US20020016208A1 - Yoke connections for universal joints - Google Patents
Yoke connections for universal joints Download PDFInfo
- Publication number
- US20020016208A1 US20020016208A1 US09/970,286 US97028601A US2002016208A1 US 20020016208 A1 US20020016208 A1 US 20020016208A1 US 97028601 A US97028601 A US 97028601A US 2002016208 A1 US2002016208 A1 US 2002016208A1
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- United States
- Prior art keywords
- yoke
- universal joint
- bearings
- bearing
- recited
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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
- 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
- F16D3/26—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected
- F16D3/38—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another
- F16D3/382—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another constructional details of other than the intermediate member
- F16D3/387—Fork construction; Mounting of fork on shaft; Adapting shaft for mounting of fork
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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
- 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
- F16D3/26—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected
- F16D3/38—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another
- F16D3/40—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another with intermediate member provided with two pairs of outwardly-directed trunnions on intersecting axes
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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
- 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
- F16D3/26—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected
- F16D3/38—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another
- F16D3/40—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another with intermediate member provided with two pairs of outwardly-directed trunnions on intersecting axes
- F16D3/41—Hooke's joints or other joints with an equivalent intermediate member to which each coupling part is pivotally or slidably connected with a single intermediate member with trunnions or bearings arranged on two axes perpendicular to one another with intermediate member provided with two pairs of outwardly-directed trunnions on intersecting axes with ball or roller bearings
Definitions
- the present invention relates to universal joints and to connection assemblies between a yoke and the shafts of a universal joint cross member.
- cross member may be preassembled with its bearings already attached.
- the cross member shaft and bearing lay in a half-circle bore in the yoke.
- Metal straps surround the bearing and are connected to the yoke with bolts. This prior art assembly requires tight dimensional control.
- the bearing is connected to the yoke with bolts.
- the mounting bolts in this universal joint connection may become loose due to the high force moments.
- small locators on the bearing may be used to transmit rotation between the bearing and yoke.
- the small locators are placed relatively far from the centerline of the shaft. The locator provides a good deal of the reaction surface for torque transmission, and the distance from the shaft centerline results in relatively high force moments.
- wing bearings support two shafts of a cross member and are bolted to a yoke.
- the yoke includes two opposed brackets, each having two arms forming a part-circular surface to receive the wing bearing and cross member shaft. The arms extend around more than 90° of the bearing's outer periphery to provide a secure engagement between the yoke and bearing.
- the bearing includes a depression on an outer wall of the bearing cup.
- the yoke bracket includes a locator finger extending between the arms of the yoke bracket, and located in the bearing depression.
- the fingers extend radially inwardly to overlay the needle bearings, and at least a portion of the shaft is received in the wing bearing. The extension places the finger relatively close to the center axis of the shaft, minimizing the moment.
- the wing bearing includes a shoulder projecting from the periphery of the bearing.
- a yoke receiving the bearing has a mating surface disposed between the bracket arms. The shoulder contacts the mating surface to provide a secure connection between the bearing and the yoke, and inhibit rotation of the bearing in the yoke.
- the yoke also includes a lip extending beyond the mating surface, and between the bracket arms to overlay a top portion of the shoulder.
- the inventive universal joint preferably combines one yoke having the prior art full circular bore mounting two shafts and a second yoke utilizing the above-described wing bearings which are bolted to the yoke.
- the universal joint manufacturer may preassemble a yoke having full circular bores onto two of the shafts of the cross member with its associated bearings. In this way, the universal joint manufacturer is able to insure proper lubrication of those bearings.
- the universal joint manufacturer may then mount the wing bearings onto the other two shafts of the cross member.
- the yoke and assembled cross member may then be shipped to the vehicle manufacturer.
- the assembler at the vehicle assembly line need only bolt the wing bearings to a second yoke.
- the benefits of the full circular bore are obtained for two of the shafts, and the benefits of utilizing a wing bearing are obtained for the other two shafts.
- the universal joint assembler mounts a conventional first yoke having full circular bores onto two of the shafts. Wing bearings are mounted on the other two shafts. That assembled yoke is then transported to the vehicle assembler.
- the vehicle assembler assembles the drive line to include the first yoke, and bolts the wing bearings onto a second yoke. In this way, the assembler at the vehicle assembly line is not required to provide any lubrication for the bearings.
- FIG. 1 is a perspective view of a universal joint in accordance with the present invention.
- FIG. 2 is an exploded perspective view of the universal joint of FIG. 1;
- FIG. 3 is a side elevation view of connection between a yoke and cross member shafts in the universal joint of FIG. 1;
- FIG. 4 is a top plan view of a connection between a yoke and cross member shafts in the universal joint of FIG. 1 with a portion cut away.
- Universal joint 20 is illustrated in FIG. 1, and incorporates two yokes 22 and 24 and a cross member 26 .
- Yokes 22 and 24 are each received on two opposing shafts of cross member 26 .
- yoke 22 includes a pair of opposing arms 25 each having a bracket 29 defining a full circular bore 32 .
- the method of connecting shafts 28 to yoke 22 includes inserting shafts 28 into bores 32 .
- Bearings 34 are then mounted onto shafts 28 by inserting a receiving cup of bearing 34 radially inwardly into bores 32 , and onto shafts 28 .
- Rings 36 are then snapped over a face 31 of bearing 34 retaining bearing 34 in bore 32 .
- yoke 24 The connection between yoke 24 and cross member 26 utilizes wing bearings 38 , as described further below.
- wing bearings 38 The connection between yoke 24 and cross member 26 utilizes wing bearings 38 , as described further below.
- the disclosed embodiment shows only one yoke utilizing wing bearings, it should be understood that some of the benefits disclosed in this application may apply to universal joints where both yokes use wing bearings.
- Yokes 22 and 24 are each connected to drive shafts 23 .
- Cross member 26 includes two pairs of shafts 28 and 30 .
- the shafts in each pair are spaced 180° from the other.
- Shafts 28 are spaced 90° from shafts 30 .
- a wing bearing 38 is mounted onto each shaft 30 .
- Wing bearing 38 has a bearing receiving cup 40 and a pair of opposed wings 42 , each having a bolt hole 44 .
- Wing bearings 38 also include a depression 46 formed on an outer face.
- Yoke 24 includes two opposed brackets 50 which each receive a wing bearing 38 .
- Bracket 50 includes a pair of arms 52 , which each include a threaded bore 54 .
- a finger 56 extends between arms 52 of each bracket 50 .
- a mating surface 62 is disposed between bracket arms 52 adjacent locator finger 56 .
- bolts 58 pass through wing bearing bolt holes 44 and are threadably received in threaded bores 54 to secure wing bearing 38 , and thus shaft 30 to yoke 24 .
- Finger 56 of bracket 50 is received in depression 46 of wing bearing 38 .
- finger 56 helps to properly locate wing bearing 38 in bracket 50 of yoke 24 .
- Finger 56 also provides a main contact surface to transmit forces between the yoke and bearing during rotation. That is, a main reaction plane of the forces between the yoke and bearing during rotation is defined at the finger 56 .
- the reaction plane has been spaced radially outwardly from the nominal outer periphery of the needle bearing surfaces. As such, a relatively large force moment is created between that reaction plane and the centerline of the shaft. This is undesirable. With applicant's invention of finger 56 extending radially inwardly over the wing bearings 38 , the force moment has been greatly reduced.
- bearing 38 includes a shoulder 60 which projects from a periphery and between wings 42 .
- Shoulder 60 spans at least 45° around the periphery of wing bearing 38 , as measured from the centerline of shaft 30 .
- shoulder 60 spans between 90° and 120° around the periphery of bearing 38 .
- shoulder 60 spans approximately 100° around the periphery of bearing 38 .
- Bearing 38 is received between bracket arms 52 , and shoulder 60 contacts mating surface 62 of bracket 50 . Mating surface 62 helps align bearing 38 and also cooperates with mating surface 62 to prevent bearing 38 from rotating in bracket 50 , thereby reducing forces which tend to loosen the bolts 58 .
- Bracket arms 52 extend forward of bracket 50 and at least partially surround shafts 30 to provide additional stability. The distance between arms 52 and the centerline of shaft 30 is significantly reduced. Preferably, ends 63 of arms 52 are spaced by at least 90° measured about the periphery of shaft 30 . Thus, the arms 52 surround wing bearing 38 , providing a secure connection.
- Lip 64 extends between bracket arms 52 and outwardly of mating surface 62 to overlay a top portion of shoulder 60 of wing bearing 38 . Lips 64 of opposed brackets 50 provide additional vibrational stability to the universal joint 20 by constraining wing bearings 38 .
- Finger 56 extends into depression 46 , which extends over needle bearings 66 , and at least a portion of shaft 30 to provide additional stability as described above. By extending over needle bearings 66 and at least a portion of shaft 30 , finger 56 reduces the distance between the reaction plane and the centerline of shaft 30 and finger 56 .
- a cross member 26 is initially inserted into a yoke 25 that has full circular bores 32 .
- Bearings 34 are then moved inwardly through the bore 32 to secure the cross member 26 within yoke 25 .
- Rings 36 are then driven inwardly through the bore 32 to secure bearings 34 within their respective bores 32 .
- Wing bearings 38 are mounted on the shafts 30 of cross member 26 .
- the assembled yoke 25 and cross member 26 may then be shipped.
- vehicle assemblers need only bolt the wing bearings 38 to the second yoke 24 .
- the vehicle assembler need not remove any bearing from the cross member, and further must only bolt one set of bearings to a yoke.
- the yoke 25 utilizes the prior art full circular bores 32 , which provide a very secure and desirable connection.
- the vehicle assembler since the assembler need not add any bearings onto the shafts 28 or 30 , the vehicle assembler is not involved in the lubrication of the universal joint bearing. For that reason, the universal joint manufacturer may insure proper lubrication of the bearing, and may lubricate the bearing such that maintenance and routine further lubrication of the universal joint should not be necessary during the expected life of the universal joint. This is a valuable benefit.
Abstract
Description
- The present invention relates to universal joints and to connection assemblies between a yoke and the shafts of a universal joint cross member.
- Modern vehicles are often equipped with universal joints that comprise a cross member having four shafts or trunnions. Bearings are mounted on each shaft, and two yokes are mounted onto opposed pairs of shafts. The yokes are mounted at positions spaced 90° relative to each other and are each connected to drive shafts. This arrangement allows rotation to be transmitted through varying angles between the drive shafts, through varying angles. This type of universal joint is particularly popular in heavy duty vehicles such as trucks.
- Universal joint assemblies experience a great deal of stress and vibration and are exposed to a hostile environment on the underside of a vehicle. Thus, the connection between the yoke and the bearings should be secure and stable. Proper functioning of a universal joint also requires adequate lubrication between the bearings and the shafts. The universal joint designs utilized in the past have not always achieved these goals for yoke and cross member connections.
- Conventionally, universal joints have utilized yokes that have full circular or cylindrical bores to receive a bearing and shaft. The full circular bore surrounds and supports the bearing during operation of the universal joint. Typically, the two shafts on the cross member are inserted within the bores in the yoke. The bearings are then inserted radially inwardly through the outer end of the bore and onto the shafts.
- One problem with this arrangement is that since the bearings are inserted through the bores in the yoke after insertion of the shafts, the universal joint manufacturer has been unable to finally mount the bearings on the cross member shafts. Rather, the bearings must be mounted on the shaft at the vehicle assembly line. Typically, the assemblers at the vehicle assembly line are not as skilled in proper lubrication or assembly of universal joint bearings as assemblers at the universal joint manufacturer. For that reason, there has sometimes been improper lubrication or assembly of universal joints assembled on the assembly line.
- To address this problem, universal joints have been developed wherein the cross member may be preassembled with its bearings already attached. In one prior art universal joint, the cross member shaft and bearing lay in a half-circle bore in the yoke. Metal straps surround the bearing and are connected to the yoke with bolts. This prior art assembly requires tight dimensional control.
- In another prior art design, the bearing is connected to the yoke with bolts. The mounting bolts in this universal joint connection may become loose due to the high force moments. With either type of assembly, small locators on the bearing may be used to transmit rotation between the bearing and yoke. The small locators are placed relatively far from the centerline of the shaft. The locator provides a good deal of the reaction surface for torque transmission, and the distance from the shaft centerline results in relatively high force moments.
- In a disclosed embodiment of the present invention, wing bearings support two shafts of a cross member and are bolted to a yoke. The yoke includes two opposed brackets, each having two arms forming a part-circular surface to receive the wing bearing and cross member shaft. The arms extend around more than 90° of the bearing's outer periphery to provide a secure engagement between the yoke and bearing. The bearing includes a depression on an outer wall of the bearing cup. The yoke bracket includes a locator finger extending between the arms of the yoke bracket, and located in the bearing depression. Preferably, the fingers extend radially inwardly to overlay the needle bearings, and at least a portion of the shaft is received in the wing bearing. The extension places the finger relatively close to the center axis of the shaft, minimizing the moment.
- In another feature of the invention, the wing bearing includes a shoulder projecting from the periphery of the bearing. A yoke receiving the bearing has a mating surface disposed between the bracket arms. The shoulder contacts the mating surface to provide a secure connection between the bearing and the yoke, and inhibit rotation of the bearing in the yoke. In a preferred embodiment, the yoke also includes a lip extending beyond the mating surface, and between the bracket arms to overlay a top portion of the shoulder.
- The inventive universal joint preferably combines one yoke having the prior art full circular bore mounting two shafts and a second yoke utilizing the above-described wing bearings which are bolted to the yoke. The universal joint manufacturer may preassemble a yoke having full circular bores onto two of the shafts of the cross member with its associated bearings. In this way, the universal joint manufacturer is able to insure proper lubrication of those bearings. The universal joint manufacturer may then mount the wing bearings onto the other two shafts of the cross member. The yoke and assembled cross member may then be shipped to the vehicle manufacturer. When the vehicle manufacturer assembles the drive line of the vehicle, the assembler at the vehicle assembly line need only bolt the wing bearings to a second yoke. Thus, the benefits of the full circular bore are obtained for two of the shafts, and the benefits of utilizing a wing bearing are obtained for the other two shafts.
- In a method of assembling a universal joint utilizing the present invention, the universal joint assembler mounts a conventional first yoke having full circular bores onto two of the shafts. Wing bearings are mounted on the other two shafts. That assembled yoke is then transported to the vehicle assembler. The vehicle assembler assembles the drive line to include the first yoke, and bolts the wing bearings onto a second yoke. In this way, the assembler at the vehicle assembly line is not required to provide any lubrication for the bearings.
- With this inventive solution, applicant has developed universal joints that require no maintenance lubrication. By insuring the proper lubrication is provided at the initial assembly, no routine lubrication maintenance is required. Thus, once assembled, the universal joint will be permanently lubricated for its expected life.
- These and other features of the present invention will be best understood from the following specification and drawings, of which the following is a brief description.
- FIG. 1 is a perspective view of a universal joint in accordance with the present invention;
- FIG. 2 is an exploded perspective view of the universal joint of FIG. 1;
- FIG. 3 is a side elevation view of connection between a yoke and cross member shafts in the universal joint of FIG. 1; and
- FIG. 4 is a top plan view of a connection between a yoke and cross member shafts in the universal joint of FIG. 1 with a portion cut away.
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Universal joint 20 is illustrated in FIG. 1, and incorporates twoyokes cross member 26. Yokes 22 and 24 are each received on two opposing shafts ofcross member 26. - The connection between
yoke 22 andcross member 26 is conventional. As shown in FIG. 2,yoke 22 includes a pair of opposingarms 25 each having abracket 29 defining a full circular bore 32. The method of connecting shafts 28 toyoke 22 includes inserting shafts 28 intobores 32.Bearings 34 are then mounted onto shafts 28 by inserting a receiving cup of bearing 34 radially inwardly intobores 32, and onto shafts 28.Rings 36 are then snapped over aface 31 of bearing 34 retainingbearing 34 inbore 32. - The connection between
yoke 24 andcross member 26 utilizeswing bearings 38, as described further below. Although, the disclosed embodiment shows only one yoke utilizing wing bearings, it should be understood that some of the benefits disclosed in this application may apply to universal joints where both yokes use wing bearings.Yokes shafts 23. -
Cross member 26 includes two pairs ofshafts 28 and 30. The shafts in each pair are spaced 180° from the other. Shafts 28 are spaced 90° fromshafts 30. Awing bearing 38 is mounted onto eachshaft 30.Wing bearing 38 has abearing receiving cup 40 and a pair ofopposed wings 42, each having abolt hole 44.Wing bearings 38 also include adepression 46 formed on an outer face. -
Yoke 24 includes twoopposed brackets 50 which each receive awing bearing 38.Bracket 50 includes a pair ofarms 52, which each include a threadedbore 54. Afinger 56 extends betweenarms 52 of eachbracket 50. Amating surface 62 is disposed betweenbracket arms 52adjacent locator finger 56. - As shown in FIG. 3,
bolts 58 pass through wing bearing bolt holes 44 and are threadably received in threadedbores 54 to securewing bearing 38, and thusshaft 30 toyoke 24.Finger 56 ofbracket 50 is received indepression 46 ofwing bearing 38. During assembly of universal joint 20,finger 56 helps to properly locatewing bearing 38 inbracket 50 ofyoke 24. -
Finger 56 also provides a main contact surface to transmit forces between the yoke and bearing during rotation. That is, a main reaction plane of the forces between the yoke and bearing during rotation is defined at thefinger 56. In prior art wing bearings, the reaction plane has been spaced radially outwardly from the nominal outer periphery of the needle bearing surfaces. As such, a relatively large force moment is created between that reaction plane and the centerline of the shaft. This is undesirable. With applicant's invention offinger 56 extending radially inwardly over thewing bearings 38, the force moment has been greatly reduced. - As shown in FIG. 4, bearing38 includes a shoulder 60 which projects from a periphery and between
wings 42. Shoulder 60 spans at least 45° around the periphery ofwing bearing 38, as measured from the centerline ofshaft 30. Preferably, shoulder 60 spans between 90° and 120° around the periphery of bearing 38. In one embodiment, shoulder 60 spans approximately 100° around the periphery of bearing 38.Bearing 38 is received betweenbracket arms 52, and shoulder 60contacts mating surface 62 ofbracket 50.Mating surface 62 helps alignbearing 38 and also cooperates withmating surface 62 to prevent bearing 38 from rotating inbracket 50, thereby reducing forces which tend to loosen thebolts 58. -
Bracket arms 52 extend forward ofbracket 50 and at least partially surroundshafts 30 to provide additional stability. The distance betweenarms 52 and the centerline ofshaft 30 is significantly reduced. Preferably, ends 63 ofarms 52 are spaced by at least 90° measured about the periphery ofshaft 30. Thus, thearms 52surround wing bearing 38, providing a secure connection. - Lip64 extends between
bracket arms 52 and outwardly ofmating surface 62 to overlay a top portion of shoulder 60 ofwing bearing 38. Lips 64 ofopposed brackets 50 provide additional vibrational stability to the universal joint 20 by constrainingwing bearings 38. -
Finger 56 extends intodepression 46, which extends over needle bearings 66, and at least a portion ofshaft 30 to provide additional stability as described above. By extending over needle bearings 66 and at least a portion ofshaft 30,finger 56 reduces the distance between the reaction plane and the centerline ofshaft 30 andfinger 56. - There are mating surfaces shown at70 between the bearing and the yoke. Those mating surfaces 70 and the
finger 56 anddepression 46 are the only machined surfaces. The bearings and yokes are otherwise as forged or cast. Surfaces 70 provide additional guidance. - In a method of assembling a universal joint according to the present invention, a
cross member 26 is initially inserted into ayoke 25 that has full circular bores 32.Bearings 34 are then moved inwardly through thebore 32 to secure thecross member 26 withinyoke 25.Rings 36 are then driven inwardly through thebore 32 to securebearings 34 within theirrespective bores 32. -
Wing bearings 38 are mounted on theshafts 30 ofcross member 26. The assembledyoke 25 andcross member 26 may then be shipped. At a vehicle assembly line, vehicle assemblers need only bolt thewing bearings 38 to thesecond yoke 24. The vehicle assembler need not remove any bearing from the cross member, and further must only bolt one set of bearings to a yoke. Theyoke 25 utilizes the prior art full circular bores 32, which provide a very secure and desirable connection. At the same time, since the assembler need not add any bearings onto theshafts 28 or 30, the vehicle assembler is not involved in the lubrication of the universal joint bearing. For that reason, the universal joint manufacturer may insure proper lubrication of the bearing, and may lubricate the bearing such that maintenance and routine further lubrication of the universal joint should not be necessary during the expected life of the universal joint. This is a valuable benefit. - A preferred description of this invention has been disclosed; however, a worker of ordinary skill in the art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.
Claims (20)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
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US09/970,286 US6454656B2 (en) | 1995-03-31 | 2001-10-02 | Yoke connections for universal joints |
Applications Claiming Priority (3)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US41452995A | 1995-03-31 | 1995-03-31 | |
US08/764,736 US6328654B1 (en) | 1995-03-31 | 1996-12-05 | Combined wing bearing and full circular bearing yoke connection for universal joint |
US09/970,286 US6454656B2 (en) | 1995-03-31 | 2001-10-02 | Yoke connections for universal joints |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US08/764,736 Continuation US6328654B1 (en) | 1995-03-31 | 1996-12-05 | Combined wing bearing and full circular bearing yoke connection for universal joint |
Publications (2)
Publication Number | Publication Date |
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US20020016208A1 true US20020016208A1 (en) | 2002-02-07 |
US6454656B2 US6454656B2 (en) | 2002-09-24 |
Family
ID=23641853
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US08/764,736 Expired - Lifetime US6328654B1 (en) | 1995-03-31 | 1996-12-05 | Combined wing bearing and full circular bearing yoke connection for universal joint |
US09/970,286 Expired - Lifetime US6454656B2 (en) | 1995-03-31 | 2001-10-02 | Yoke connections for universal joints |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US08/764,736 Expired - Lifetime US6328654B1 (en) | 1995-03-31 | 1996-12-05 | Combined wing bearing and full circular bearing yoke connection for universal joint |
Country Status (3)
Country | Link |
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US (2) | US6328654B1 (en) |
AU (1) | AU5528296A (en) |
WO (1) | WO1996030666A1 (en) |
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US20060183555A1 (en) * | 2005-02-11 | 2006-08-17 | Norbert Gross | Insulation For A Universal Cross Joint |
WO2022200981A1 (en) * | 2021-03-24 | 2022-09-29 | Cilag Gmbh International | Multi-axis pivot joints for surgical instruments and methods for manufacturing same |
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Families Citing this family (153)
Publication number | Priority date | Publication date | Assignee | Title |
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AU5528296A (en) * | 1995-03-31 | 1996-10-16 | Rockwell International Corporation | Yoke connections for universal joints |
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US11857181B2 (en) | 2007-06-04 | 2024-01-02 | Cilag Gmbh International | Robotically-controlled shaft based rotary drive systems for surgical instruments |
US11849941B2 (en) | 2007-06-29 | 2023-12-26 | Cilag Gmbh International | Staple cartridge having staple cavities extending at a transverse angle relative to a longitudinal cartridge axis |
US7887422B2 (en) | 2007-08-02 | 2011-02-15 | American Axle & Manufacturing, Inc. | Universal joint with bearing cup retention mechanism |
US8636736B2 (en) | 2008-02-14 | 2014-01-28 | Ethicon Endo-Surgery, Inc. | Motorized surgical cutting and fastening instrument |
RU2493788C2 (en) | 2008-02-14 | 2013-09-27 | Этикон Эндо-Серджери, Инк. | Surgical cutting and fixing instrument, which has radio-frequency electrodes |
US8210411B2 (en) | 2008-09-23 | 2012-07-03 | Ethicon Endo-Surgery, Inc. | Motor-driven surgical cutting instrument |
US9005230B2 (en) | 2008-09-23 | 2015-04-14 | Ethicon Endo-Surgery, Inc. | Motorized surgical instrument |
US11648005B2 (en) | 2008-09-23 | 2023-05-16 | Cilag Gmbh International | Robotically-controlled motorized surgical instrument with an end effector |
US9386983B2 (en) | 2008-09-23 | 2016-07-12 | Ethicon Endo-Surgery, Llc | Robotically-controlled motorized surgical instrument |
US8608045B2 (en) | 2008-10-10 | 2013-12-17 | Ethicon Endo-Sugery, Inc. | Powered surgical cutting and stapling apparatus with manually retractable firing system |
US20110011206A1 (en) * | 2009-07-14 | 2011-01-20 | Knight Donn C | Driveline yoke with brake rotor |
US9309928B2 (en) | 2010-08-04 | 2016-04-12 | Arvinmeritor Technology, Llc | Yoke with stiffness ring |
US9386988B2 (en) | 2010-09-30 | 2016-07-12 | Ethicon End-Surgery, LLC | Retainer assembly including a tissue thickness compensator |
US8740038B2 (en) | 2010-09-30 | 2014-06-03 | Ethicon Endo-Surgery, Inc. | Staple cartridge comprising a releasable portion |
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US11812965B2 (en) | 2010-09-30 | 2023-11-14 | Cilag Gmbh International | Layer of material for a surgical end effector |
US9566061B2 (en) | 2010-09-30 | 2017-02-14 | Ethicon Endo-Surgery, Llc | Fastener cartridge comprising a releasably attached tissue thickness compensator |
US11925354B2 (en) | 2010-09-30 | 2024-03-12 | Cilag Gmbh International | Staple cartridge comprising staples positioned within a compressible portion thereof |
US9629814B2 (en) | 2010-09-30 | 2017-04-25 | Ethicon Endo-Surgery, Llc | Tissue thickness compensator configured to redistribute compressive forces |
AU2012250197B2 (en) | 2011-04-29 | 2017-08-10 | Ethicon Endo-Surgery, Inc. | Staple cartridge comprising staples positioned within a compressible portion thereof |
JP6105041B2 (en) | 2012-03-28 | 2017-03-29 | エシコン・エンド−サージェリィ・インコーポレイテッドEthicon Endo−Surgery,Inc. | Tissue thickness compensator containing capsules defining a low pressure environment |
BR112014024102B1 (en) | 2012-03-28 | 2022-03-03 | Ethicon Endo-Surgery, Inc | CLAMP CARTRIDGE ASSEMBLY FOR A SURGICAL INSTRUMENT AND END ACTUATOR ASSEMBLY FOR A SURGICAL INSTRUMENT |
US9101358B2 (en) | 2012-06-15 | 2015-08-11 | Ethicon Endo-Surgery, Inc. | Articulatable surgical instrument comprising a firing drive |
US20140001231A1 (en) | 2012-06-28 | 2014-01-02 | Ethicon Endo-Surgery, Inc. | Firing system lockout arrangements for surgical instruments |
US9289256B2 (en) | 2012-06-28 | 2016-03-22 | Ethicon Endo-Surgery, Llc | Surgical end effectors having angled tissue-contacting surfaces |
BR112015021098B1 (en) | 2013-03-01 | 2022-02-15 | Ethicon Endo-Surgery, Inc | COVERAGE FOR A JOINT JOINT AND SURGICAL INSTRUMENT |
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US9775609B2 (en) | 2013-08-23 | 2017-10-03 | Ethicon Llc | Tamper proof circuit for surgical instrument battery pack |
JP6636452B2 (en) | 2014-04-16 | 2020-01-29 | エシコン エルエルシーEthicon LLC | Fastener cartridge including extension having different configurations |
US20150297225A1 (en) | 2014-04-16 | 2015-10-22 | Ethicon Endo-Surgery, Inc. | Fastener cartridges including extensions having different configurations |
JP6532889B2 (en) | 2014-04-16 | 2019-06-19 | エシコン エルエルシーEthicon LLC | Fastener cartridge assembly and staple holder cover arrangement |
BR112017004361B1 (en) | 2014-09-05 | 2023-04-11 | Ethicon Llc | ELECTRONIC SYSTEM FOR A SURGICAL INSTRUMENT |
US20160066913A1 (en) | 2014-09-05 | 2016-03-10 | Ethicon Endo-Surgery, Inc. | Local display of tissue parameter stabilization |
US9924944B2 (en) | 2014-10-16 | 2018-03-27 | Ethicon Llc | Staple cartridge comprising an adjunct material |
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US10245027B2 (en) | 2014-12-18 | 2019-04-02 | Ethicon Llc | Surgical instrument with an anvil that is selectively movable about a discrete non-movable axis relative to a staple cartridge |
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JP2020121162A (en) | 2015-03-06 | 2020-08-13 | エシコン エルエルシーEthicon LLC | Time dependent evaluation of sensor data to determine stability element, creep element and viscoelastic element of measurement |
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US10105139B2 (en) | 2015-09-23 | 2018-10-23 | Ethicon Llc | Surgical stapler having downstream current-based motor control |
US11890015B2 (en) | 2015-09-30 | 2024-02-06 | Cilag Gmbh International | Compressible adjunct with crossing spacer fibers |
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US10292704B2 (en) | 2015-12-30 | 2019-05-21 | Ethicon Llc | Mechanisms for compensating for battery pack failure in powered surgical instruments |
US11213293B2 (en) | 2016-02-09 | 2022-01-04 | Cilag Gmbh International | Articulatable surgical instruments with single articulation link arrangements |
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US20170296173A1 (en) | 2016-04-18 | 2017-10-19 | Ethicon Endo-Surgery, Llc | Method for operating a surgical instrument |
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US10758230B2 (en) | 2016-12-21 | 2020-09-01 | Ethicon Llc | Surgical instrument with primary and safety processors |
US10537325B2 (en) | 2016-12-21 | 2020-01-21 | Ethicon Llc | Staple forming pocket arrangement to accommodate different types of staples |
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CN107355485A (en) * | 2017-05-27 | 2017-11-17 | 镇江远大传动机械有限公司 | A kind of universal joint |
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US20220378425A1 (en) | 2021-05-28 | 2022-12-01 | Cilag Gmbh International | Stapling instrument comprising a control system that controls a firing stroke length |
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Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1985531A (en) * | 1932-06-06 | 1934-12-25 | Carl E Swenson | Method of making universal joints |
US2161234A (en) * | 1937-02-17 | 1939-06-06 | Joseph E Padgett | Universal joint |
US2212763A (en) * | 1939-10-16 | 1940-08-27 | Universal Products Co Inc | Universal joint |
FR1050969A (en) * | 1951-02-21 | 1954-01-12 | Borg Warner | Improvements relating to a universal joint |
US2698527A (en) * | 1951-08-15 | 1955-01-04 | Borg Warner | Universal joint assembly |
US3423958A (en) * | 1967-01-09 | 1969-01-28 | Robert K Koelling | Flexible coupling assembly and couplings therefor |
US3645115A (en) * | 1970-10-05 | 1972-02-29 | Caterpillar Tractor Co | Universal joint with laminate bearings |
JPS5238004A (en) * | 1975-08-18 | 1977-03-24 | Kubota Ltd | Method of producing composite board made of woody plywood and asbestos cement board |
US4575361A (en) * | 1985-01-07 | 1986-03-11 | Dana Corporation | Universal joint yoke |
US5035676A (en) * | 1985-06-13 | 1991-07-30 | Morgan Construction Company | Split yoke universal joint |
US4710038A (en) * | 1985-12-02 | 1987-12-01 | Dana Corporation | Bearing cap assembly |
FR2597940B1 (en) * | 1986-04-28 | 1990-05-25 | Glaenzer Spicer Sa | CARDAN JOINT WITH FRONT GROOVED BEARINGS |
US4881924A (en) * | 1987-12-07 | 1989-11-21 | Dana Corporation | Yoke for Hookes-type universal joint |
US5000609A (en) * | 1987-12-23 | 1991-03-19 | Dana Corporation | Retainer for universal joint bearing cups |
US5376051A (en) * | 1991-05-06 | 1994-12-27 | Dana Corporation | Bearing cup and retainer strap for universal joint |
US5178584A (en) * | 1991-09-13 | 1993-01-12 | Rockford Powertrain, Inc. | Driveline yoke with headed pin for captivating a universal joint cross |
AU5528296A (en) * | 1995-03-31 | 1996-10-16 | Rockwell International Corporation | Yoke connections for universal joints |
US5647799A (en) * | 1995-06-15 | 1997-07-15 | Dana Corporation | Bearing cap for universal joint having anti-rotation protrusions |
US5643090A (en) * | 1995-12-26 | 1997-07-01 | Dana Corporation | Strap for retaining a bearing cup in a universal joint assembly |
-
1996
- 1996-03-27 AU AU55282/96A patent/AU5528296A/en not_active Abandoned
- 1996-03-27 WO PCT/US1996/004181 patent/WO1996030666A1/en active Application Filing
- 1996-12-05 US US08/764,736 patent/US6328654B1/en not_active Expired - Lifetime
-
2001
- 2001-10-02 US US09/970,286 patent/US6454656B2/en not_active Expired - Lifetime
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US20060183555A1 (en) * | 2005-02-11 | 2006-08-17 | Norbert Gross | Insulation For A Universal Cross Joint |
US7445554B2 (en) * | 2005-02-11 | 2008-11-04 | Ford Global Technologies, Llc | Insulation for a universal cross joint |
WO2022200981A1 (en) * | 2021-03-24 | 2022-09-29 | Cilag Gmbh International | Multi-axis pivot joints for surgical instruments and methods for manufacturing same |
US11944336B2 (en) | 2021-03-24 | 2024-04-02 | Cilag Gmbh International | Joint arrangements for multi-planar alignment and support of operational drive shafts in articulatable surgical instruments |
Also Published As
Publication number | Publication date |
---|---|
AU5528296A (en) | 1996-10-16 |
US6328654B1 (en) | 2001-12-11 |
WO1996030666A1 (en) | 1996-10-03 |
US6454656B2 (en) | 2002-09-24 |
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