Continuously variable transmission

Abstract
Components, subassemblies, systems, and/or methods for continuously variable transmissions (CVT) are provided. In one embodiment, a CVT has a number of spherical planets in contact with an idler assembly. Various idler assemblies can be used to facilitate to improve durability, fatigue life, and efficiency of a CVT. In one embodiment, the idler assembly has two rolling elements having contact surfaces that are angled with respect to a longitudinal axis of the CVT. In some embodiments, a bearing is operably coupled between the first and second rolling elements. The bearing is configured to balance axial force between the first and second rolling elements. In one embodiment, the bearing is a ball bearing. In another embodiment, the bearing is an angular contact bearing. In yet other embodiments, needle roller bearings are employed.
Description
BACKGROUND

Field of the Invention


This disclosure relates generally to mechanical and/or electro-mechanical power modulation devices and methods. More particularly, this disclosure relates to continuously and/or infinitely variable, planetary power modulating devices, and methods for modulating power flow in a power train or drive, such as power flow from a prime mover to one or more auxiliary or driven devices.


Description of the Related Art


Continuously variable transmissions (CVT) having spherical planets such as those generally described in U.S. Pat. No. 7,011,600 to Miller et al, U.S. Pat. No. 5,236,403 to Schievelbusch, or U.S. Pat. No. 2,469,653 to Kopp, typically have a rotatable support member or an idler component in contact with each spherical planet. In some systems, the idler is a generally cylindrical member located radially inward of each spherical planet. During operation of these types of CVTs, the spherical planets exert forces on the idler that generate high stress at the location contacting the spherical planets. The type of stress is commonly known as a hertzian contact stress. Fatigue life and/or durability of a rolling element, such as an idler, is a function of the hertzian stress exerted on the rolling element over time. High stress exerted on the idler component leads to lower fatigue life and lower efficiency performance of the CVT.


Thus, there exists a continuing need for devices and methods to improve the fatigue life of idler components. Embodiments of power modulating devices and/or drivetrains described below address one or more of these needs.


SUMMARY OF THE INVENTION

The systems and methods herein described have several features, no single one of which is solely responsible for its desirable attributes. Without limiting the scope as expressed by the claims that follow, its more prominent features will now be discussed briefly. After considering this discussion, and particularly after reading the section entitled “Detailed Description of Certain Embodiments” one will understand how the features of the system and methods provide several advantages over traditional systems and methods.


One aspect of the disclosure relates to a continuously variable transmission (CVT) having a longitudinal axis. In one embodiment, the CVT includes a group of spherical traction planets. Each traction planet has an axle about which it rotates. The axle is configured to tilt with respect to the longitudinal axis. The CVT includes an idler assembly in contact with each of the traction planets. In one embodiment, the idler assembly is located radially inward of each of the traction planets. The idler assembly has first and second rolling elements. The first and second rolling elements are configured to rotate at different speeds corresponding to the tilt of the traction planets.


Another aspect of the disclosure relates to a continuously variable transmission (CVT) having a group of traction planet assemblies arranged angularly about a longitudinal axis of the CVT. In one embodiment, the CVT includes a first carrier coupled to the each of the traction planet assemblies. The first carrier is provided with a number of radially offset slots. The first carrier is configured to guide the traction planet assemblies. The CVT also includes an idler assembly in contact with each of the traction planets. The idler assembly is located radially inward of each traction planet. The idler assembly has first and second rolling elements.


Yet another aspect of the disclosure relates to a continuously variable accessory drive system (CVAD). In one embodiment, the CVAD has a shaft arranged along a longitudinal axis of the CVAD. The CVAD includes a first traction ring coaxial about the longitudinal axis. The CVAD also includes a group of traction planets in contact with the first traction ring. The traction planets are arranged angularly about the longitudinal axis. In one embodiment, the CVAD includes a carrier operably coupled to the each of the traction planets. The carrier is provided with a number of radially offset guide slots. The CVAD also includes an idler assembly in contact with each of the traction planets. The idler assembly is located radially inward of each traction planet. The idler assembly has first and second rolling elements. The CVAD includes an alternator coupled to the shaft.


One aspect of the invention relates to an idler assembly for a continuously variable transmission (CVT) having a group of traction planet assemblies arranged about a longitudinal axis. Each traction planet assembly is operably coupled to a carrier having a number of radially offset guide slots. In one embodiment, the idler assembly includes first and second rolling elements in contact with each traction planet assembly. The first and second rolling elements are located radially inward of each traction planet assembly. The idler assembly also includes a bearing operably coupling the first rolling element to the second rolling element. The bearing is configured to balance axial force between the first and second rolling elements.





BRIEF DESCRIPTION OF THE FIGURES


FIG. 1 is a cross-sectional view of an embodiment of a continuously variable accessory drive (CVAD) having a skew control system.



FIG. 2 is a partially cross-sectional perspective view of certain components of the CVAD of FIG. 1.



FIG. 3 is a cross-sectional exploded view of an idler assembly that can be used with the CVAD of FIG. 1.



FIG. 4 is a plan view of a carrier that can be used with the CVAD of FIG. 1.



FIG. 5 is a plan view of a carrier that can be used with the CVAD of FIG. 1.



FIG. 6 is a diagram of one embodiment of an idler assembly that can be used with the CVAD of FIG. 1.



FIG. 7 is a diagram of one embodiment of an idler assembly that can be used with the CVAD of FIG. 1.



FIG. 8 is a diagram of one embodiment of an idler assembly that can be used with the CVAD of FIG. 1.





DETAILED DESCRIPTION OF CERTAIN EMBODIMENTS

The preferred embodiments will be described now with reference to the accompanying figures, wherein like numerals refer to like elements throughout. The terminology used in the descriptions below is not to be interpreted in any limited or restrictive manner simply because it is used in conjunction with detailed descriptions of certain specific embodiments. Furthermore, embodiments of the disclosure can include several novel features, no single one of which is solely responsible for its desirable attributes or which is essential to practicing the embodiments described. Certain CVT embodiments described here are generally related to the type disclosed in U.S. Pat. Nos. 6,241,636; 6,419,608; 6,689,012; 7,011,600; 7,166,052; U.S. patent application Ser. No. 11/243,484; Ser. No. 11/543,311; Ser. No. 12/198,402, Ser. No. 12/251,325; and Patent Cooperation Treaty patent applications PCT/US2007/023315, PCT/IB2006/054911, PCT/US2008/068929, and PCT/US2007/023315, PCT/US2008/074496. The entire disclosures of each of these patents and patent applications are hereby incorporated herein by reference.


As used here, the terms “operationally connected,” “operationally coupled,” “operationally linked,” “operably connected,” “operably coupled,” “operably linked,” and like terms, refer to a relationship (mechanical, linkage, coupling, etc.) between elements whereby operation of one element results in a corresponding, following, or simultaneous operation or actuation of a second element. It is noted that in using said terms to describe certain embodiments, specific structures or mechanisms that link or couple the elements are typically described. However, unless otherwise specifically stated, when one of said terms is used, the term indicates that the actual linkage or coupling may take a variety of forms, which in certain instances will be readily apparent to a person of ordinary skill in the relevant technology. For description purposes, the term “axial” as used here refers to a direction or position along an axis that is parallel to a main or longitudinal axis of a transmission or variator. The term “radial” is used here to indicate a direction or position that is perpendicular relative to a longitudinal axis of a transmission or variator.


It should be noted that reference herein to “traction” does not exclude applications where the dominant or exclusive mode of power transfer is through “friction.” Without attempting to establish a categorical difference between traction and friction drives here, generally these may be understood as different regimes of power transfer. Traction drives usually involve the transfer of power between two elements by shear forces in a thin fluid layer trapped between the elements. The fluids used in these applications usually exhibit traction coefficients greater than conventional mineral oils. The traction coefficient (μ) represents the maximum available traction forces which would be available at the interfaces of the contacting components and is a measure of the maximum available drive torque. Typically, friction drives generally relate to transferring power between two elements by frictional forces between the elements. For the purposes of this disclosure, it should be understood that the CVTs described here may operate in both tractive and frictional applications. For example, in the embodiment where a CVT is used for a bicycle application, the CVT can operate at times as a friction drive and at other times as a traction drive, depending on the torque and speed conditions present during operation.


Embodiments disclosed here are related to the control of a variator and/or a CVT using generally spherical planets each having a tiltable axis of rotation that can be adjusted to achieve a desired ratio of input speed to output speed during operation. In some embodiments, adjustment of said axis of rotation involves angular displacement of the planet axis in a first plane in order to achieve an angular adjustment of the planet axis in a second plane, wherein the second plane is substantially perpendicular to the first plane. The angular displacement in the first plane is referred to here as “skew,” “skew angle,” and/or “skew condition”. For discussion purposes, the first plane is generally parallel to a longitudinal axis of the variator and/or the CVT. The second plane can be generally perpendicular to the longitudinal axis. In one embodiment, a control system coordinates the use of a skew angle to generate forces between certain contacting components in the variator that will tilt the planet axis of rotation substantially in the second plane. The tilting of the planet axis of rotation adjusts the speed ratio of the variator. The aforementioned skew angle, or skew condition, can be applied in a plane substantially perpendicular to the plane of the page of FIG. 1, for example. Embodiments of transmissions employing certain skew control systems for attaining a desired speed ratio of a variator will be discussed.


One aspect of the torque/speed regulating devices disclosed here relates to drive systems wherein a prime mover drives various driven devices. In this sense, regulating is used to mean varying the transmission ratio to vary the torque or speed of the power being provided to the accessory to correspond with the operating requirements of the accessory being driven from the CVT. The prime mover can be, for example, an electrical motor and/or an internal combustion engine. For purposes of description here, an accessory includes any machine or device that can be powered by a prime mover. For purposes of illustration and not limitation, said machine or device can be a power takeoff device (PTO), pump, compressor, generator, auxiliary electric motor, etc. Accessory devices configured to be driven by a prime mover may also include alternators, water pumps, power steering pumps, fuel pumps, oil pumps, air conditioning compressors, cooling fans, superchargers, turbochargers and any other device that is typically powered by an automobile engine. As previously stated, usually, the speed of a prime mover varies as the speed or power requirements change; however, in many cases the accessories operate optimally at a given, substantially constant speed. Embodiments of the torque/speed regulating devices disclosed here can be used to control the speed of the power delivered to the accessories powered by a prime mover.


For example, in some embodiments, the speed regulators disclosed here can be used to control the speed of automotive accessories driven by a pulley attached to the crankshaft of an automotive engine. Usually, accessories must perform suitably both when the engine idles at low speed and when the engine runs at high speed. Often accessories operate optimally at one speed and suffer from reduced efficiency at other speeds. Additionally, the accessory design is compromised by the need to perform over a large speed range rather than an optimized narrow speed range. In many cases when the engine runs at a speed other than low speed, accessories consume excess power and, thereby, reduce vehicle fuel economy. The power drain caused by the accessories also reduces the engine's ability to power the vehicle, necessitating a larger engine in some cases.


In other situations, inventive embodiments of the torque/speed regulating devices disclosed here can be used to decrease or increase speed and/or torque delivered to the accessories for achieving optimal system performance. In certain situations, embodiments of the torque/speed regulating devices disclosed here can be used to increase speed to the accessories when the prime mover runs at low speed and to decrease speed to the accessories when the prime mover runs at high speed. Thus, the design and operation of accessories can be optimized by allowing the accessories to operate at one, substantially favorable speed, and the accessories need not be made larger than necessary to provide sufficient performance at low speeds. For example, the embodiments of the torque/speed regulating devices disclosed here can enable more power to be extracted from an accessory such as an alternator when the prime mover or engine is running at low idle speed. The accessories can also be made smaller because the torque/speed regulating devices can reduce speed to the accessories when the prime mover runs at high speed, reducing the stress load the accessories must withstand at high rpm. Because the accessories are not subjected to high speeds, their expected service life can increase substantially. In some cases, smoother vehicle operation results because the accessories do not have to run at low or high speed. Further, a vehicle can operate more quietly at high speed because the accessories run at a lower speed.


Embodiments of a continuously variable transmission (CVT), and components and subassemblies thereof, will be described now with reference to FIGS. 1-8. FIG. 1 shows a CVT 10 that can be used in many applications including, but not limited to, continuously variable accessory drives, human powered vehicles (for example, bicycles), light electrical vehicles, hybrid human-, electric-, or internal combustion powered vehicles, industrial equipment, wind turbines, etc. Any technical application that requires modulation of mechanical power transfer between a power input and a power sink (for example, a load) can implement embodiments of the CVT 10 in its power train.


Referring now to FIGS. 1-3, in one embodiment the CVT 10 is provided with a number of traction planet assemblies 12 arranged radially about a longitudinal axis 14. Each traction planet assembly 12 includes a spherical traction planet 16 configured to rotate about a planet axle 18. The planet axle 18 can tilt with respect to the longitudinal axis 14. Ends of the planet axle 18 can be coupled to first and second carriers 20, 21. In one embodiment, the first and second carriers 20, 21 are adapted to rotate with respect to each other. The CVT 10 can be provided with a first traction ring assembly 22 in contact with each of the traction planets 16. In one embodiment, the first traction ring assembly 22 is adapted to receive a power input from a drive pulley 23. The CVT 10 can be provided with a second traction ring assembly 24 in contact with each of the traction planets 16. In one embodiment, the first and second traction ring assemblies 22, 24 are each provided with a traction ring 26 and an axial force generator assembly 28. In some embodiments, the axial force generator assembly 28 can include a tone wheel configured to cooperate with, for example, a speed sensor (not shown). The CVT 10 is provided with a shaft 30 arranged along the longitudinal axis 14. The shaft 30 can be configured to transfer power to an accessory (not shown), such as an alternator. The shaft 30 is configured to drive, among other things, a pump 32. In one embodiment, the pump 32 is a gerotor type pump having an inner driven gear 31 coupled to an outer gear 33. The inner driven gear 31 is coupled to the shaft 30. The pump 32 is in fluid communication with a lubricant manifold 34. The lubricant manifold 34 is attached to a pump cavity 35. The pump cavity 35 and the lubricant manifold 34 substantially enclose the pump 32. The pump cavity 35 is coupled to a housing 36. The housing 36 substantially encloses and supports components of the CVT 10. The lubricant manifold 34, the pump cavity 35, and the shaft 30 are provided with a number of passages that are appropriately arranged to introduce a lubricant from a reservoir (not shown) into the pump 32 and deliver the lubricant to internal components of the CVT 10. In one embodiment, the reservoir is integral with the housing 36. In some embodiments, the reservoir can be remotely located.


In one embodiment, the CVT 10 is provided with an idler assembly 40 arranged radially inward of, and in contact with, each of the traction planets 16. The idler assembly 40 couples to a sleeve 42. The sleeve 42 is coaxial with, and surrounds, the shaft 30. In some embodiments, the sleeve 42 can be integral to the shaft 30. The sleeve 42 can be made of a different material than the shaft 30. For example, the sleeve 42 can be made of a material that has properties appropriate for a bearing race or a journal. In one embodiment, the idler assembly 40 includes a first rolling element 44 operably coupled to a second rolling element 46. The first rolling element 44 is radially supported on the sleeve 42 by a bearing 48. The bearing 48 can be a needle roller bearing, for example. The second rolling element 46 is radially supported by a bearing 50. The bearing 50 can be a needle roller bearing, for example. The second rolling element 46 is supported in the axial direction by a bearing 52. The bearing 52 can be a ball bearing, for example. The bearing 52 is coupled to a race 53. The race 53 is attached to the first rolling element 44 with, for example, a clip 54. The bearing 52 is positioned in a manner to balance the axial force applied to the first rolling element 44 with the axial force applied to the second rolling element 46.


During operation of the CVT 10, the first and second rolling elements 44, 46 rotate about the longitudinal axis 14. The first and second rolling elements 44, 46 each rotate at a speed corresponding to the tilt angle of the planet axle 18 with respect to the longitudinal axle 14. Under some operating conditions, for example when the planet axle 18 is substantially parallel to the longitudinal axis 14, the speed of the first rolling element 44 is substantially equal to the speed of the second rolling element 46. Under other operating conditions, the speed of the first rolling element 44 can be higher than the speed of the second rolling element 46. Under yet other operating conditions, the speed of the first rolling element 44 can be lower than the speed of the second rolling element 46. During operation of the CVT 10, the difference in speed between the first and second rolling elements 44, 46 is transmitted to the bearing 52. This is advantageous since the speed difference between the first and second rolling elements 44, 46 is typically small. It is well known that parasitic losses from bearings are related to the speed and load at which a bearing operates. Since the bearing 52 typically operates under relatively high axial loads, reducing the speed at which the bearing 52 operates serves to reduce the parasitic loss of the bearing 52.


Referring now specifically to FIG. 3, in one embodiment the first rolling element 44 is a generally cylindrical body having a ring 56 formed on one end. The first rolling element 44 is provided with a shoulder 58 extending from the ring 56. The shoulder 58 has a number of holes 60 arranged radially about the circumference of the cylindrical body. The holes 60 can facilitate the flow of lubricant to, for example, the bearing 50. In some embodiments, the holes 60 facilitate the flow of lubricant to the contacting surfaces between the traction planets 16 and the first and second rolling elements 44, 46. The shoulder 58 is provided with a groove 62 formed on the outer periphery of the cylindrical body. The groove 62 is adapted to receive the clip 54. The first rolling element 44 is provided with grooves 64 on the inner circumference of the cylindrical body. The grooves 64 are adapted to receive, for example, clips 66 (FIG. 2). The clips 66 facilitate the retention of the bearing 48 (FIG. 2) with respect to the first rolling element 44.


Turning now to FIG. 4, in one embodiment the first carrier 20 is a substantially bowl-shaped body having a central bore 72. The bowl-shaped body can be provided with a number of guide slots 74 arranged angularly about the central bore 72. The guide slots 74 are aligned with a radial construction line 76 when viewed in the plane of the page of FIG. 4. The guide slots 74 are adapted to receive one end of the planet axle 18. The bowl-shaped body is provided with a flange 77 formed about the outer periphery. The flange 77 can be adapted to attach to the housing 36.


Referring now to FIG. 5, in one embodiment the second carrier 21 is a substantially bowl-shaped body having a central bore 82. The bowl-shaped body can be provided with a number of guide slots 84 arranged angularly about the central bore 82. Each guide slot 84 is sized to accommodate the coupling of the second carrier 21 to the planet axle 18. The guide slots 84 are angularly offset from the radial construction line 76 when viewed in the plane of the page of FIG. 5. The angular offset can be approximated by an angle 88. The angle 88 is formed between the radial construction line 76 and a construction line 90. The construction line 90 substantially bisects the guide slot 84 when viewed in the plane of the page of FIG. 5. In some embodiments, the angle 88 is between 3 degrees and 45 degrees. A low angle 88 would provide faster shift rates in a given application but rotation of the carrier 21 must be controlled over a very small range. A high angle 88 would provide slower shift rates in a given application but rotation of carrier 21 would be controlled over a larger range. In effect, a low angle 88 produces a highly responsive transmission ratio change but potentially more difficult to control or stabilize, while a high angle can be less responsive in transmission ratio change but easy to control by comparison. In some embodiments, where it is desirable to have high speed, fast shift rates, the angle 88 can be, for example, 10 degrees. In other embodiments, where it is desirable to have slower speed, precise control of transmission ratio, the angle 88 can be about 30 degrees. However, the said values of the angle 88 are provided as an illustrative example, and the angle 88 can be varied in any manner a designer desires. In some embodiments, the angle 88 can be any angle in the range of 10 to 25 degrees including any angle in between or fractions thereof. For example, the angle can be 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, or any portion thereof. In other embodiments, the angle 88 can be 20 degrees. In one embodiment, the guide slots 84 can be arranged so that the construction line 90 is radially offset from a construction line 91 by a distance 92. The construction line 91 is parallel to the construction line 90 and intersects the center of the bowl-shaped body.


In one embodiment, the second carrier 21 is coupled to a clevis 94. The clevis 94 can be accessed through an opening (not shown) in the housing 36 to facilitate the coupling of the clevis 94 to an actuator (not shown). During operation of the CVT 10, a change in transmission ratio can be accomplished by rotating the second carrier 21 with respect to the first carrier 20. A rotation of the second carrier 21 can be accomplished by moving the clevis 94 with the actuator.


Referring now to FIG. 6, in one embodiment an idler assembly 100 includes a spherical traction planet 101. The spherical traction planet 101 can be provided with a tiltable axis of rotation (not shown). The idler assembly 100 includes first and second rolling elements 102, 103, respectively. In some embodiments, the first rolling element 102 can be coupled to at least one bearing 104 at a radially inward location. In other embodiments, the bearing 104 is not used. The second rolling element 103 can be coupled to at least one bearing 105 at a radially inward location. The bearing 105 is supported by the first rolling element 102. The second rolling element 103 can be axially coupled to the first rolling element 102 with a bearing 106. In some embodiments, the bearing 106 can be an angular contact bearing, in such cases the bearing 105 can be removed. The bearing 106 is coupled to a shoulder 107 attached to the first rolling element 102. In one embodiment, the shoulder 107 is integral to the first rolling element 102. In other embodiments, the shoulder 107 is a separate component that is fixedly attached to the first rolling element 102. Each of the first and second rolling elements 102, 103 are provided with contact surfaces 109, 110, respectively. The contact surfaces 109, 110 are in contact with the traction planet 101. The contact surfaces 109, 110 are angled with respect to a longitudinal axis 111 at an angle 112 when viewed in the plane of the page of FIG. 6. In some embodiments, the angle 112 can be any angle in the range of 0 to 45 degrees including any angle in between or fractions thereof. For example, the angle can be 0, 1, 2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14, 15, 16, 17, 18, 19, 20, 21, 22, 23, 24, 25, 26, 27, 28, 29, 30, 31, 32, 33, 34, 35, 36, 37, 38, 39, 40, 41, 42, 43, 44, 45 or any portion thereof. In other embodiments, the angle 112 can be 10 degrees. In some embodiments, the first rolling element 102 is configured to receive an input power.


Passing now to FIG. 7, in one embodiment an idler assembly 120 can include first and second rolling elements 121, 122, respectively. The first and second rolling elements 121, 122 are each coupled to a bearing 123. The bearings 123 can be attached to a sleeve 124 with, for example, clips 125. The first and second rolling elements 121, 122 are each provided with a contact surface 126. The contact surfaces 126 are in contact with the traction planet 101. The contact surfaces 126 are formed at the angle 112 relative to the longitudinal axis 111 when viewed in the plane of the page of FIG. 7.


Referring now to FIG. 8, in one embodiment an idler assembly 130 can include first and second rolling elements 132, 133, respectively. The first and second rolling elements 132, 133 are each coupling to a bearing 136. The bearing 136 can be provided with a cage 137. The first rolling element 132 has an extension 134. The extension 134 coupled to the bearing 136. In one embodiment, the bearing 136 is an angular contact bearing. The first rolling element 132 is provided with a contact surface 139. The contact surface 139 is in contact with the traction planet 101. The second rolling element 133 is provided with a contact surface 140. The contact surfaces 139, 140 are formed at the angle 112 relative to the longitudinal axis 111 when viewed in the plane of the page of FIG. 8.


It should be noted that the description above has provided dimensions for certain components or subassemblies. The mentioned dimensions, or ranges of dimensions, are provided in order to comply as best as possible with certain legal requirements, such as best mode. However, the scope of the embodiments described herein are to be determined solely by the language of the claims, and consequently, none of the mentioned dimensions is to be considered limiting on the embodiments, except in so far as any one claim makes a specified dimension, or range of thereof, a feature of the claim.


The foregoing description details certain embodiments of the disclosure. It will be appreciated, however, that no matter how detailed the foregoing appears in text, the disclosure can be practiced in many ways. As is also stated above, it should be noted that the use of particular terminology when describing certain features or aspects of the disclosure should not be taken to imply that the terminology is being re-defined herein to be restricted to including any specific characteristics of the features or aspects of the disclosure with which that terminology is associated.

Claims
  • 1. A continuously variable accessory drive (CVAD) for coupling to a power source, the CVAD comprising: a variator disposed within a housing, the variator comprising a plurality of tiltable traction planet assemblies arranged about a longitudinal axis, each tiltable traction planet assembly rotatable around an axle,a pair of carriers, each carrier having a plurality of guide slots, wherein each axle of the plurality of tiltable traction planet assemblies is coupled to the pair of carriers, wherein rotation of at least one of the pair of carriers causes angular displacement in a first plane to achieve an angular displacement in a second plane for each of the plurality of tiltable traction planet assemblies,a first traction ring coaxial about the longitudinal axis;a second traction ring coaxial about the longitudinal axis, the first traction ring and the second traction ring being in contact with the plurality of traction planets, andan idler assembly located radially inward of the plurality of traction planets, wherein the idler assembly comprises: a first rolling element rotatable about an axis at a first speed corresponding to a tilt angle of a planet axle relative to the longitudinal axis,a second rolling element rotatable about the axis at a second speed corresponding to the tilt angle of a planet axle relative to the longitudinal axis, each of the first rolling element and the second rolling element comprising first and second surfaces angled for contact with the plurality of traction planet assemblies, the first surface angled at a first angle and the second surface angled less than the first angle, anda first bearing interposed between the first rolling element and the second rolling element, the first bearing positioned radially inward of the second rolling element.
  • 2. The continuously variable accessory drive (CVAD) of claim 1, wherein the first angle is in the range between 0 and 45 degrees.
  • 3. The continuously variable accessory drive (CVAD) of claim 2, wherein the first angle is in the range between 0 and 10 degrees.
  • 4. The continuously variable accessory drive (CVAD) of claim 1, further comprising a second bearing, the second bearing positioned axially between at least a portion of the first rolling element and at least a portion of the second rolling element.
  • 5. The continuously variable accessory drive (CVAD) of claim 1, wherein the power source is an internal combustion engine capable of idling at a low speed and running at a high speed, wherein as the speed of the power source changes, the CVAD changes the speed of power delivered to an accessory for achieving optimal system performance.
  • 6. The continuously variable accessory drive (CVAD) of claim 5, wherein the optimal system performance comprises operating the accessory within a narrow speed range.
  • 7. The continuously variable accessory drive (CVAD) of claim 5, wherein the optimal system performance comprises operating the accessory at a constant speed.
  • 8. The continuously variable accessory drive (CVAD) of claim 5, wherein the accessory comprises one of a compressor, a turbocharger, and a supercharger.
  • 9. The continuously variable accessory drive (CVAD) of claim 5, wherein the accessory comprises one of an alternator and a generator.
  • 10. The continuously variable accessory drive (CVAD) of claim 5, wherein achieving optimal system performance comprises reducing a stress load on the accessory.
  • 11. The continuously variable accessory drive (CVAD) of claim 5, further comprising: a pump coupled to a shaft arranged along the longitudinal axis;a lubricant manifold; anda lubricant reservoir.
  • 12. The continuously variable accessory drive (CVAD) of claim 11, wherein the lubricant reservoir is remotely located from the housing.
  • 13. The continuously variable accessory drive (CVAD) of claim 1, wherein the first traction ring is coupled to an accessory via a pulley.
  • 14. The continuously variable accessory drive (CVAD) of claim 1, wherein the CVAD is coupled to an accessory via a shaft.
RELATED APPLICATIONS

This application is a continuation of U.S. patent application Ser. No. 14/541,875, filed Nov. 14, 2014 and scheduled to issue on Mar. 22, 2016 as U.S. Pat. No. 9,291,251, which is a continuation of U.S. patent application Ser. No. 13/288,711, filed Nov. 3, 2011 and issued as U.S. Pat. No. 8,888,643 on Nov. 18, 2014, which claims the benefit of U.S. Provisional Application No. 61/412,290, filed on Nov. 10, 2010. The disclosures of all of the above-referenced prior applications, publications, and patents are considered part of the disclosure of this application, and are incorporated by reference herein in their entirety.

US Referenced Citations (657)
Number Name Date Kind
719595 Huss Feb 1903 A
1121210 Techel Dec 1914 A
1175677 Barnes Mar 1916 A
1207985 Null et al. Dec 1916 A
1380006 Nielsen May 1921 A
1390971 Samain Sep 1921 A
1558222 Beetow Oct 1925 A
1629092 Arter et al. May 1927 A
1629902 Arter et al. May 1927 A
1686446 Gilman Oct 1928 A
1774254 Daukus Aug 1930 A
1793571 Vaughn Feb 1931 A
1847027 Thomsen et al. Feb 1932 A
1850189 Weiss Mar 1932 A
1858696 Weiss May 1932 A
1865102 Hayes Jun 1932 A
1903228 Thomson Mar 1933 A
1978439 Sharpe Oct 1934 A
2030203 Gove et al. Feb 1936 A
2060884 Madle Nov 1936 A
2086491 Dodge Jul 1937 A
2100629 Chilton Nov 1937 A
2109845 Madle Mar 1938 A
2112763 Cloudsley Mar 1938 A
2131158 Almen et al. Sep 1938 A
2134225 Christiansen Oct 1938 A
2152796 Erban Apr 1939 A
2196064 Erban Apr 1940 A
2209254 Ahnger Jul 1940 A
2259933 Holloway Oct 1941 A
2269434 Brooks Jan 1942 A
2325502 Auguste Jul 1943 A
RE22761 Wemp May 1946 E
2461258 Brooks Feb 1949 A
2469653 Kopp May 1949 A
2480968 Ronai Sep 1949 A
2553465 Monge May 1951 A
2586725 Henry Feb 1952 A
2595367 Picanol May 1952 A
2596538 Dicke May 1952 A
2597849 Alfredeen May 1952 A
2675713 Acker Apr 1954 A
2696888 Chillson et al. Dec 1954 A
2868038 Billeter May 1955 A
2716357 Rennerfelt Aug 1955 A
2730904 Rennerfelt Jan 1956 A
2748614 Weisel Jun 1956 A
2959070 Flinn Jan 1959 A
2873911 Perrine Feb 1959 A
2874592 Oehrli Feb 1959 A
2883883 Chillson Apr 1959 A
2891213 Kern Jun 1959 A
2901924 Banker Sep 1959 A
2913932 Oehrli Nov 1959 A
2931234 Hayward Apr 1960 A
2931235 Hayward Apr 1960 A
2949800 Neuschotz Aug 1960 A
2959063 Perry Nov 1960 A
2959972 Madson Nov 1960 A
2964959 Beck Dec 1960 A
3008061 Mims et al. Nov 1961 A
3035460 Guichard May 1962 A
3048056 Wolfram Aug 1962 A
3051020 Hartupee Aug 1962 A
3086704 Hurtt Apr 1963 A
3087348 Kraus Apr 1963 A
3154957 Kashihara Nov 1964 A
3163050 Kraus Dec 1964 A
3176542 Monch Apr 1965 A
3184983 Kraus May 1965 A
3204476 Rouverol Sep 1965 A
3209606 Yamamoto Oct 1965 A
3211364 Wentling et al. Oct 1965 A
3216283 General Nov 1965 A
3229538 Schlottler Jan 1966 A
3237468 Schlottler Mar 1966 A
3246531 Kashihara Apr 1966 A
3248960 Schottler May 1966 A
3273468 Allen Sep 1966 A
3280646 Lemieux Oct 1966 A
3283614 Hewko Nov 1966 A
3292443 Felix Dec 1966 A
3340895 Osgood, Jr. et al. Sep 1967 A
3407687 Hayashi Oct 1968 A
3430504 Dickenbrock Mar 1969 A
3439563 Petty Apr 1969 A
3440895 Fellows Apr 1969 A
3464281 Hiroshi et al. Sep 1969 A
3477315 Macks Nov 1969 A
3487726 Burnett Jan 1970 A
3487727 Gustafsson Jan 1970 A
3574289 Scheiter et al. Apr 1971 A
3581587 Dickenbrock Jun 1971 A
3661404 Bossaer May 1972 A
3695120 Titt Oct 1972 A
3707888 Schottler Jan 1973 A
3727473 Bayer Apr 1973 A
3727474 Fullerton Apr 1973 A
3736803 Horowitz et al. Jun 1973 A
3768715 Tout Oct 1973 A
3800607 Zurcher Apr 1974 A
3802284 Sharpe et al. Apr 1974 A
3810398 Kraus May 1974 A
3820416 Kraus Jun 1974 A
3866985 Whitehurst Feb 1975 A
3891235 Shelly Jun 1975 A
3934493 Hillyer Jan 1976 A
3954282 Hege May 1976 A
3987681 Keithley et al. Oct 1976 A
3996807 Adams Dec 1976 A
4023442 Woods et al. May 1977 A
4098146 McLarty Jul 1978 A
4103514 Grosse-Entrup Aug 1978 A
4159653 Koivunen Jul 1979 A
4169609 Zampedro Oct 1979 A
4177683 Moses Dec 1979 A
4227712 Dick Oct 1980 A
4314485 Adams Feb 1982 A
4345486 Olesen Aug 1982 A
4369667 Kemper Jan 1983 A
4382186 Cronin May 1983 A
4391156 Tibbals Jul 1983 A
4459873 Black Jul 1984 A
4464952 Stubbs Aug 1984 A
4468984 Castelli et al. Sep 1984 A
4494524 Wagner Jan 1985 A
4496051 Ortner Jan 1985 A
4501172 Kraus Feb 1985 A
4515040 Takeuchi et al. May 1985 A
4526255 Hennessey et al. Jul 1985 A
4546673 Shigematsu et al. Oct 1985 A
4560369 Hattori Dec 1985 A
4567781 Russ Feb 1986 A
4569670 McIntosh Feb 1986 A
4574649 Seol Mar 1986 A
4585429 Marier Apr 1986 A
4617838 Anderson Oct 1986 A
4630839 Seol Dec 1986 A
4631469 Tsuboi et al. Dec 1986 A
4651082 Kaneyuki Mar 1987 A
4663990 Itoh et al. May 1987 A
4700581 Tibbals, Jr. Oct 1987 A
4713976 Wilkes Dec 1987 A
4717368 Yamaguchi et al. Jan 1988 A
4735430 Tomkinson Apr 1988 A
4738164 Kaneyuki Apr 1988 A
4744261 Jacobson May 1988 A
4756211 Fellows Jul 1988 A
4781663 Reswick Nov 1988 A
4838122 Takamiya et al. Jun 1989 A
4856374 Kreuzer Aug 1989 A
4869130 Wiecko Sep 1989 A
4881925 Hattori Nov 1989 A
4900046 Aranceta-Angoitia Feb 1990 A
4909101 Terry Mar 1990 A
4918344 Chikamori et al. Apr 1990 A
4964312 Kraus Oct 1990 A
5006093 Itoh et al. Apr 1991 A
5020384 Kraus Jun 1991 A
5025685 Kobayashi et al. Jun 1991 A
5033322 Nakano Jul 1991 A
5033571 Morimoto Jul 1991 A
5037361 Takahashi Aug 1991 A
5044214 Barber Sep 1991 A
5059158 Bellio et al. Oct 1991 A
5069655 Schivelbusch Dec 1991 A
5083982 Sato Jan 1992 A
5099710 Nakano Mar 1992 A
5121654 Fasce Jun 1992 A
5125677 Ogilvie et al. Jun 1992 A
5138894 Kraus Aug 1992 A
5156412 Meguerditchian Oct 1992 A
5230258 Nakano Jul 1993 A
5236211 Meguerditchian Aug 1993 A
5236403 Schievelbusch Aug 1993 A
5267920 Hibi Dec 1993 A
5273501 Schievelbusch Dec 1993 A
5318486 Lutz Jun 1994 A
5319486 Vogel et al. Jun 1994 A
5330396 Lohr et al. Jul 1994 A
5355749 Obara et al. Oct 1994 A
5375865 Terry, Sr. Dec 1994 A
5379661 Nakano Jan 1995 A
5383677 Thomas Jan 1995 A
5387000 Sato Feb 1995 A
5401221 Fellows et al. Mar 1995 A
5451070 Lindsay et al. Sep 1995 A
5489003 Ohyama et al. Feb 1996 A
5508574 Vlock Apr 1996 A
5562564 Folino Oct 1996 A
5564998 Fellows Oct 1996 A
5601301 Liu Feb 1997 A
5607373 Ochiai et al. Mar 1997 A
5645507 Hathaway Jul 1997 A
5651750 Imanishi et al. Jul 1997 A
5664636 Ikuma et al. Sep 1997 A
5669845 Muramoto et al. Sep 1997 A
5690346 Keskitalo Nov 1997 A
5722502 Kubo Mar 1998 A
5746676 Kawase et al. May 1998 A
5755303 Yamamoto et al. May 1998 A
5799541 Arbeiter Sep 1998 A
5823052 Nobumoto Oct 1998 A
5846155 Taniguchi et al. Dec 1998 A
5888160 Miyata et al. Mar 1999 A
5895337 Fellows et al. Apr 1999 A
5899827 Nakano et al. May 1999 A
5902207 Sugihara May 1999 A
5967933 Valdenaire Oct 1999 A
5976054 Yasuoka Nov 1999 A
5984826 Nakano Nov 1999 A
5995895 Watt et al. Nov 1999 A
6000707 Miller Dec 1999 A
6003649 Fischer Dec 1999 A
6004239 Makino Dec 1999 A
6006151 Graf Dec 1999 A
6012538 Sonobe et al. Jan 2000 A
6015359 Kunii Jan 2000 A
6019701 Mori et al. Feb 2000 A
6029990 Busby Feb 2000 A
6042132 Suenaga et al. Mar 2000 A
6045477 Schmidt Apr 2000 A
6045481 Kumagai Apr 2000 A
6053833 Masaki Apr 2000 A
6053841 Kolde et al. Apr 2000 A
6054844 Frank Apr 2000 A
6066067 Greenwood May 2000 A
6071210 Kato Jun 2000 A
6074320 Miyata et al. Jun 2000 A
6076846 Clardy Jun 2000 A
6079726 Busby Jun 2000 A
6083139 Deguchi Jul 2000 A
6086506 Petersmann et al. Jul 2000 A
6095940 Ai et al. Aug 2000 A
6099431 Hoge et al. Aug 2000 A
6101895 Yamane Aug 2000 A
6113513 Itoh et al. Sep 2000 A
6119539 Papanicolaou Sep 2000 A
6119800 McComber Sep 2000 A
6159126 Oshidari Dec 2000 A
6171210 Miyata et al. Jan 2001 B1
6174260 Tsukada et al. Jan 2001 B1
6186922 Bursal et al. Feb 2001 B1
6210297 Knight Apr 2001 B1
6217473 Ueda et al. Apr 2001 B1
6217478 Vohmann et al. Apr 2001 B1
6241636 Miller Jun 2001 B1
6243638 Abo et al. Jun 2001 B1
6251038 Ishikawa et al. Jun 2001 B1
6258003 Hirano et al. Jul 2001 B1
6261200 Miyata et al. Jul 2001 B1
6296593 Gotou Oct 2001 B1
6311113 Danz et al. Oct 2001 B1
6312358 Goi et al. Nov 2001 B1
6322475 Miller Nov 2001 B2
6325386 Shoge Dec 2001 B1
6358174 Folsom et al. Mar 2002 B1
6358178 Wittkopp Mar 2002 B1
6367833 Horiuchi Apr 2002 B1
6371878 Bowen Apr 2002 B1
6375412 Dial Apr 2002 B1
6390945 Young May 2002 B1
6390946 Hibi et al. May 2002 B1
6406399 Ai Jun 2002 B1
6414401 Kuroda et al. Jul 2002 B1
6419608 Miller Jul 2002 B1
6425838 Matsubara et al. Jul 2002 B1
6434960 Rousseau Aug 2002 B1
6440037 Takagi et al. Aug 2002 B2
6459978 Tamiguchi et al. Oct 2002 B2
6461268 Milner Oct 2002 B1
6482094 Kefes Nov 2002 B2
6492785 Kasten et al. Dec 2002 B1
6494805 Ooyama et al. Dec 2002 B2
6499373 Van Cor Dec 2002 B2
6514175 Taniguchi et al. Feb 2003 B2
6532890 Chen Mar 2003 B2
6551210 Miller Apr 2003 B2
6558285 Sieber May 2003 B1
6575047 Reik et al. Jun 2003 B2
6659901 Sakai et al. Dec 2003 B2
6672418 Makino Jan 2004 B1
6676559 Miller Jan 2004 B2
6679109 Gierling et al. Jan 2004 B2
6682432 Shinozuka Jan 2004 B1
6689012 Miller Feb 2004 B2
6721637 Abe et al. Apr 2004 B2
6723014 Shinso et al. Apr 2004 B2
6723016 Sumi Apr 2004 B2
6805654 Nishii Oct 2004 B2
6808053 Kirkwood et al. Oct 2004 B2
6839617 Mensler et al. Jan 2005 B2
6849020 Sumi Feb 2005 B2
6859709 Joe et al. Feb 2005 B2
6868949 Braford Mar 2005 B2
6931316 Joe et al. Aug 2005 B2
6932739 Miyata et al. Aug 2005 B2
6942593 Nishii et al. Sep 2005 B2
6945903 Miller Sep 2005 B2
6949049 Miller Sep 2005 B2
6958029 Inoue Oct 2005 B2
6991575 Inoue Jan 2006 B2
6991579 Kobayashi et al. Jan 2006 B2
7011600 Miller et al. Mar 2006 B2
7011601 Miller Mar 2006 B2
7014591 Miller Mar 2006 B2
7029418 Taketsuna et al. Apr 2006 B2
7032914 Miller Apr 2006 B2
7036620 Miller et al. May 2006 B2
7044884 Miller May 2006 B2
7063195 Berhan Jun 2006 B2
7063640 Miller Jun 2006 B2
7074007 Miller Jul 2006 B2
7074154 Miller Jul 2006 B2
7074155 Miller Jul 2006 B2
7077777 Miyata et al. Jul 2006 B2
7086979 Frenken Aug 2006 B2
7086981 Ali et al. Aug 2006 B2
7094171 Inoue Aug 2006 B2
7111860 Grimaldos Sep 2006 B1
7112158 Miller Sep 2006 B2
7112159 Miller et al. Sep 2006 B2
7125297 Miller et al. Oct 2006 B2
7131930 Miller et al. Nov 2006 B2
7140999 Miller Nov 2006 B2
7147586 Miller et al. Dec 2006 B2
7153233 Miller et al. Dec 2006 B2
7156770 Miller Jan 2007 B2
7160220 Shinojima et al. Jan 2007 B2
7160222 Miller Jan 2007 B2
7163485 Miller Jan 2007 B2
7163486 Miller et al. Jan 2007 B2
7166052 Miller et al. Jan 2007 B2
7166056 Miller et al. Jan 2007 B2
7166057 Miller et al. Jan 2007 B2
7166058 Miller et al. Jan 2007 B2
7169076 Miller et al. Jan 2007 B2
7172529 Miller et al. Feb 2007 B2
7175564 Miller Feb 2007 B2
7175565 Miller et al. Feb 2007 B2
7175566 Miller et al. Feb 2007 B2
7192381 Miller et al. Mar 2007 B2
7197915 Luh et al. Apr 2007 B2
7198582 Miller et al. Apr 2007 B2
7198583 Miller et al. Apr 2007 B2
7198584 Miller et al. Apr 2007 B2
7198585 Miller et al. Apr 2007 B2
7201693 Miller et al. Apr 2007 B2
7201694 Miller et al. Apr 2007 B2
7201695 Miller et al. Apr 2007 B2
7204777 Miller et al. Apr 2007 B2
7214159 Miller et al. May 2007 B2
7217215 Miller et al. May 2007 B2
7217216 Inoue May 2007 B2
7217219 Miller May 2007 B2
7217220 Careau et al. May 2007 B2
7226379 Ibamoto et al. Jun 2007 B2
7232395 Miller et al. Jun 2007 B2
7234873 Kato et al. Jun 2007 B2
7235031 Miller et al. Jun 2007 B2
7238136 Miller et al. Jul 2007 B2
7238137 Miller et al. Jul 2007 B2
7238138 Miller et al. Jul 2007 B2
7238139 Roethler et al. Jul 2007 B2
7246672 Shirai et al. Jul 2007 B2
7250018 Miller et al. Jul 2007 B2
7261663 Miller et al. Aug 2007 B2
7275610 Kuang et al. Oct 2007 B2
7285068 Hosoi Oct 2007 B2
7288042 Miller et al. Oct 2007 B2
7288043 Shioiri et al. Oct 2007 B2
7320660 Miller Jan 2008 B2
7322901 Miller et al. Jan 2008 B2
7343236 Wilson Mar 2008 B2
7347801 Guenter et al. Mar 2008 B2
7383748 Rankin Jun 2008 B2
7383749 Rankin Jun 2008 B2
7384370 Miller Jun 2008 B2
7393300 Miller et al. Jul 2008 B2
7393302 Miller Jul 2008 B2
7393303 Miller Jul 2008 B2
7395731 Miller et al. Jul 2008 B2
7396209 Miller et al. Jul 2008 B2
7402122 Miller Jul 2008 B2
7410443 Miller Aug 2008 B2
7419451 Miller Sep 2008 B2
7422541 Miller Sep 2008 B2
7422546 Miller et al. Sep 2008 B2
7427253 Miller Sep 2008 B2
7431677 Miller et al. Oct 2008 B2
7452297 Miller et al. Nov 2008 B2
7455611 Miller et al. Nov 2008 B2
7455617 Miller et al. Nov 2008 B2
7462123 Miller et al. Dec 2008 B2
7462127 Miller et al. Dec 2008 B2
7470210 Miller et al. Dec 2008 B2
7478885 Urabe Jan 2009 B2
7481736 Miller et al. Jan 2009 B2
7510499 Miller et al. Mar 2009 B2
7540818 Miller et al. Jun 2009 B2
7547264 Usoro Jun 2009 B2
7574935 Rohs et al. Aug 2009 B2
7591755 Petrzik et al. Sep 2009 B2
7632203 Miller Dec 2009 B2
7651437 Miller et al. Jan 2010 B2
7654928 Miller et al. Feb 2010 B2
7670243 Miller Mar 2010 B2
7686729 Miller et al. Mar 2010 B2
7727101 Miller Jun 2010 B2
7727106 Maheu et al. Jun 2010 B2
7727107 Miller Jun 2010 B2
7727108 Miller et al. Jun 2010 B2
7727110 Miller et al. Jun 2010 B2
7727115 Serkh Jun 2010 B2
7731615 Miller et al. Jun 2010 B2
7762919 Smithson et al. Jul 2010 B2
7762920 Smithson et al. Jul 2010 B2
7770674 Miles et al. Aug 2010 B2
7785228 Smithson et al. Aug 2010 B2
7828685 Miller Nov 2010 B2
7837592 Miller Nov 2010 B2
7871353 Nichols et al. Jan 2011 B2
7882762 Armstrong et al. Feb 2011 B2
7883442 Miller et al. Feb 2011 B2
7885747 Miller et al. Feb 2011 B2
7887032 Malone Feb 2011 B2
7909723 Triller et al. Mar 2011 B2
7909727 Smithson et al. Mar 2011 B2
7914029 Miller et al. Mar 2011 B2
7959533 Nichols et al. Jun 2011 B2
7963880 Smithson et al. Jun 2011 B2
7967719 Smithson et al. Jun 2011 B2
7976426 Smithson et al. Jul 2011 B2
8066613 Smithson et al. Nov 2011 B2
8066614 Miller et al. Nov 2011 B2
8070635 Miller Dec 2011 B2
8087482 Miles et al. Jan 2012 B2
8123653 Smithson et al. Feb 2012 B2
8133149 Smithson et al. Mar 2012 B2
8142323 Tsuchiya et al. Mar 2012 B2
8167759 Pohl et al. May 2012 B2
8171636 Smithson et al. May 2012 B2
8230961 Schneidewind Jul 2012 B2
8262536 Nichols et al. Sep 2012 B2
8267829 Miller et al. Sep 2012 B2
8313404 Carter et al. Nov 2012 B2
8313405 Bazyn et al. Nov 2012 B2
8317650 Nichols et al. Nov 2012 B2
8317651 Lohr Nov 2012 B2
8321097 Vasiliotis et al. Nov 2012 B2
8342999 Miller Jan 2013 B2
8360917 Nichols et al. Jan 2013 B2
8376889 Hoffman et al. Feb 2013 B2
8376903 Pohl et al. Feb 2013 B2
8382631 Hoffman et al. Feb 2013 B2
8382637 Tange Feb 2013 B2
8393989 Pohl Mar 2013 B2
8398518 Nichols et al. Mar 2013 B2
8469853 Miller et al. Jun 2013 B2
8469856 Thomassy Jun 2013 B2
8480529 Pohl et al. Jul 2013 B2
8496554 Pohl et al. Jul 2013 B2
8506452 Pohl et al. Aug 2013 B2
8512195 Lohr et al. Aug 2013 B2
8517888 Brookins Aug 2013 B1
8535199 Lohr et al. Sep 2013 B2
8550949 Miller Oct 2013 B2
8585528 Carter et al. Nov 2013 B2
8608609 Sherrill Dec 2013 B2
8622866 Bazyn et al. Jan 2014 B2
8626409 Vasiliotis et al. Jan 2014 B2
8628443 Miller et al. Jan 2014 B2
8641572 Nichols et al. Feb 2014 B2
8641577 Nichols et al. Feb 2014 B2
8663050 Nichols et al. Mar 2014 B2
8678974 Lohr Mar 2014 B2
8708360 Miller et al. Apr 2014 B2
8721485 Lohr et al. May 2014 B2
8738255 Carter et al. May 2014 B2
8776633 Armstrong et al. Jul 2014 B2
8784248 Murakami et al. Jul 2014 B2
8790214 Lohr et al. Jul 2014 B2
8818661 Keilers et al. Aug 2014 B2
8827856 Younggren et al. Sep 2014 B1
8827864 Durack Sep 2014 B2
8845485 Smithson et al. Sep 2014 B2
8852050 Thomassy Oct 2014 B2
8870711 Pohl et al. Oct 2014 B2
8888643 Lohr et al. Nov 2014 B2
8900085 Pohl et al. Dec 2014 B2
8920285 Smithson et al. Dec 2014 B2
8924111 Fuller Dec 2014 B2
8961363 Shiina et al. Feb 2015 B2
8992376 Ogawa et al. Mar 2015 B2
8996263 Quinn et al. Mar 2015 B2
9017207 Pohl et al. Apr 2015 B2
9022889 Miller May 2015 B2
9046158 Miller et al. Jun 2015 B2
9074674 Nichols et al. Jul 2015 B2
9086145 Pohl et al. Jul 2015 B2
9121464 Nichols et al. Sep 2015 B2
9182018 Bazyn et al. Nov 2015 B2
9239099 Carter et al. Jan 2016 B2
9249880 Vasiliotis et al. Feb 2016 B2
9273760 Pohl et al. Mar 2016 B2
9279482 Nichols et al. Mar 2016 B2
9291251 Lohr Mar 2016 B2
9528561 Nichols et al. Dec 2016 B2
9574643 Pohl Feb 2017 B2
9656672 Schieffelin May 2017 B2
20010008192 Morisawa Jul 2001 A1
20010023217 Miyagawa et al. Sep 2001 A1
20010041644 Yasuoka et al. Nov 2001 A1
20010044358 Taniguchi Nov 2001 A1
20010044361 Taniguchi et al. Nov 2001 A1
20020019285 Henzler Feb 2002 A1
20020028722 Sakai et al. Mar 2002 A1
20020037786 Hirano et al. Mar 2002 A1
20020045511 Geiberger et al. Apr 2002 A1
20020049113 Watanabe et al. Apr 2002 A1
20020117860 Man et al. Aug 2002 A1
20020128107 Wakayama Sep 2002 A1
20020161503 Joe et al. Oct 2002 A1
20020169051 Oshidari Nov 2002 A1
20020179348 Tamai et al. Dec 2002 A1
20030015358 Abe et al. Jan 2003 A1
20030015874 Abe et al. Jan 2003 A1
20030022753 Mizuno et al. Jan 2003 A1
20030036456 Skrabs Feb 2003 A1
20030132051 Nishii et al. Jul 2003 A1
20030135316 Kawamura et al. Jul 2003 A1
20030144105 O'Hora Jul 2003 A1
20030160420 Fukuda Aug 2003 A1
20030216216 Inoue et al. Nov 2003 A1
20030221892 Matsumoto et al. Dec 2003 A1
20040038772 McIndoe et al. Feb 2004 A1
20040058772 Inoue et al. Mar 2004 A1
20040067816 Taketsuna et al. Apr 2004 A1
20040082421 Wafzig Apr 2004 A1
20040092359 Imanishi et al. May 2004 A1
20040119345 Takano Jun 2004 A1
20040171457 Fuller Sep 2004 A1
20040204283 Inoue Oct 2004 A1
20040231331 Iwanami et al. Nov 2004 A1
20040254047 Frank et al. Dec 2004 A1
20050037876 Unno et al. Feb 2005 A1
20050064986 Ginglas Mar 2005 A1
20050085979 Carlson et al. Apr 2005 A1
20050181905 Ali et al. Aug 2005 A1
20050184580 Kuan et al. Aug 2005 A1
20050227809 Bitzer et al. Oct 2005 A1
20050229731 Parks et al. Oct 2005 A1
20050233846 Green et al. Oct 2005 A1
20060000684 Agner Jan 2006 A1
20060006008 Brunemann et al. Jan 2006 A1
20060052204 Eckert et al. Mar 2006 A1
20060054422 Dimsey et al. Mar 2006 A1
20060108956 Clark May 2006 A1
20060111212 Ai et al. May 2006 A9
20060154775 Ali et al. Jul 2006 A1
20060172829 Ishio Aug 2006 A1
20060180363 Uchisasai Aug 2006 A1
20060223667 Nakazeki Oct 2006 A1
20060234822 Morscheck et al. Oct 2006 A1
20060234826 Moehlmann et al. Oct 2006 A1
20060276299 Imanishi Dec 2006 A1
20070004552 Matsudaira et al. Jan 2007 A1
20070004556 Rohs et al. Jan 2007 A1
20070099753 Matsui et al. May 2007 A1
20070149342 Guenter et al. Jun 2007 A1
20070155552 De Cloe Jul 2007 A1
20070155567 Miller et al. Jul 2007 A1
20070193391 Armstrong et al. Aug 2007 A1
20070228687 Parker Oct 2007 A1
20080009389 Jacobs Jan 2008 A1
20080032852 Smithson et al. Feb 2008 A1
20080032854 Smithson et al. Feb 2008 A1
20080039269 Smithson et al. Feb 2008 A1
20080039273 Smithson et al. Feb 2008 A1
20080039276 Smithson et al. Feb 2008 A1
20080081728 Faulring et al. Apr 2008 A1
20080139363 Williams Jun 2008 A1
20080149407 Shibata et al. Jun 2008 A1
20080183358 Thomson et al. Jul 2008 A1
20080200300 Smithson et al. Aug 2008 A1
20080228362 Muller et al. Sep 2008 A1
20080284170 Cory Nov 2008 A1
20080305920 Nishii et al. Dec 2008 A1
20090023545 Beaudoin Jan 2009 A1
20090082169 Kolstrup Mar 2009 A1
20090107454 Hiyoshi et al. Apr 2009 A1
20090221391 Bazyn Sep 2009 A1
20090251013 Vollmer et al. Oct 2009 A1
20100093479 Carter et al. Apr 2010 A1
20100145573 Vasilescu Jun 2010 A1
20100181130 Chou Jul 2010 A1
20100267510 Nichols Oct 2010 A1
20110127096 Schneidewind Jun 2011 A1
20110230297 Shiina et al. Sep 2011 A1
20110237385 Andre Parise Sep 2011 A1
20110291507 Post Dec 2011 A1
20110319222 Ogawa et al. Dec 2011 A1
20120035011 Menachem et al. Feb 2012 A1
20120035015 Ogawa et al. Feb 2012 A1
20120258839 Smithson et al. Oct 2012 A1
20130035200 Noji et al. Feb 2013 A1
20130053211 Fukuda et al. Feb 2013 A1
20130190123 Pohl et al. Jul 2013 A1
20130288848 Carter et al. Oct 2013 A1
20130337971 Kostrup Dec 2013 A1
20140148303 Nichols et al. May 2014 A1
20140206499 Lohr Jul 2014 A1
20140248988 Lohr et al. Sep 2014 A1
20140257650 Carter et al. Sep 2014 A1
20140274536 Versteyhe Sep 2014 A1
20140323260 Miller et al. Oct 2014 A1
20140329637 Thomassy et al. Nov 2014 A1
20140335991 Lohr et al. Nov 2014 A1
20140365059 Keilers et al. Dec 2014 A1
20150018154 Thomassy Jan 2015 A1
20150039195 Pohl et al. Feb 2015 A1
20150051801 Quinn et al. Feb 2015 A1
20150080165 Pohl et al. Mar 2015 A1
20150226323 Pohl et al. Aug 2015 A1
20150233473 Miller et al. Aug 2015 A1
20150260284 Miller et al. Sep 2015 A1
20150337928 Smithson Nov 2015 A1
20150345599 Ogawa Dec 2015 A1
20150369348 Nichols et al. Dec 2015 A1
20160003349 Kimura et al. Jan 2016 A1
20160031526 Watarai Feb 2016 A1
20160040763 Nichols et al. Feb 2016 A1
20160061301 Bazyn et al. Mar 2016 A1
20160131231 Carter et al. May 2016 A1
20160146342 Vasiliotis et al. May 2016 A1
20160186847 Nichols et al. Jun 2016 A1
20160244063 Carter et al. Aug 2016 A1
20160273627 Miller et al. Sep 2016 A1
20160281825 Lohr et al. Sep 2016 A1
20160290451 Lohr Oct 2016 A1
20160298740 Carter et al. Oct 2016 A1
20160347411 Yamamoto et al. Dec 2016 A1
20160362108 Keilers et al. Dec 2016 A1
20170072782 Miller et al. Mar 2017 A1
20170082049 David et al. Mar 2017 A1
20170103053 Nichols et al. Apr 2017 A1
20170159812 Pohl et al. Jun 2017 A1
20170163138 Pohl Jun 2017 A1
20170204948 Thomassy et al. Jul 2017 A1
20170204969 Thomassy et al. Jul 2017 A1
20170211698 Lohr Jul 2017 A1
20170268638 Nichols et al. Sep 2017 A1
20170274903 Carter et al. Sep 2017 A1
20170276217 Nichols et al. Sep 2017 A1
20170284519 Kolstrup Oct 2017 A1
20170284520 Lohr et al. Oct 2017 A1
20170314655 Miller et al. Nov 2017 A1
Foreign Referenced Citations (223)
Number Date Country
118064 Dec 1926 CH
1054340 Sep 1991 CN
2245830 Jan 1997 CN
1157379 Aug 1997 CN
1167221 Dec 1997 CN
1178573 Apr 1998 CN
1178751 Apr 1998 CN
1204991 Jan 1999 CN
1283258 Feb 2001 CN
1300355 Jun 2001 CN
1412033 Apr 2003 CN
1434229 Aug 2003 CN
1474917 Feb 2004 CN
1483235 Mar 2004 CN
1568407 Jan 2005 CN
1654858 Aug 2005 CN
2714896 Aug 2005 CN
1736791 Feb 2006 CN
1847702 Oct 2006 CN
1860315 Nov 2006 CN
1940348 Apr 2007 CN
101016076 Aug 2007 CN
498 701 May 1930 DE
1171692 Jun 1964 DE
2021027 Dec 1970 DE
2 310880 Sep 1974 DE
2 136 243 Jan 1975 DE
2436496 Feb 1975 DE
39 40 919 Jun 1991 DE
19851738 May 2000 DE
10155372 May 2003 DE
102011016672 Oct 2012 DE
102012023551 Jun 2014 DE
102014007271 Dec 2014 DE
0 432 742 Dec 1990 EP
0 528 381 Feb 1993 EP
0 528 382 Feb 1993 EP
0 635 639 Jan 1995 EP
0 638 741 Feb 1995 EP
0 831 249 Mar 1998 EP
0 832 816 Apr 1998 EP
0 976 956 Feb 2000 EP
1 136 724 Sep 2001 EP
1 251 294 Oct 2002 EP
1 366 978 Mar 2003 EP
1 433 641 Jun 2004 EP
1 624 230 Feb 2006 EP
2 893 219 Jul 2015 EP
620375 Apr 1927 FR
2460427 Jan 1981 FR
2590638 May 1987 FR
391448 Apr 1933 GB
592320 Sep 1947 GB
906002 Sep 1962 GB
919430 Feb 1963 GB
1132473 Nov 1968 GB
1165545 Oct 1969 GB
1376057 Dec 1974 GB
2031822 Apr 1980 GB
2035481 Jun 1980 GB
2035482 Jun 1980 GB
2080452 Aug 1982 GB
38-025315 Nov 1963 JP
41-3126 Feb 1966 JP
42-2843 Feb 1967 JP
42-2844 Feb 1967 JP
44-1098 Jan 1969 JP
47-000448 Jan 1972 JP
47-207 Jun 1972 JP
47-20535 Jun 1972 JP
47-00962 Nov 1972 JP
47-29762 Nov 1972 JP
48-54371 Jul 1973 JP
49-12742 Mar 1974 JP
49-012742 Mar 1974 JP
49-013823 Apr 1974 JP
49-041536 Nov 1974 JP
50-114581 Sep 1975 JP
51-25903 Aug 1976 JP
51-150380 Dec 1976 JP
52-35481 Mar 1977 JP
53-048166 Jan 1978 JP
55-135259 Oct 1980 JP
56-24251 Mar 1981 JP
56-047231 Apr 1981 JP
56-101448 Aug 1981 JP
56-127852 Oct 1981 JP
58-065361 Apr 1983 JP
59-069565 Apr 1984 JP
59-144826 Aug 1984 JP
59-190557 Oct 1984 JP
60-247011 Dec 1985 JP
61-031754 Feb 1986 JP
61-053423 Mar 1986 JP
61-144466 Jul 1986 JP
61-173722 Oct 1986 JP
61-270552 Nov 1986 JP
62-075170 Apr 1987 JP
63-125854 May 1988 JP
63-219953 Sep 1988 JP
63-160465 Oct 1988 JP
01-039865 Nov 1989 JP
01-286750 Nov 1989 JP
01-308142 Dec 1989 JP
02-130224 May 1990 JP
02-157483 Jun 1990 JP
02-271142 Jun 1990 JP
02-182593 Jul 1990 JP
03-149442 Jun 1991 JP
03-223555 Oct 1991 JP
04-166619 Jun 1992 JP
04-272553 Sep 1992 JP
04-327055 Nov 1992 JP
04-351361 Dec 1992 JP
05-087154 Apr 1993 JP
06-050169 Feb 1994 JP
06-050358 Feb 1994 JP
07-42799 Feb 1995 JP
07-133857 May 1995 JP
07-139600 May 1995 JP
07-259950 Oct 1995 JP
08-135748 May 1996 JP
08-170706 Jul 1996 JP
08-247245 Sep 1996 JP
08-270772 Oct 1996 JP
09-024743 Jan 1997 JP
09-089064 Mar 1997 JP
10-061739 Mar 1998 JP
10-078094 Mar 1998 JP
10-089435 Apr 1998 JP
10-115355 May 1998 JP
10-115356 May 1998 JP
10-194186 Jul 1998 JP
10-225053 Aug 1998 JP
10-511621 Nov 1998 JP
11-063130 Mar 1999 JP
11-091411 Apr 1999 JP
11-210850 Aug 1999 JP
11-240481 Sep 1999 JP
11-257479 Sep 1999 JP
2000-6877 Jan 2000 JP
2000-46135 Feb 2000 JP
2000-177673 Jun 2000 JP
2001-027298 Jan 2001 JP
2001-071986 Mar 2001 JP
2001-107827 Apr 2001 JP
2001-165296 Jun 2001 JP
2001-234999 Aug 2001 JP
2001-328466 Nov 2001 JP
2002-147558 May 2002 JP
2002-250421 Jun 2002 JP
2002-307956 Oct 2002 JP
2002-533626 Oct 2002 JP
2002-372114 Dec 2002 JP
2003-028257 Jan 2003 JP
2003-56662 Feb 2003 JP
2003-161357 Jun 2003 JP
2003-194206 Jul 2003 JP
2003-194207 Jul 2003 JP
2003-320987 Nov 2003 JP
2003-336732 Nov 2003 JP
2004-011834 Jan 2004 JP
2004-38722 Feb 2004 JP
2004-162652 Jun 2004 JP
2004-189222 Jul 2004 JP
2004-526917 Sep 2004 JP
2004-301251 Oct 2004 JP
2005-003063 Jan 2005 JP
2005-096537 Apr 2005 JP
2005-188694 Jul 2005 JP
2005-240928 Sep 2005 JP
2005-312121 Nov 2005 JP
2006-015025 Jan 2006 JP
2006-283900 Oct 2006 JP
2006-300241 Nov 2006 JP
2007-085404 Apr 2007 JP
2007-321931 Dec 2007 JP
2008-002687 Jan 2008 JP
2008-133896 Jun 2008 JP
2010-069005 Apr 2010 JP
2012-225390 Nov 2012 JP
2015-227690 Dec 2015 JP
2015-227691 Dec 2015 JP
2002 0054126 Jul 2002 KR
10-2002-0071699 Sep 2002 KR
98467 Jul 1961 NE
74007 Jan 1984 TW
175100 Dec 1991 TW
218909 Jan 1994 TW
227206 Jul 1994 TW
275872 May 1996 TW
360184 Jun 1999 TW
366396 Aug 1999 TW
401496 Aug 2000 TW
510867 Nov 2002 TW
512211 Dec 2002 TW
582363 Apr 2004 TW
590955 Jun 2004 TW
I225129 Dec 2004 TW
I225912 Jan 2005 TW
I235214 Jan 2005 TW
M294598 Jul 2006 TW
200637745 Nov 2006 TW
200821218 May 2008 TW
WO 9908024 Feb 1999 WO
WO 9920918 Apr 1999 WO
WO 0173319 Oct 2001 WO
WO 03100294 Dec 2003 WO
WO 05083305 Sep 2005 WO
WO 05108825 Nov 2005 WO
WO 05111472 Nov 2005 WO
WO 06091503 Aug 2006 WO
WO 07077502 Jul 2007 WO
WO 08078047 Jul 2008 WO
WO 08100792 Aug 2008 WO
WO 10135407 Nov 2010 WO
WO 11064572 Jun 2011 WO
WO 11101991 Aug 2011 WO
WO 11121743 Oct 2011 WO
WO 12030213 Mar 2012 WO
WO 13042226 Mar 2013 WO
WO 14186732 Nov 2014 WO
WO 16062461 Apr 2016 WO
Non-Patent Literature Citations (5)
Entry
Office Action dated Aug. 29, 2013 in U.S. Appl. No. 13/288,711.
Office Action dated Apr. 2, 2014 in U.S. Appl. No. 13/288,711.
Thomassy: An Engineering Approach to Simulating Traction EHL. CVT-Hybrid International Conference Mecc/Maastricht/The Netherlands, Nov. 17-19, 2010, p. 97.
Office Action dated Mar. 5, 2015 in U.S. Appl. No. 14/541,875.
Office Action dated Aug. 3, 2015 in U.S. Appl. No. 14/541,875.
Related Publications (1)
Number Date Country
20160201772 A1 Jul 2016 US
Provisional Applications (1)
Number Date Country
61412290 Nov 2010 US
Continuations (2)
Number Date Country
Parent 14541875 Nov 2014 US
Child 15074267 US
Parent 13288711 Nov 2011 US
Child 14541875 US