of the joint assembly having a first centering flange embodiment of the present invention, and an enlarged, partial, cross-sectional view of the first centering flange embodiment;
- FIGS. 6-14 are enlarged, partial, cross-sectional views of various alternative embodiments of the centering flange of the joint assembly of the present invention.
- FIGS. 15 and 16 are enlarged, partial, cross-sectional views of the joint assembly of FIG. 2 showing it in different states of assembly.
- first 20 and second 22 rotating parts are shown generally at 24 .
- first rotating part 20 is described as including a constant velocity or CV joint.
- the joint assembly 24 may be any joint assembly capable of operatively coupling parts for rotation, while allowing the parts to deviate from perfect axial alignment with one another.
- the first rotating part 20 includes a CV joint having a first CV joint member 26 , known as an inner race in some embodiments and a second CV joint member 28 , known as an outer race in some embodiments, that is mounted to the second rotating part 22 , thereby forming joint assembly 24 .
- the first CV joint member 26 is formed with an outer curved surface 30 (see FIG. 3 ) in which a plurality of first ball grooves 32 are formed.
- the second CV joint member 28 has an open end 34 in which the first CV joint member 26 is disposed, an opposite end 36 closed by a cover, and an inner curved surface 38 in which a plurality of second ball grooves 40 are formed.
- At least one torque-transmitting element 44 is disposed between the first 26 and second 28 CV joint members to operatively couple the first 26 and second 28 CV joint members.
- the at least one torque-transmitting element 44 is further defined as a plurality of torque-transmitting balls 44 arranged in pairs of the first 32 and second 40 ball grooves between the first 26 and second 28 CV joint members.
- a cage 46 contains and secures the plurality of balls 44 between the first 26 and second 28 CV joint members.
- the balls 44 transmit torque between the CV joint members 26 , 28 .
- the first 26 and second 28 CV joint members, the cage 46 , and the balls 44 may be formed of any material capable of transferring torque between the first 20 and second 22 rotating parts including ferrous and non-ferrous metals, and the like.
- the first CV joint member 26 includes an opening 48 with splines for fitting onto mating splines of a stub shaft of the first rotating part 20 .
- the stub shaft of the first rotating part 20 may, for example, form part of a drive shaft, with the joint assembly 24 being utilized to transmit rotational energy, e.g., torque, from the drive shaft to the second rotating part 22 wherein the second rotating part 22 may be an output shaft for extending to a transfer case, an input shaft of a differential, or the like.
- a boot 54 is mounted onto the second CV joint member 28 and is arranged to be fitted onto the stub shaft of the first rotating part 20 to retain lubrication within the CV joint.
- the boot 54 may comprise any suitable material that is sufficiently flexible to allow the CV joint to operate through a wide range of angles, such as thermoplastic and elastomeric materials.
- the second CV joint member 28 of first rotating part 20 is formed with a radial mounting flange 56 adjacent the closed end 36 .
- the radial mounting flange 56 is adapted to be bolted to a mating flange 58 of the second rotating part 22 in securing joint assembly 24 together.
- the mating flange 58 has a shoulder 62 with a cylindrical inner surface 64 of predetermined diameter centered about a second axis 66 of the second rotating part 22 .
- Inner surface 64 defines a void in second rotating part 22 .
- the second CV joint member 28 of first rotating part 20 further includes an annular pilot projection or centering flange 68 disposed about an axis 70 of the second CV joint member 28 and extending axially toward the second rotating part 22 .
- the centering flange 68 is received in the void defined by, and is dimensioned for a substantially interference fit with the cylindrical inner surface 64 in order to center the second CV joint member 28 of the first rotating part 20 on the second rotating part 22 during mounting with radial mounting flange 56 of the second CV joint member 28 and mating flange 58 of the second rotating part 22 positioned to be bolted together in securing joint assembly 24 together, after which axes 66 , 70 are aligned.
- the substantially interference fit refers to the overall fit between the centering flange 68 and the cylindrical inner surface 64 while also including imperfections in the shapes of the centering flange 68 and the cylindrical inner surface 64 that may result in portions not being in an interference fit with one another.
- the centering flange 68 is preferably fixed to the second CV joint member 28 of first rotating part 20 , and more preferably is integrally formed with the second CV joint member 28 .
- the centering flange 68 is formed with a profiled outer surface 72 that enables the centering flange 68 to be slid into engagement with the cylindrical inner surface 64 of the shoulder 62 while the axes 66 , 70 are misaligned (i.e., with the second CV joint member 28 of first rotating part 20 slightly cocked relative to the second rotating part 22 , as shown in FIG.
- centering flange 68 and cylindrical inner surface 64 are interengaged and axes 66 , 70 are misaligned, as shown in FIG. 15 , and a state of more complete mounting or assembly wherein centering flange 68 and cylindrical inner surface 64 have a substantially interference fit and axes 66 , 70 are aligned, as shown in FIG. 16 .
- the outer surface 72 of centering flange 68 is convexly curved in the axial direction in order to provide contact with the cylindrical inner surface 64 of the shoulder 62 .
- the centering flange 68 is disposed about the axis 70 of the second CV joint member 28 of the first rotating part 20 and has a first length L 1 .
- the first length L 1 is considered the overall axial length of the centering flange 68 relative to the axis 70 of the second CV joint member 28 .
- the centering flange 68 has a contact section 76 configured for being in a substantially interference fit with the inner cylindrical surface 64 of the shoulder 62 of the mating flange 58 when mounting the centering flange 68 to the inner cylindrical surface 64 .
- the contact section 76 has a second length L 2 substantially smaller than the first length L 1 of the centering flange 68 such that the substantially interference fit between the centering flange 68 and the inner cylindrical surface 64 provides alignment of the axes 66 , 70 of the centering flange 68 and the second rotating part 22 while minimizing forces necessary to mount the centering flange 68 to the second rotating part 22 .
- the term substantially smaller is further defined as the second length L 2 being less than 70 percent of the first length L 1 . In a further embodiment, the term substantially smaller is further defined as the second length L 2 being less than 50 percent of the first length L 1 . In yet another embodiment, the term substantially smaller is further defined as the second length L 2 being less than 30 percent of the first length L 1 .
- the centering flange 68 also includes at least one non-contact section 80 configured for not being in a substantially interference fit with the inner cylindrical surface 64 of the shoulder 62 .
- the non-contact section 80 radially extends from the axis 70 of the second CV joint member 28 at a first maximum radius R 1 and the contact section 76 radially extends from the axis 70 at a second maximum radius R 2 greater than the first maximum radius R 1 .
- the contact section 76 extends further radially outwardly than the non-contact section 80 to provide the substantially interference fit between the contact section 76 and the inner cylindrical surface 64 .
- the outer surface 72 may comprise any of a number of shapes in cross-sectional profile that will provide a contact section 76 for being in a substantially interference fit with the inner cylindrical surface 64 while minimizing the forces necessary to mount the centering flange 68 to the second rotating part 22 and accommodating misalignment during connection of the second CV joint member 28 of the first rotating part 20 with the second rotating part 22 .
- various shapes of the outer surface 72 are contemplated by the present invention. Some of these shapes are shown in FIGS. 5-14 .
- the second length L 2 is respectively represented as L 3 -L 11 .
- the contact section reaches the second maximum radius R 2 only locally along its respective axial length L 2 -L 11 .
- the numerals referring to like parts in FIGS. 6-14 have been respectively increased by increments of 100.
- the outer surface 72 , 172 is further defined as a curved surface.
- the curved surface 72 of FIG. 5 is formed at a single radius R 3
- the curved surface 172 of FIG. 6 is formed at multiple radii R 4 , R 5 .
- the outer surface 272 , 372 is further defined as a plurality of joined frustoconical surfaces.
- differing first and second frustoconical surfaces are arranged such that the bases of the first and second frustoconical surfaces are included in the contact section 276 , while the second frustoconical surface also includes the non-contact section 280 .
- the contact section 376 is partially defined at the intersection of two similar frustoconical surfaces.
- the outer surface 472 is further defined as a semi-elliptical surface.
- the outer surface 572 is further defined as a parabolic surface.
- the outer surface 672 is further defined as a plurality of frustoconical surfaces joined by a cylindrical surface.
- the outer surface 772 includes a projection or protrusion 78 extending radially outwardly relative to the axis 70 of the second joint member 728 .
- the protrusion 78 includes the contact section 776 , while the non-contact section 780 lies on both sides of the protrusion 78 .
- the outer surface 872 is further defined as a curved surface as in FIGS. 5 and 6 , except that the curved surface is formed at a single radius R 6 with an offset.
- the offset is in the non-contact section 880 .
- the outer surface 972 is further defined as a plurality of frustoconical surfaces joined by a curved surface.
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Mutual Connection Of Rods And Tubes (AREA)
- Rolling Contact Bearings (AREA)
- Motor Power Transmission Devices (AREA)
- Joints Allowing Movement (AREA)
- Flanged Joints, Insulating Joints, And Other Joints (AREA)
Abstract
Description
- This application is a continuation of co-pending U.S. patent application Ser. No. 11/355,365, filed Feb. 16, 2006, which claims priority to and all the benefits of, and incorporates by reference, U.S. provisional patent application Ser. No. 60/654,323, filed Feb. 18, 2005.
- 1. Field of the Invention
- The present invention relates generally to joint assemblies for operatively coupling rotating parts. More specifically, the present invention relates to joint assemblies comprising multiple joint members with one of the joint members having a centering flange for mounting to one of the rotating parts.
- 2. Description of Related Art
- Joint assemblies for operatively coupling first and second rotating parts are well known in the art. One particularly well known joint assembly is that formed between one end of what is referred to as a constant velocity or CV joint that is included in the first rotating part, and the second rotating part. A typical CV joint of a first rotating part comprises a first CV joint member and a second CV joint member, the second CV joint member having an end adapted for mounting to a second rotating part as part of a joint assembly. A plurality of torque-transmitting elements, usually in the form of torque-transmitting balls, are disposed between the first and second CV joint members to operatively couple the first and second CV joint members. The first CV joint member can be fixed to other portions of the first rotating part in any number of fashions, such as by splined fits and the like. The second CV joint member often includes a centering flange for mating with the second rotating part.
- Referring to
FIG. 1 , one such centeringflange 10 is shown. Here, the centeringflange 10 of second CVjoint member 12 of the first rotating part has an overall length L1. The centeringflange 10 also has acontact section 14 configured for being in a substantially interference fit with an innercylindrical surface 16 of the second rotatingpart 18. Thecontact section 14 has a second length L2 that extends a substantial portion of the overall length L1. Since thecontact section 14 of second CVjoint member 12 is in a substantially interference fit with the innercylindrical surface 16 of the second rotatingpart 18, the volume of material in thecontact section 14 must be displaced when mounting the centeringflange 10 of second CVjoint member 12 to the second rotatingpart 18, either by forces deflecting the centeringflange 10 radially inwardly or by forces deforming the centeringflange 10. The larger the volume of material to be displaced, the larger the force required to mount the centeringflange 10 to the second rotatingpart 18, and likewise, the larger the force required to remove the centeringflange 10 from the second rotatingpart 18 to repair or replace the joint assembly. Furthermore, this prior art centering flange, which is cylindrical so as to present a straight pilot, requires a precision fit and is susceptible to binding. - Therefore, there is a need in the art for a centering flange that has a contact section configured in a way such that the substantially interference fit between the centering flange and the second rotating part provides alignment between the centering flange and the second rotating part while minimizing the forces necessary to mount the centering flange to the second rotating part.
- The present invention provides a joint assembly for operatively coupling first and second rotating parts. The first rotating part includes a CV joint that has a first CV joint member and a second CV joint member, the second CV joint member adapted for mounting to the second rotating part. At least one torque-transmitting element is disposed between the first and second CV joint members for operatively coupling the first and second CV joint members. The second CV joint member includes a centering flange disposed about an axis and having a first length for mounting to the second rotating part. The centering flange has a contact section configured for being in a substantially interference fit with the second rotating part when mounting the centering flange to the second rotating part. The contact section has a second length substantially smaller than the first length of the centering flange such that the substantially interference fit between the centering flange and the second rotating part provides alignment between the centering flange and the second rotating part while minimizing forces necessary to mount the centering flange to the second rotating part.
- By making the length of the contact section substantially smaller than the overall length of the centering flange, the substantially interference fit requires displacement of less material than the prior art centering flange shown in
FIG. 1 with the same outer dimensions. As a result, tolerances between the centering flange and the second rotating part can be increased. In other words, variations in dimensions of the centering flange of the present invention can be higher than the prior art centering flange since the contact section of the centering flange of the present invention is much smaller than that of the prior art centering flange. - Other advantages of the present invention will be readily appreciated, as the same becomes better understood by reference to the following detailed description when considered in connection with the accompanying drawings wherein:
-
FIG. 1 is a partial, cross-sectional, exploded view of a prior art joint assembly, showing its centering flange; -
FIG. 2 is a cross-sectional, exploded view of a joint assembly of the present invention, showing its centering flange on a CV joint member; -
FIG. 3 is an end view of the portion of the joint assembly ofFIG. 2 that includes the CV joint of the first rotating part, with the cover enclosing the CV joint closed end removed; -
FIGS. 4 and 5 respectively show a partial, cross-sectional, exploded view of the joint assembly having a first centering flange embodiment of the present invention, and an enlarged, partial, cross-sectional view of the first centering flange embodiment; -
FIGS. 6-14 are enlarged, partial, cross-sectional views of various alternative embodiments of the centering flange of the joint assembly of the present invention; and -
FIGS. 15 and 16 are enlarged, partial, cross-sectional views of the joint assembly ofFIG. 2 showing it in different states of assembly. - Referring to the Figures, wherein like numerals indicate like or corresponding parts throughout the several views, a joint assembly for coupling first 20 and second 22 rotating parts is shown generally at 24. In one embodiment, the first rotating
part 20 is described as including a constant velocity or CV joint. However, thejoint assembly 24 may be any joint assembly capable of operatively coupling parts for rotation, while allowing the parts to deviate from perfect axial alignment with one another. - Referring to
FIGS. 2-3 , the first rotatingpart 20 includes a CV joint having a first CVjoint member 26, known as an inner race in some embodiments and a second CVjoint member 28, known as an outer race in some embodiments, that is mounted to the second rotatingpart 22, thereby formingjoint assembly 24. As is typical of known CV joints, the first CVjoint member 26 is formed with an outer curved surface 30 (seeFIG. 3 ) in which a plurality offirst ball grooves 32 are formed. The second CVjoint member 28 has anopen end 34 in which the first CVjoint member 26 is disposed, anopposite end 36 closed by a cover, and an innercurved surface 38 in which a plurality ofsecond ball grooves 40 are formed. - As is also typical of known CV joints, at least one torque-transmitting
element 44 is disposed between the first 26 and second 28 CV joint members to operatively couple the first 26 and second 28 CV joint members. The at least one torque-transmittingelement 44 is further defined as a plurality of torque-transmittingballs 44 arranged in pairs of the first 32 and second 40 ball grooves between the first 26 and second 28 CV joint members. Acage 46 contains and secures the plurality ofballs 44 between the first 26 and second 28 CV joint members. Theballs 44 transmit torque between the CVjoint members cage 46, and theballs 44 may be formed of any material capable of transferring torque between the first 20 and second 22 rotating parts including ferrous and non-ferrous metals, and the like. - Preferably, the first CV
joint member 26 includes an opening 48 with splines for fitting onto mating splines of a stub shaft of the first rotatingpart 20. It should be appreciated by those skilled in the art that the stub shaft of the first rotatingpart 20 may, for example, form part of a drive shaft, with thejoint assembly 24 being utilized to transmit rotational energy, e.g., torque, from the drive shaft to the second rotatingpart 22 wherein the second rotatingpart 22 may be an output shaft for extending to a transfer case, an input shaft of a differential, or the like. - A
boot 54 is mounted onto the second CVjoint member 28 and is arranged to be fitted onto the stub shaft of the first rotatingpart 20 to retain lubrication within the CV joint. Theboot 54 may comprise any suitable material that is sufficiently flexible to allow the CV joint to operate through a wide range of angles, such as thermoplastic and elastomeric materials. - Referring to
FIGS. 4 , 15 and 16, the second CVjoint member 28 of first rotatingpart 20 is formed with aradial mounting flange 56 adjacent the closedend 36. Theradial mounting flange 56 is adapted to be bolted to amating flange 58 of the second rotatingpart 22 in securingjoint assembly 24 together. Themating flange 58 has ashoulder 62 with a cylindricalinner surface 64 of predetermined diameter centered about asecond axis 66 of the second rotatingpart 22.Inner surface 64 defines a void in second rotatingpart 22. - The second CV
joint member 28 of first rotatingpart 20 further includes an annular pilot projection or centeringflange 68 disposed about anaxis 70 of the second CVjoint member 28 and extending axially toward the second rotatingpart 22. The centeringflange 68 is received in the void defined by, and is dimensioned for a substantially interference fit with the cylindricalinner surface 64 in order to center the second CVjoint member 28 of the first rotatingpart 20 on the second rotatingpart 22 during mounting withradial mounting flange 56 of the second CVjoint member 28 andmating flange 58 of the second rotatingpart 22 positioned to be bolted together in securingjoint assembly 24 together, after whichaxes flange 68 and the cylindricalinner surface 64 while also including imperfections in the shapes of the centeringflange 68 and the cylindricalinner surface 64 that may result in portions not being in an interference fit with one another. The centeringflange 68 is preferably fixed to the second CVjoint member 28 of first rotatingpart 20, and more preferably is integrally formed with the second CVjoint member 28. - Referring to
FIG. 5 , the centeringflange 68 is formed with a profiledouter surface 72 that enables the centeringflange 68 to be slid into engagement with the cylindricalinner surface 64 of theshoulder 62 while theaxes joint member 28 of firstrotating part 20 slightly cocked relative to the secondrotating part 22, as shown inFIG. 15 ) without causing the second CVjoint member 28 to bind at the centeringflange 68 with the secondrotating part 22 as one of a plurality of bolts is being tightened during a transition between a state of partial mounting or assembly wherein centeringflange 68 and cylindricalinner surface 64 are interengaged and axes 66, 70 are misaligned, as shown inFIG. 15 , and a state of more complete mounting or assembly wherein centeringflange 68 and cylindricalinner surface 64 have a substantially interference fit and axes 66, 70 are aligned, as shown inFIG. 16 . In one embodiment, shown inFIG. 5 for instance, theouter surface 72 of centeringflange 68 is convexly curved in the axial direction in order to provide contact with the cylindricalinner surface 64 of theshoulder 62. - To better understand the fit between the centering
flange 68 and the innercylindrical surface 64 of theshoulder 62, the geometry and dimensioning of the centeringflange 68 is now described. The centeringflange 68 is disposed about theaxis 70 of the second CVjoint member 28 of the firstrotating part 20 and has a first length L1. The first length L1 is considered the overall axial length of the centeringflange 68 relative to theaxis 70 of the second CVjoint member 28. - The centering
flange 68 has acontact section 76 configured for being in a substantially interference fit with the innercylindrical surface 64 of theshoulder 62 of themating flange 58 when mounting the centeringflange 68 to the innercylindrical surface 64. Thecontact section 76 has a second length L2 substantially smaller than the first length L1 of the centeringflange 68 such that the substantially interference fit between the centeringflange 68 and the innercylindrical surface 64 provides alignment of theaxes flange 68 and the secondrotating part 22 while minimizing forces necessary to mount the centeringflange 68 to the secondrotating part 22. - In one embodiment, the term substantially smaller is further defined as the second length L2 being less than 70 percent of the first length L1. In a further embodiment, the term substantially smaller is further defined as the second length L2 being less than 50 percent of the first length L1. In yet another embodiment, the term substantially smaller is further defined as the second length L2 being less than 30 percent of the first length L1.
- The centering
flange 68 also includes at least onenon-contact section 80 configured for not being in a substantially interference fit with the innercylindrical surface 64 of theshoulder 62. Thenon-contact section 80 radially extends from theaxis 70 of the second CVjoint member 28 at a first maximum radius R1 and thecontact section 76 radially extends from theaxis 70 at a second maximum radius R2 greater than the first maximum radius R1. As a result, thecontact section 76 extends further radially outwardly than thenon-contact section 80 to provide the substantially interference fit between thecontact section 76 and the innercylindrical surface 64. - The
outer surface 72 may comprise any of a number of shapes in cross-sectional profile that will provide acontact section 76 for being in a substantially interference fit with the innercylindrical surface 64 while minimizing the forces necessary to mount the centeringflange 68 to the secondrotating part 22 and accommodating misalignment during connection of the second CVjoint member 28 of the firstrotating part 20 with the secondrotating part 22. In other words, various shapes of theouter surface 72 are contemplated by the present invention. Some of these shapes are shown inFIGS. 5-14 . InFIGS. 6-14 , the second length L2 is respectively represented as L3-L11. Moreover, in the depicted embodiments the contact section reaches the second maximum radius R2 only locally along its respective axial length L2-L11. Additionally, the numerals referring to like parts inFIGS. 6-14 have been respectively increased by increments of 100. - In
FIGS. 5 and 6 , theouter surface curved surface 72 ofFIG. 5 is formed at a single radius R3, while thecurved surface 172 ofFIG. 6 is formed at multiple radii R4, R5. - In
FIGS. 7 and 8 , theouter surface FIG. 7 , differing first and second frustoconical surfaces are arranged such that the bases of the first and second frustoconical surfaces are included in thecontact section 276, while the second frustoconical surface also includes thenon-contact section 280. InFIG. 8 , thecontact section 376 is partially defined at the intersection of two similar frustoconical surfaces. - In
FIG. 9 , theouter surface 472 is further defined as a semi-elliptical surface. - In
FIG. 10 , theouter surface 572 is further defined as a parabolic surface. - In
FIG. 11 , theouter surface 672 is further defined as a plurality of frustoconical surfaces joined by a cylindrical surface. - In
FIG. 12 , theouter surface 772 includes a projection or protrusion 78 extending radially outwardly relative to theaxis 70 of the secondjoint member 728. The protrusion 78 includes the contact section 776, while thenon-contact section 780 lies on both sides of the protrusion 78. - In
FIG. 13 , theouter surface 872 is further defined as a curved surface as inFIGS. 5 and 6 , except that the curved surface is formed at a single radius R6 with an offset. In this embodiment, the offset is in thenon-contact section 880. - In
FIG. 14 , theouter surface 972 is further defined as a plurality of frustoconical surfaces joined by a curved surface. - Obviously, many modifications and variations of the present invention are possible in light of the above teachings. The invention may be practiced otherwise than as specifically described within the scope of the appended claims.
Claims (22)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US12/491,931 US20090263181A1 (en) | 2005-02-18 | 2009-06-25 | Joint assembly with centering flange |
US13/421,849 US8449399B2 (en) | 2005-02-18 | 2012-03-15 | Joint assembly with centering flange |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US65432305P | 2005-02-18 | 2005-02-18 | |
US11/355,365 US20060185124A1 (en) | 2005-02-18 | 2006-02-16 | Joint assembly with centering flange |
US12/491,931 US20090263181A1 (en) | 2005-02-18 | 2009-06-25 | Joint assembly with centering flange |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/355,365 Continuation US20060185124A1 (en) | 2005-02-18 | 2006-02-16 | Joint assembly with centering flange |
Related Child Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/421,849 Continuation US8449399B2 (en) | 2005-02-18 | 2012-03-15 | Joint assembly with centering flange |
Publications (1)
Publication Number | Publication Date |
---|---|
US20090263181A1 true US20090263181A1 (en) | 2009-10-22 |
Family
ID=36911038
Family Applications (3)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/355,365 Abandoned US20060185124A1 (en) | 2005-02-18 | 2006-02-16 | Joint assembly with centering flange |
US12/491,931 Abandoned US20090263181A1 (en) | 2005-02-18 | 2009-06-25 | Joint assembly with centering flange |
US13/421,849 Expired - Fee Related US8449399B2 (en) | 2005-02-18 | 2012-03-15 | Joint assembly with centering flange |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US11/355,365 Abandoned US20060185124A1 (en) | 2005-02-18 | 2006-02-16 | Joint assembly with centering flange |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US13/421,849 Expired - Fee Related US8449399B2 (en) | 2005-02-18 | 2012-03-15 | Joint assembly with centering flange |
Country Status (5)
Country | Link |
---|---|
US (3) | US20060185124A1 (en) |
EP (1) | EP1853832B1 (en) |
AT (1) | ATE471465T1 (en) |
DE (1) | DE602006014941D1 (en) |
WO (1) | WO2006089102A1 (en) |
Cited By (2)
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US20190032571A1 (en) * | 2013-06-06 | 2019-01-31 | United Technologies Corporation | Spline ring for a fan drive gear flexible support |
US20220349456A1 (en) * | 2019-06-26 | 2022-11-03 | Schaeffler Technologies AG & Co. KG | Press-fit-interlocking connection and belt tensioner having such a connection |
Families Citing this family (10)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060185124A1 (en) | 2005-02-18 | 2006-08-24 | Kozlowski Keith A | Joint assembly with centering flange |
EP2434158B1 (en) * | 2010-09-27 | 2013-08-07 | Delphi Technologies Holding S.à.r.l. | Drive shaft for a positive displacement pump |
DE102011081861A1 (en) * | 2011-05-17 | 2012-11-22 | Winergy Ag | Drive system for a wind turbine |
DE102013218192B4 (en) | 2013-09-11 | 2023-12-21 | Volkswagen Aktiengesellschaft | Constant velocity joint for attachment to a transmission flange |
US20150323040A1 (en) * | 2014-05-07 | 2015-11-12 | Schaeffler Technologies AG & Co. KG | Closed damper hub |
JP6769100B2 (en) * | 2016-05-11 | 2020-10-14 | 株式会社ジェイテクト | Manufacturing method of outer ring of constant velocity joint |
DE102017010421A1 (en) * | 2017-11-10 | 2019-05-16 | Neumayer Tekfor Engineering Gmbh | joint arrangement |
DE102018124078B4 (en) * | 2018-09-28 | 2022-11-03 | Ifa-Technologies Gmbh | Outer part for homokinetic joints and roller bearings |
US11261919B2 (en) | 2019-10-02 | 2022-03-01 | Neapco Intellectual Property Holdings, Llc | Joint assembly having a piloting cover for centering a mating flange relative to an outer race of a constant velocity joint |
KR102334359B1 (en) * | 2020-09-25 | 2021-12-06 | 엠피웍스주식회사 | Double walled gas pipes |
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Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20190032571A1 (en) * | 2013-06-06 | 2019-01-31 | United Technologies Corporation | Spline ring for a fan drive gear flexible support |
US10927768B2 (en) * | 2013-06-06 | 2021-02-23 | Raytheon Technologies Corporation | Spline ring for a fan drive gear flexible support |
US20220349456A1 (en) * | 2019-06-26 | 2022-11-03 | Schaeffler Technologies AG & Co. KG | Press-fit-interlocking connection and belt tensioner having such a connection |
DE102019117170B4 (en) | 2019-06-26 | 2023-01-12 | Schaeffler Technologies AG & Co. KG | Belt tensioner with a press-fit form-fit connection |
US12123494B2 (en) * | 2019-06-26 | 2024-10-22 | Schaeffler Technologies AG & Co. KG | Press-fit-interlocking connection and belt tensioner having such a connection |
Also Published As
Publication number | Publication date |
---|---|
US20060185124A1 (en) | 2006-08-24 |
ATE471465T1 (en) | 2010-07-15 |
US8449399B2 (en) | 2013-05-28 |
US20120237290A1 (en) | 2012-09-20 |
WO2006089102A1 (en) | 2006-08-24 |
EP1853832B1 (en) | 2010-06-16 |
DE602006014941D1 (en) | 2010-07-29 |
EP1853832A1 (en) | 2007-11-14 |
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Owner name: STEERING SOLUTIONS IP HOLDING CORPORATION, MICHIGA Free format text: ASSIGNMENT OF ASSIGNORS INTEREST;ASSIGNOR:GM GLOBAL TECHNOLOGY OPERATIONS, INC.;REEL/FRAME:028325/0709 Effective date: 20120514 |
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