Cycle suspension with rotation sensor

Information

  • Patent Grant
  • 12258095
  • Patent Number
    12,258,095
  • Date Filed
    Thursday, December 1, 2022
    2 years ago
  • Date Issued
    Tuesday, March 25, 2025
    18 days ago
Abstract
A suspension assembly for a cycle includes a plurality of links pivotably connected to one another by a plurality of pivots. A rotation sensor measures an angular relationship between two links and a setpoint of the suspension assembly is adjusted based on the angular measurements.
Description
INCORPORATION BY REFERENCE TO ANY PRIORITY APPLICATIONS

Any and all applications for which a foreign or domestic priority claim is identified in the Application Data Sheet as filed with the present application are hereby incorporated by reference under 37 CFR 1.57.


FIELD OF THE INVENTION

The disclosure is generally directed to wheel suspension assemblies for cycles, and is more specifically directed to wheel suspension assemblies for cycles that include a rotation sensor for measuring angular displacement between two links in the wheel suspension assembly.


BACKGROUND

Suspensions are important components of wheeled vehicles, including cycles. Suspensions allow a wheel to move in a compliant manner, relative to a frame, in response to ground conditions as a rider pilots the vehicle, while improving handling and control during riding. In many cases, suspensions comprise links and pivot assemblies which together form an articulating mechanism which allows a wheel to move. Pivot assemblies allow suspension components such as links to articulate in one or more degrees of freedom, typically via rotation.


Recently, telescopic front suspension forks have dominated suspension systems for two-wheeled vehicles. A telescopic fork includes sliding stanchions connected in a steerable manner to a vehicle frame, and at the same time, includes a telescoping mechanism for wheel displacement. Few, if any, telescopic forks include pivot assemblies.


Linkage front suspensions, comprising links and pivot assemblies, have been attempted in the past as an alternative to telescopic forks, yet they have failed to achieve market acceptance. In contrast, linkages comprising links and pivot assemblies account for almost all the rear suspensions available for two wheeled suspension structures sold today, and almost no examples of solely telescopic or sliding rear suspension structures can be found in today's marketplace.


While linkages including links and pivot assemblies can be economically manufactured, and typically feature very low friction, and linkages are also relatively easy to seal from the elements, many front suspension linkages suffer from poor kinematic performance, usually driven by prioritizing brake dive performance rather than stability.


Telescopic forks on the other hand use sliding stanchions, which require very expensive and tight manufacturing tolerances. Outer surfaces of the stanchion typically slide against bushings to allow for compliance. Front suspension for a cycle is subject to large bending forces fore and aft and less significant lateral forces. Because telescopic forks have relatively large stanchions, and relatively large sliding surfaces and seals, large breakaway friction in the system (known as stiction) is generated by these components. Stiction resists compression of the suspension in reaction to bumps, which is a drawback in a suspension product where the goal is to react to road or terrain conditions, for example by deflecting in response to ground conditions, and/or absorbing impact from bumps. Additionally, as the telescopic fork is loaded in the fore/aft direction (usually on impact or braking), the bushings bind, resulting in even greater stiction at the exact moment when a rider needs the most compliance. Telescopic forks and their large sliding bushings also require smooth stanchion surfaces and significant maintenance and upkeep to keep performance from diminishing quickly.


The quality of cycle suspension performance is correlated to proper setup for the rider. Proper setup for the rider includes adjusting the performance characteristics of certain suspension components to optimize overall ride characteristics, for a rider's weight and ability for example.


Adjusting rider setup on a telescopic fork or rear shock typically involves measuring fork or shock compression, which typically requires two people, one to compress the suspension and the other to measure the suspension displacement with a ruler. This is a difficult, time consuming, and frequently inaccurate method of measuring suspension displacement. External devices such as tape measures adapted for one person suspension displacement measuring have been tried with limited success. Another method involves affixing an o-ring around the stanchion or sliding shaft, and letting the o-ring contact the fork or shock seal. As the suspension compresses, the o-ring is forced along the stanchion or shaft via contact with the fork or shock seal, and then when the suspension is fully extended, the o-ring remains at the compressed position due to friction, and a measurement between measurement between the o-ring and fork or shock seal can be made to determine suspension travel used. Using an o-ring to measure travel is problematic because it can trap dirt and grit against the stanchion or shaft, causing surface damage and further compromising friction, stiction, and suspension performance. Furthermore, o-rings are fragile thin section pieces of rubber that can be easily damaged or degrade over time, and in some cases are impossible or difficult to replace when damaged due to fork or shock construction.


SUMMARY

In accordance with a first embodiment, a suspension assembly for a cycle includes a first link having a first pivot and a second link movably connected to the first link by the first pivot. A rotation sensor is operably connected to the first pivot. The rotation sensor measures angular displacement between the first link and the second link.


In accordance with a second embodiment, a front wheel suspension assembly for a cycle includes a first front suspension link having a first pivot and a second front suspension link movably connected to the first suspension link by the first pivot. A front wheel of a cycle is operably connected to one of the first front suspension link or the second front suspension link. A rotation sensor is operably connected to the first pivot, and the rotation sensor measures angular displacement between the first front suspension link and the second front suspension link.


In accordance with a third embodiment, a suspension assembly for a cycle includes a first link having a first pivot and a second link movably connected to the first link by the first pivot. A shock absorber is operably coupled to the first link or to the second link. The shock absorber includes a damper with a variable orifice.


The first, second, and third embodiments may include any one or more of the following aspects.


In one aspect, the first pivot is a fixed pivot and in another aspect, the first pivot is a floating pivot.


In another aspect, the first link is a fork arm.


In yet another aspect, the rotation sensor comprises one of a magnetic sensor, an optical sensor, an electrical sensor, an accelerometer, a potentiometer, or a resistive sensor.


In yet another aspect, the rotation sensor is one of an optical reflective sensor or an optical interrupter sensor.


In yet another aspect, the rotation sensor is one of a variable reluctance sensor, an eddy current killed oscillator sensor, a Wiegand sensor, or a Hall effect sensor.


In accordance with a fourth embodiment, a method for adjusting a suspension assembly for a cycle includes providing a suspension assembly including a first link having a first pivot, a second link movably connected to the first link by the first pivot, and a rotation sensor operably connected to the first pivot. The rotation sensor measures a first angular relationship between the first link and the second link when the suspension assembly is in an uncompressed state. The first angular relationship is output to a processor. The suspension assembly is moved into a compressed state. The rotation sensor measures a second angular relationship between the first link and the second link in the compressed date. The second angular relationship is output to the processor. A difference between the first angular relationship and the second angular relationship is calculated in the processor to determine a setpoint value for a component of the suspension assembly. The setpoint value from the processor is output to a display. A component of the suspension assembly is adjusted based on the setpoint value.


The fourth embodiment may include any one or more of the following aspects.


In one aspect, the first pivot is a fixed pivot and in another aspect, the first pivot is a floating pivot.


In another aspect, the first link is a fork arm.


In yet another aspect, the rotation sensor comprises one of a magnetic sensor, an optical sensor, an electrical sensor, an accelerometer, a potentiometer, or a resistive sensor.


In yet another aspect, the rotation sensor is one of an optical reflective sensor or an optical interrupter sensor.


In yet another aspect, the rotation sensor is one of a variable reluctance sensor, an eddy current killed oscillator sensor, a Wiegand sensor, or a Hall effect sensor.


In yet another aspect, the step of adjusting the component includes changing a characteristic of a shock absorber, a damper, or a combination of a shock absorber and a damper, based on the setpoint value.


In yet another aspect, the characteristic is a fluid flow rate through an orifice.


In yet another aspect, a size of the orifice is changed based on the setpoint value.


In yet another aspect, the step of adjusting the component includes changing a characteristic of one of a gas spring or a coil spring.


In yet another aspect, the characteristic is a spring constant.


In yet another aspect, the spring constant is changed by varying gas pressure in the gas spring.


In yet another aspect, the gas pressure is varied by changing an internal volume of the gas spring





BRIEF DESCRIPTION OF THE DRAWINGS


FIG. 1 is a side view of a cycle including a front wheel suspension assembly and a rear wheel suspension assembly constructed according to the teachings of the disclosure.



FIG. 2 is a side view of the front wheel assembly of FIG. 1.



FIG. 3 is a side view of a shock absorber of the front wheel assembly of FIG. 2.



FIG. 4 is a schematic diagram of two fluid chambers in a damper separated by a flow control device.



FIG. 5 is side view of the front wheel assembly of FIG. 2 in an uncompressed state.



FIG. 6 is a side view of the front wheel assembly of FIG. 2 in a partially compressed state.



FIG. 7 is a side view of the front wheel assembly of FIG. 2 in a further compressed state.



FIG. 8 is a side view of the front wheel assembly of FIG. 2 including a rotation sensor.



FIG. 9 is a side view of a link and a passive travel indicator of the front wheel assembly of FIG. 2.



FIG. 10A is a cross-sectional top view of the link of FIG. 9, including a pivot assembly, taken along line A-A of FIG. 9.



FIG. 10B is a close-up cross-sectional view of the pivot assembly and travel indicator of FIG. 9.



FIG. 11A is a side view of the link of FIG. 9 in a resting or unactuated first state.



FIG. 11B is a side view of the link of FIG. 9 in an actuated or partially rotated state.



FIG. 11C is a side plan view of the link of FIG. 9, returned to the resting or unactuated first state, with an indicator pointer of the travel indicator indicating a maximum percentage of travel reached.



FIG. 12 illustrates various views of a pivot assembly.



FIG. 13 is a perspective view of another embodiment of a front wheel suspension assembly including various adjustment ports for the shock absorber.



FIG. 14 is a side view of the front wheel suspension assembly of FIG. 13.



FIG. 15 is a logic diagram illustrating a method of adjusting a setpoint to customize ride characteristics for a rider.





DETAILED DESCRIPTION

The present invention is not limited to the specific embodiments described below, which are intended as exemplary illustrations of individual aspects of the invention. Functionally equivalent methods and components fall within the scope of the invention. Various modifications of the invention, in addition to those shown and described herein, will be apparent to those skilled in the art from the foregoing description. Such modifications are intended to fall within the scope of the appended claims. Throughout this application, the singular includes the plural and the plural includes the singular, unless indicated otherwise. The words “formed,” “provided,” “disposed,” and “located” are used interchangeably to denote relative positioning in the instant description. All cited publications, patents, and patent applications are herein incorporated by reference in their entirety.


The disclosed rotation sensor may be combined with multi-link cycle suspension assemblies, such as the suspension assemblies described in U.S. patent application Ser. No. 15/661,821, filed on Jul. 27, 2017; and the disclosed rotation sensor may be used in conjunction with pivot assemblies such as the pivot assemblies described in U.S. patent application Ser. No. 16/153,396, filed on Oct. 5, 2018. Each of U.S. patent application Ser. Nos. 15/661,821 and 16/153,396 are hereby incorporated by reference herein.


Turning now to FIG. 1, a cycle 10 includes a front wheel 51a and a rear wheel 51b, and a front wheel suspension assembly 12 including one or more pivot assemblies 20. While generally identified by the single reference numeral 20 in FIG. 1, specific pivot assemblies may be assigned unique reference numerals in further figures to clarify the location and/or function of unique pivot assemblies. All pivot assemblies identified by unique reference numerals below are pivot assemblies 20 as illustrated in FIG. 1. Additionally, while generally identified by a single reference numeral 22 in FIG. 1, the specific links may be assigned unique reference numerals in further figures to clarify the location and/or function of unique links. All links identified by unique reference numerals bellow are links 22 as illustrated in FIG. 1.


The front wheel suspension assembly 12 also includes a plurality of pivotably connected links 22. One or more of the links 22 may be pivotably connected to a frame member, such as a fork arm 24. The frame member 24 may act as a fixed location for the pivotably connected links 22. As the front wheel 51a moves relative to the frame member, due to changing ground topography/conditions, the links 22 articulate relative to one another, and relative to the frame member 24, thus allowing the front wheel 51a to move relative to the frame member 24 in a compliant manner in response to the changing ground topography/conditions as a rider pilots the cycle 10. The front wheel suspension assembly 12, and thus the links 22, improve handling and control during riding by directing movement of the front wheel 51a relative to the frame member 24 in a predictable and predetermined manner.

    • A rotation sensor 101 is included on one pivot assembly 20 to measure angular displacement between pivotably connected links 22 during compression of the front wheel suspension assembly 12, thereby providing the rider a measurement that may be used as a basis for making changes to suspension settings (e.g., changes to spring forces in a shock absorber or spring unit and/or to frictional forces in the pivot assembly) in a purposeful manner. As a result of these changes, the performance of the front wheel suspension assembly 12 is altered and improved, thus producing a better riding experience that is customized to the rider according to the manufacturer recommendations and/or a rider's preferences or capabilities. Although the rotation sensor 101 is illustrated in FIG. 1 as being located at a certain pivot 20, in other embodiments, the rotation sensor 101 may be located at any pivot 20 location, and/or at other locations in the front wheel suspension assembly 12.


As used herein, the term “operably connected” or “operable connection” means any direct or indirect connection between two elements. For example, if a first element is directly connected to a first link in a suspension assembly, the first element is “operably connected” to all links in the suspension assembly because the first element is indirectly connected to all links in the suspension assembly by the direct connection to the first link.


As illustrated in FIG. 2, the fork arm 24 is operably connected to a steering shaft 34. The steering shaft 34 includes a steering axis S that is formed by a central axis of the steering shaft 34. The fork arm 24 has a first end and 36 a second end 38, the fork arm 24 including a fork arm fixed pivot 40 and a fork arm shock pivot 42. The fork arm shock pivot 42 operably connects a suspension device, such as a shock absorber 44 to the fork arm 24. The shock absorber 44 is considered to be operably connected to (or to form an operable connection with) any link 22 in the front wheel suspension assembly 12 when the shock absorber 44 is directly connected to one link 22 in the front wheel suspension assembly 12. In other words, the shock absorber 44 is directly connected to one link 22 and indirectly connected to every other link 22 in the front wheel suspension assembly, and thus operably connected to (or forms an operable connection with) all links 22 in the front wheel suspension assembly 12. For example, the fork arm shock pivot 42 allows relative motion, in this case rotation, between the shock absorber 44 and the fork arm 24. In other embodiments, other types of relative motion, such as flexure or translation, between the shock absorber 44 and the fork arm 24 may be employed. The fork arm fixed pivot 40 pivotably connects one element of the front wheel suspension assembly 12, as discussed further below, to the fork arm 24.


A shock link 50 is pivotably connected to the first arm fixed pivot 40. The shock link 50 includes a shock link fixed pivot 52 and a shock link floating pivot 54 spaced apart from one another along a length of the shock link 50. The shock link 50 is pivotably connected to the fork arm fixed pivot 40 at the shock link fixed pivot 52 such that the shock link 50 is rotatable about the shock link fixed pivot 52 and the shock link fixed pivot 52 remains in a fixed location relative to the fork arm 24, while the shock link floating pivot 54 is movable relative to the fork arm 24.


A pivot, as used herein, includes any connection structure that may be used to operably connect one element to another element, and that allows relative movement between the connected components. An operative connection may allow for one component to move in relation to another while constraining movement in one or more degrees of freedom. For example, the one degree of freedom may be pivoting about an axis. In one embodiment, a pivot may be formed from a journal or through hole in one component and an axle in another component. In other examples, pivots may include ball and socket joints. Yet other examples of pivots include, but are not limited to singular embodiments and combinations of, compliant mounts, sandwich style mounts, post mounts, bushings, bearings, ball bearings, plain bearings, flexible couplings, flexure pivots, journals, holes, pins, bolts, and other fasteners. Also, as used herein, a fixed pivot is defined as a pivotable structure that does not change position relative the fork arm 24. As used herein, a floating pivot is defined as a pivot that is movable (or changes position) relative to another element, and in this case, is movable relative to fork arm 24. Some examples of pivot structures are further discussed with reference to FIG. 12 below.


The linkage or front wheel suspension assembly 12 is configured in a trailing orientation. A trailing orientation is defined herein as a linkage that includes a fixed pivot that is forward of the corresponding floating pivot when the cycle is traveling in the forward direction of travel as represented by arrow A in FIG. 2. In other words, the floating pivot trails the fixed pivot when the cycle is traveling in the forward direction of travel. For example, in the illustrated embodiment, the shock link fixed pivot 52 is forward of the shock link floating pivot 54. The disclosed linkage or suspension assembly 12 is also characterized as a multi-link or multi-bar suspension assembly. A multi-link suspension assembly is defined herein as a suspension assembly having a plurality of interconnected links in which any part of the front wheel 51a is directly connected to a link in the plurality of interconnected links that is not directly connected to the fork arm 24.


Turning now to FIG. 3, the shock absorber 44 includes a first shock mount 56 and a second shock mount 58, the first shock mount 56 being pivotably connected to the fork arm shock pivot 42, the second shock mount 58 being pivotably connected to a shock connection pivot 60 located between the shock link fixed pivot 52 and the shock link floating pivot 54 along a length of the shock link 50. The shock absorber 44 includes a spring, such as a gas spring 92 having a spring body 88 (other embodiments may include other types of springs, such as a coil spring), a damper 94 having a damper body 89, an inshaft 80, and outshaft 90, a damper piston 83, a gas piston 81, and a shaft seal 85. In the art, a damper may also be referred to as a dashpot and a gas spring may also be referred to as a mechanical spring.


The inshaft 80 and outshaft 90 can comprise a singular component or plurality of components, and may be combined with other components. In some embodiments, the damper piston 83 may be connected to or include a portion or the entirety of the inshaft 80 or outshaft 90. In some embodiments, the damper piston 83 has a greater radial cross-sectional area than the inshaft 80 or the outshaft 90. The inshaft 80 and outshaft 90 can extend between and through a shaft seal 85 to operably connect a gas spring with a damper to provide concurrent movement of the inshaft 80, outshaft 90, gas piston 81, and damper piston 83 during suspension compression and extension.


The spring body 88 may include a gas chamber 88a, which is pressurized with a gas. The pressurized gas biases the gas piston 81 towards the damper body 89. The pressure of the gas within the gas chamber 88a may be changed, as discussed further below, by either changing the volume of the gas chamber 88a, or by adding or subtracting gas molecules to/from the gas chamber 88a, to adjust a setpoint of the front wheel suspension assembly 12 according to rider ability or characteristics.


The damper body 89 may include a first fluid chamber 89a and a second fluid chamber 89b, and a damping fluid. The damping fluid moves between the first fluid chamber 89a and the second fluid chamber 89b, which are separated by a flow control device, such as a flow restriction or a variable orifice (see FIG. 4) thus creating a resistive or damping force in a direction opposite to the movement of the damper piston 83. In other embodiments, the first fluid chamber 89a and the second fluid chamber 89b may be located on one side of the damper piston 83 and separated by a flow control device, and in other embodiments, the first fluid chamber 89a and the second fluid chamber 89b may be fluidly connected by an external flow control device.


Dampers can be dry-friction, or hydraulically based with fluid elements. Dampers dissipate motion energy in the front wheel suspension assembly 12 by producing a force that opposes the direction of motion. Generally, hydraulic dampers include two or more fluid chambers. Fluid moves from one chamber to the other during movement of a piston. Generally, one chamber experiences high pressure during compression and the other chamber experiences high pressure during extension or rebound. As fluid moves between the two chambers, it passes through a flow control device, such as a flow restriction. As the fluid moves through the flow restriction, cavitation can occur due to pressure differences. Increasing the pressure of the oil can reduce cavitation. The oil pressure may be increased by applying force from a spring, such as a gas spring, to the damper stem. For example, in the disclosed embodiment, the gas spring 92 is connected to the outshaft 90, which is connected to the damper piston 83.


In one embodiment, the damper 94 may comprise a twin-tube damper. In other embodiments, the damper 94 may comprise a through-rod telescopic damper, a single tube telescopic damper, or a single tube telescopic damper with a compression piston. Some examples of single tube and twin-tube dampers may be found in “Development of software that can predict damper curves on shock absorbers,” Uppsala Universitet, Examensarbete 15 hp, June 2013; “Understanding your Dampers: A guide from Jim Kasprzak,” www.kaztechnolgies.com; “Flow control valves,” Hydraulics and Pneumatics, Jan. 1, 2012, http://hydraulicspneumatics.com/200/TechZone/HydraulicValves/Article/False/6409/TechZone-HydraulicValves; and “The Shock Absorber Handbook,” John C. Dixon, Chichester, England, John Wiley, 2007; each of which is hereby incorporated by reference herein.


In some embodiments, the flow control device may comprise a flow restriction such as a narrow passageway. In other embodiments, the flow control device may comprise a variable orifice having an orifice or passageway with a variable cross-sectional area. In other embodiments, the flow control device may comprise a valve, such as a calibrated needle valve. In yet other embodiments, the flow control device may comprise a fluid control regulator. In yet other embodiments, the flow control device may comprise an electrohydraulic valve with a closed loop feedback.


In some embodiments, the flow control device may be located in the damper piston, which is sometimes called a piston valve. In other embodiments, the flow control device may be located between two chambers that are not separated by the piston, this location is sometimes called a foot valve. In other embodiments, the damper may include more than one flow control device, each flow control device targeting a different flow characteristic, such as one flow control device that targets a high speed characteristic and another flow control device that targets a low speed characteristic.


Turning now to FIG. 4, a schematic diagram of the first and second fluid chambers 89a, 89b is illustrated. The first and second fluid chambers 89a, 89b are fluidly connected and are separated by the flow control device, such as a variable orifice 83a.


The pressure of the gas in the gas chamber 88a and the flow control device may be adjusted to change the performance characteristics (or setup) of the front wheel suspension assembly 12, as further discussed below.


The damper piston mates to or includes a damper piston seal 93. In some embodiments, the damper piston seal 93 may comprise; multiple, or combinations of glide ring, wear band, o-ring. X-ring, Q ring, quad ring, Teflon seal, cap seal, piston ring, solid piston, T seal, V ring, U cup, urethane seal, PSQ seal, preloaded piston band, or other type of band or seal. The damper piston seal 93 is intended to seal damping fluid between each side of the damper piston 83, while allowing axial movement of the damper piston 83 and therefore axial movement of the inshaft 80 and/or outshaft 90.


In certain embodiments, the gas spring 92 has certain advantages over other types of springs. The gas spring 92 uses a pressurized gas such as air, nitrogen, or other gases to act on the area of a gas piston 81, which results in a force against the gas piston 81. In certain embodiments, a user can change the gas pressure and therefore the force output at the gas piston 81. This allows the user to tailor output force based on preferences or to meet the requirements of varying road conditions. In certain embodiments, a gas spring 92 may comprise pressures that can act on both sides of the gas piston 81. By varying the volume of gas acting on each side of the gas piston 81 and the area of each side of the gas piston 81, one can vary the amount of force output at the gas piston 81 at various points in the damper displacement. This variability can be a valuable tool for allowing the user to tailor output force based on their preference or to meet the requirements of varying road conditions.


The gas piston 81 can be connected to or include a portion or the entirety of the inshaft 80 or outshaft 90. In preferred embodiments, the gas piston 81 has a greater radial cross-sectional area than the inshaft 80 or the outshaft 90. In certain other preferred embodiments, the gas piston 81 has a greater radial cross-sectional area than the damper piston 83. The gas piston 81 mates to or includes a gas piston seal 91. In some embodiments, the gas piston seal 91 may comprise; singular, multiple, or combinations of glide ring, wear band, o-ring. X-ring, Q ring, quad ring, Teflon seal, cap seal, piston ring, solid piston, T seal, V ring, U cup, urethane seal, PSQ seal, preloaded piston band, or other type of band or seal. The gas piston seal 91 is intended to seal gas between each side of the gas piston 81, while allowing axial movement of the gas piston 81 and therefore axial movement of the inshaft 80 and/or outshaft 90.


The shock absorber 44 includes the shaft seals 85. The shaft seals 45 are used to seal damping fluid or gas inside the damper body 89 or spring body 88 while allowing axial movement of an inshaft 80 and/or outshaft 90. The shaft seals 45 can be located at one end of a spring body 88, while sealing gas inside the spring body 88 and allowing axial movement of an inshaft 80 or outshaft 90. The shaft seals 45 can be located at one or more ends of a damper body 89, while sealing damping fluid inside the damper body 89 and allowing axial movement of an inshaft 80 or outshaft 90.


Returning now to FIG. 2, a wheel carrier 62 includes a wheel carrier first pivot 64 and a wheel carrier second pivot 66 spaced apart from one another along a length of the wheel carrier 62. Both the wheel carrier first pivot 64 and the wheel carrier second pivot 66 are floating pivots, as they both move relative to the first arm 32. A wheel mount 68 is adapted to be connected to a center of a wheel, for example the front wheel 51a. In the disclosed embodiment, a center of the front wheel 51a is rotatably connected to the wheel mount 68. The wheel carrier first pivot 64 is pivotably connected to the shock link floating pivot 54 so that the wheel carrier second pivot 66 is pivotable about the wheel carrier first pivot 64 relative to the shock link floating pivot 54.


A control link 70 includes a control link floating pivot 72 and a control link fixed pivot 74. The control link floating pivot 72 is pivotably connected to the wheel carrier second pivot 66, and the control link fixed pivot 74 is pivotably connected to a fork arm control pivot 76 located on the fork arm 24 such that the control link floating pivot 72 is pivotable about the control link fixed pivot 74, which remains in a fixed location relative to the fork arm control pivot 76.


In some embodiments, the shock connection pivot 60 is closer to the shock link fixed pivot 52 than to the shock link floating pivot 54, as illustrated in FIG. 2. As a function of suspension compression and link movement, a perpendicular distance D between a central axis I of an inshaft 80 of the shock absorber 44 and a center of the shock link fixed pivot 52 varies as the shock absorber 44 is compressed and extended, as the shock absorber pivots about the first shock mount 56. This pivoting and varying of the perpendicular distance D allows the leverage ratio and motion ratio to vary as the shock absorber 44 compresses and extends. As a function of suspension compression and link movement, a mechanical trail distance T varies as the shock absorber 44 compresses and extends. The mechanical trail distance T is defined as the perpendicular distance between the steering axis S and the contact point 82 of the front wheel 51a with the ground 84. More specifically, as the suspension compresses, beginning at a state of full extension, the mechanical trail distance T increases, thus increasing stability during compression. Compression is usually experienced during braking, cornering, and shock absorbing, all of which benefit from increased stability that results from the mechanical trail distance increase.


Mechanical trail (or “trail”, or “caster”) is an important metric relating to handling characteristics of two-wheeled cycles. Mechanical trail is a configuration in which the wheel is rotatably attached to a fork, which has a steering axis that is offset from the contact point of the wheel with the ground. When the steering axis is forward of the contact point, as in the case of a shopping cart, this configuration allows the caster wheel to follow the direction of cart travel. If the contact point moves forward of the steering axis (for example when reversing direction of a shopping cart), the directional control becomes unstable and the wheel spins around to the original position in which the contact point trails the steering axis. The friction between the ground and the wheel causes a self-righting torque that tends to force the wheel to trail the steering axis. The greater the distance between the contact point and perpendicular to the steering axis, the more torque is generated, and the greater the stability of the system. Similarly, the longer the distance between the cycle wheel contact point and perpendicular to the steering axis, the more torque is generated, and the greater the stability of the system. Conversely, the shorter the distance between the cycle wheel contact point and perpendicular to the steering axis, the less torque is generated, and the lower the stability of the system.


This caster effect is an important design characteristic in cycles. Generally, the caster effect describes the cycle rider's perception of stability resulting from the mechanical trail distance described above. If the wheel gets out of line, a self-aligning torque automatically causes the wheel to follow the steering axis again due to the orientation of the wheel ground contact point being behind the steering axis of the fork. As the contact point of the wheel with the ground is moved further behind the steering axis, self aligning torque increases. This increase in stability is referred to herein as the caster effect.


In the disclosed front wheel suspension assembly 12, when the suspension is at a state of full extension, the steering axis of the fork 30 projects ahead of the contact point 82. As the suspension assembly moves towards a state of full compression, the steering axis S projects farther ahead of the contact point 82, which results in the stability increasing. This increased stability stands in contrast to known telescopic fork cycles, which experience reduced trail and thus reduced stability during compression.


Leverage ratios or motion ratios are important metrics relating to performance characteristics of some suspensions. In certain embodiments, a shock absorber can be compressed at a constant or variable rate as the suspension moves at a constant rate towards a state of full compression. As a wheel is compressed, incremental suspension compression distance measurements are taken. Incremental suspension compression distance is measured from the center of the wheel at the wheel rotation axis and parallel with the steering axis, starting from a state of full suspension extension, and moving towards a state of full suspension compression. These incremental measurements are called the incremental suspension compression distance. A shock absorber length can be changed by wheel link, and/or brake link, and/or control link movements as the suspension compresses. At each incremental suspension compression distance measurement, a shock absorber length measurement is taken. The relationship between incremental suspension compression distance change and shock absorber length change for correlating measurements of the suspension's compression is called leverage ratio or motion ratio. Leverage ratio and motion ratio are effectively equivalent but mathematically different methods of quantifying the effects of variable suspension compression distance versus shock compression distance. Overall leverage ratio is the average leverage ratio across the entire range of compression. Overall leverage ratio can be calculated by dividing the total suspension compression distance by the total shock absorber compression distance. Overall motion ratio is the average motion ratio across the entire range of compression. Overall motion ratio can be calculated by dividing the total shock absorber compression distance by the total suspension compression distance.


Generally, a suspended wheel has a compressible wheel suspension travel distance that features a beginning travel state where the suspension is completely uncompressed to a state where no further suspension extension can take place, and an end travel state where a suspension is completely compressed to a state where no further suspension compression can take place. At the beginning of the wheel suspension travel distance, when the suspension is in a completely uncompressed state, the shock absorber is in a state of least compression, and the suspension is easily compressed. As the suspended wheel moves compressively, force at the wheel changes in relation to shock absorber force multiplied by a leverage ratio. A leverage ratio is defined as the ratio of compressive wheel travel change divided by shock absorber measured length change over an identical and correlating given wheel travel distance. A motion ratio is defined as the ratio of shock absorber measured length change divided by compressive wheel travel change over an identical and correlating given wheel travel distance.


In known telescopic forks no leverage ratio exists and, the leverage ratio is always equivalent to 1:1 due to the direct coupling of the wheel to the shock absorber.


A leverage ratio curve is a graphed quantifiable representation of leverage ratio versus wheel compression distance or percentage of full compression distance. Wheel compression distance, suspension compression, or wheel travel is measured from the center of the wheel at the wheel rotation axis and parallel with the steering axis, with the initial 0 percent measurement taken at full suspension extension with the vehicle unladen. As a suspension is compressed from a state of full extension to a state of full compression at a constant rate, measurements of shock absorber length are taken as the shortest distance between a first shock pivot and a second shock pivot at equal increments of suspension compression. When graphed as a curve on a Cartesian graph, leverage ratio is shown on the Y axis escalating from the x axis in a positive direction, and vertical wheel travel is shown on the X axis escalating from the Y axis in a positive direction.


A motion ratio curve is a graphed quantifiable representation of motion ratio versus wheel compression distance or percentage of full compression distance. Wheel compression distance, suspension compression, or wheel travel is measured from the center of the wheel at the wheel rotation axis and parallel with the steering axis, with the initial 0 percent measurement taken at full suspension extension with the vehicle unladen. As a suspension is compressed from a state of full extension to a state of full compression, measurements of shock absorber length are taken as the shortest distance between a first shock pivot and a second shock pivot at equal increments of suspension compression. When graphed as a curve on a Cartesian graph, motion ratio is shown on the Y axis escalating from the x axis in a positive direction, and vertical wheel travel is shown on the X axis escalating from the Y axis in a positive direction.

    • In certain embodiments, a leverage ratio or motion ratio curve can be broken down into three equal parts in relation to wheel compression distance or vertical wheel travel, a beginning ⅓ (third), a middle ⅓, and an end ⅓. In certain embodiments, a beginning ⅓ can comprise a positive slope, zero slope, and/or a negative slope. In certain embodiments, a middle ⅓ can comprise a positive slope, zero slope, and/or a negative slope. In certain embodiments, an end ⅓ can comprise a positive slope, zero slope, and/or a negative slope. Certain preferred leverage ratio embodiments can comprise a beginning ⅓ with a positive slope, a middle ⅓ with a less positive slope, and an end ⅓ with a more positive slope. Certain preferred leverage ratio embodiments can comprise a beginning ⅓ with a negative slope, a middle ⅓ with negative and zero slope, and an end ⅓ with a positive slope. Certain preferred leverage ratio embodiments can comprise a beginning ⅓ with a positive and negative slope, a middle ⅓ with negative and zero slope, and an end ⅓ with a positive slope. Certain preferred leverage ratio embodiments can comprise a beginning ⅓ with a positive and negative slope, a middle ⅓ with negative and zero slope, and an end ⅓ with a more negative slope. Certain preferred motion ratio embodiments can comprise a beginning ⅓ with a negative slope, a middle ⅓ with a less negative slope, and an end ⅓ with a more negative slope. Certain preferred motion ratio embodiments can comprise a beginning ⅓ with a positive slope, a middle ⅓ with positive and zero slope, and an end ⅓ with a negative slope. Certain preferred motion ratio embodiments can comprise a beginning ⅓ with a negative and positive slope, a middle ⅓ with positive and zero slope, and an end ⅓ with a negative slope. Certain preferred motion ratio embodiments can comprise a beginning ⅓ with a negative and positive slope, a middle ⅓ with positive and zero slope, and an end ⅓ with a more positive slope.


In contrast to telescopic suspensions, the disclosed front wheel suspension assembly 12 provides a greater than 1:1 overall leverage ratio between the shock absorber 44 and the shock link 50, due to the indirect coupling of the front wheel 51a and the shock absorber 44. Additionally, because of the movement arcs of the various linkage elements, at any given point during compression, instantaneous leverage ratio and motion ratio can vary non-linearly.


The central axis I of the inshaft 80 of the shock absorber 44 is arranged to form an angle B of between 0° and 20° relative to a central axis F of the fork arm 24, the central axis F of the fork arm 24 being defined by a line formed between the fork arm shock pivot 42 and the fork arm fixed pivot 40. In other embodiments, the central axis I of the inshaft 80 of the shock absorber 44 forms an angle with the central axis F of the fork arm 24 of between 0° and 15°. In other embodiments, the central axis I of the inshaft 80 of the shock absorber 44 forms an angle with the central axis F of the fork arm 24 of between 0° and 30°. The angle B may vary within these ranges during compression and extension.


In some embodiments, the fork arm 24 includes a hollow portion 86 and the shock absorber 44 is located at least partially within the hollow portion 86 of the fork arm 24.


The shock link fixed pivot 52 is offset forward of the central axis I of the inshaft 80 of the shock absorber 44. In other words, the central axis I of the inshaft 80 of the shock absorber 44 is positioned between the shock link fixed pivot 52 and the shock link floating pivot 54 in a plane defined by the central axis I of the inshaft 80, the shock link fixed pivot 52 and the shock link floating pivot 54 (i.e., the plane defined by the view of FIG. 2).


A line between the wheel carrier first pivot 64 and the wheel carrier second pivot 66 defines a wheel carrier axis WC, and the wheel mount 68 is offset from the wheel carrier axis WC in a plane defined by the wheel carrier axis WC and the wheel mount 68 (i.e., the plane defined by the view of FIG. 2). In some embodiments, the wheel mount 68 is offset from the wheel carrier axis WC towards the fork arm 24, for example the embodiment illustrated in FIG. 2. In other embodiments, the wheel mount 68 may be offset from the wheel carrier axis WC away from the fork arm 24. In yet other embodiments, the wheel mount 68 may lie on the wheel carrier axis WC.


In the embodiment of FIG. 2, the wheel mount 68 is located aft of the shock link fixed pivot 52, such that the central axis I of the inshaft 80 of the shock absorber 44 is located between the wheel mount 68 and the shock link fixed pivot 52 in a plane defined by the central axis I of the inshaft 80 of the shock absorber 44, the wheel mount 68 and the shock link fixed pivot 52 (i.e., the plane defined by the view of FIG. 2).


Returning to FIG. 3, the shock absorber 44 may include an inline shock absorber having a damper body 89 and a spring body 88 that are sequentially arranged along a substantially common central axis.


The damper body 89 and the spring body 88 shall be considered to be inline and arranged sequentially along a substantially common central axis when a central axis of the spring body 88 and a central axis of the damper body 89 are offset from one another by a maximum of 100% of the outside diameter of an inshaft 80. In other embodiments, the damper body 89 and the spring body 88 are offset from one another by a maximum of 50% of the outside diameter of the inshaft 80. In other embodiments, the damper body 89 and the spring body 88 are offset from one another by a maximum of 33% of the outside diameter of the inshaft 80. In yet other embodiments, the damper body 89 and the spring body 88 are offset from one another by a maximum of 25% of the outside diameter of the inshaft 80. In a preferred embodiment, the damper body 89 and the spring body 88 share a common central axis.


The inshaft 80 extends from the damper body 89, and an outshaft 90 extends through the damper body 89 and into the spring body 88. The second shock mount 58 is formed at one end of the inshaft 80, and the inshaft 80 is pivotably connected to the shock connection pivot 60 by the second shock mount 58 such that the inshaft 80 and the outshaft 90 are compressible and extendable relative to the damper body 89 as the shock link 50 pivots about the shock link fixed pivot 52. In the embodiments of FIG. 3, the damper body 89 is located between the spring body 88 and the second shock mount 58. In other embodiments, the spring body may be located between the damper body and the second shock mount.


Returning now to FIG. 2, the control link 70 is pivotably mounted to the fork arm 24 at the fork arm control pivot 76 that is located between the fork arm fixed pivot 40 and the fork arm shock pivot 42, along a length of the fork arm 24.


Turning to FIGS. 5-7, generally, as the front wheel suspension assembly 12 initially compresses (e.g., one or more links in the suspension assembly has a component of movement in a direction 510 that is substantially parallel to the steering axis S), a mechanical trail distance T initially increases due to the angular change in the steering axis S, which projects a bottom of the steering axis forward, relative to the wheel contact point 82 with the ground 84. This increase in mechanical trail distance T also increases the caster effect by creating a larger moment arm, between the steering axis 82 and the wheel contact point 82, to correct off-center deflections of the front wheel 51a. As a result, the front wheel 51a becomes more statically and dynamically stable as the front wheel suspension assembly 12 compresses and the mechanical trail distance T increases.


For example, for each embodiment disclosed herein, when suspension assembly compression is initiated (relative to an uncompressed state), mechanical trail distance T increases. Mechanical trail distance T may increase, for example continuously increase, from a minimum value in the uncompressed state of the suspension assembly to a maximum value in the fully compressed state of the suspension assembly. In other embodiments, mechanical trail distance T may increase initially from the uncompressed state of the suspension assembly to a maximum value at a partially compressed intermediate state of the suspension assembly, and then mechanical trail distance T may decrease from the maximum value as the suspension assembly continues compression from the partially compressed intermediate state to the fully compressed state.


When the disclosed front wheel suspension assembly 12 is at a fully extended state (e.g., uncompressed), as illustrated in FIG. 5, for example, the steering axis S projects ahead of the contact point 82, where the front wheel 51a contacts the ground 84. In various states of compression between uncompressed and fully compressed, suspension assembly compression can be measured as a component of linear distance that the wheel mount 68 moves in a travel direction 510 aligned with and parallel to the steering axis S. Alternatively, as discussed further below with respect to FIG. 8, suspension assembly compression may be measured as a change in the angular relationship between two links in the suspension assembly.


As the front wheel suspension assembly 12 initially begins to compress, the front wheel suspension assembly 12 moves through a partially compressed intermediate state, as illustrated in FIG. 6. In the partially compressed intermediate state illustrated in FIG. 6, the steering axis S projects farther ahead of the contact point 82 than in the fully extended state of FIG. 5, which results in a decrease of an offset distance 515 of the wheel mount and a corresponding increase in the mechanical trail distance T. In the embodiment of FIGS. 5-7, the offset distance 515, which is defined as the perpendicular distance between the steering axis S and a center of the wheel mount 68 of the front wheel 51a, decreases as the front wheel suspension assembly 12 compresses. The offset distance 515 generally decreases during suspension assembly compression because the wheel mount 68 moves in the aft direction, to the left in FIGS. 5-7. In other embodiments, as the front wheel suspension assembly 12 compresses, beginning at a state of full extension, the offset distance 515 can increase or decrease, during suspension compression, depending on variables including wheel 51a diameter, steering angle 520, and initial mechanical trail distance T.


The mechanical trail distance T is larger in the partially compressed intermediate state of FIG. 6 than in the fully extended state of FIG. 5. This increase in mechanical trail distance T results in increased stability, as described above. This increased mechanical trail distance T, and corresponding increase in stability, is the opposite result of what happens when telescopic fork suspension assemblies compress, which is a reduced mechanical trail distance and thus, a reduction in stability. Increasing mechanical trail distance as the suspension assembly compresses is a significant performance advantage over existing suspension assemblies.


As stated above, the increase in mechanical trail distance T as the front wheel suspension assembly 12 compresses advantageously increases wheel stability due to the increased caster effect. Compression is usually experienced during challenging riding conditions, such as braking, cornering, and shock absorbing, all of which benefit from the advantageously increased stability that results from the mechanical trail distance increase observed in the disclosed front wheel suspension assemblies.


As the front wheel suspension assembly 12 moves towards the further compressed state, for example as illustrated in FIG. 7, the steering axis S projects even farther ahead of the contact point 82, which results in a further decrease of a wheel carrier displacement distance 515 and a corresponding further increase in the mechanical trail distance T. The mechanical trail distance T is larger in the further compressed state of FIG. 7 than in the fully extended state of FIG. 5 or than in the partially compressed intermediate state of FIG. 6. This increase in mechanical trail distance T results in further increased stability. In the embodiment of FIGS. 5-7, increased mechanical trail distance T, and thus increased stability, occur when the suspension assembly is in the further compressed state (FIG. 7). In some embodiments, the mechanical trail distance T may decrease between the further compressed state (FIG. 7) and a fully compressed state (not shown). In yet other embodiments, the mechanical trail distance T may continue to increase from the further compressed state (FIG. 7) to the fully compressed state (not shown).


As a function of suspension compression and link movement, the mechanical trail distance T, and the offset distance 515, vary as the suspension assembly compresses and extends. In some embodiments, the mechanical trail distance T may increase, for example continuously increase, from full extension to full compression. In some embodiments, the increase in mechanical trail distance T may occur at a non constant (e.g., increasing or decreasing) rate.


Turning now to FIG. 8, in some embodiments, a rotation sensor 101 may be located at any of the pivots, for example, at the shock link fixed pivot 52 in the embodiment of FIG. 8. The rotation sensor 101 measures angular displacement between the shock link 50 and the fork arm 24. In other embodiments, the rotation sensor 101 may measure angular displacement between any of the other links and may be located at any of the other pivots. The rotation sensor 101 may transmit the sensed data to a processor 102. In some embodiments, the processor 102 may be directly communicatively linked with the rotation sensor 101, where data is displayed on a monitor or display unit (not shown). In other embodiments, the processor 102 may be located remote from the rotation sensor 101 and data may be transmitted wirelessly. The processor 102 may process data from the rotation sensor 101 for display on a display unit, and/or save historical sensor data for later use. The data from the rotation sensor 101 may be used to modify the setup (e.g., change the ride characteristics) of the front wheel suspension assembly 12, which will be further described below with reference to FIGS. 13-15.


Advantageously, the rotation sensor 101 measures instantaneous rotation data that may be electronically output to a processor and/or a display for real-time use. The rotation sensor 101 also advantageously measures rotation data from a starting point without the need to be reset before every measurement. As a result, the rotation sensor 101 is capable of measuring a lesser rotation immediately after a greater rotation, without the need to reset the sensor. Additionally, the rotation sensor 101 can average measurements, or output other statistical data from as set of rotational measurement readings.


Turning now to FIGS. 9-12, in some embodiments, a pivot assembly 20 may also include an indicator 16 and a scale 18 in addition to a bolt 2 and a pivot body 4. The indicator 16 and scale 18 measure maximum deflection of the pivot assembly 20 during compression of the suspension assembly 12.


The pivot assembly 20 is seated in a central aperture 133 of a housing, such as a body of a link 114. The link 114 may be any of the links illustrated above. For example, the link 114 may be the shock link 50, the wheel carrier 60, or the control link 70. The indicator 16 is located about a circumference of the bolt 2, and the indicator 16 includes a first retention feature or protrusion 134, and a pointer 130. The bolt 2 includes a second retention feature or channel 140. In other embodiments, the second retention feature may be located about a circumference of the pivot body 4. While the first retention feature is illustrated as a protrusion 134 and the second retention feature is illustrated as a channel 140, in other embodiments, the protrusion 134 and the channel 140 may be reversed, or other retention features may be used that axially locate the indicator 16 relative to the pivot assembly 20 while allowing rotational movement between the indicator 16 and the pivot assembly 20 when a threshold force is exceeded.


The scale 18 is located on an external component, such as on the housing 114. The housing 114 may be part of a link 122, or in other embodiments, the housing may be part of a frame member, such as the fork arm 124. A bearing 110 is installed in the central aperture 133. The bearing 110 facilitates rotational movement between the pivot assembly 20 and the housing 114. The pivot assembly 20 positions the bearing 110 in radial and axial directions relative to the housing 114 such that any combination of links 122 or frame members 24 can articulate in a pivotable or rotatable manner. The first interference member 134 on the indicator 16 interfaces with, or is partially seated within, the second interference member 140 on the bolt 2, such that the first interference member 134 and second interference member 140 allow rotation of the indicator 16 when enough force is applied to overcome rotational friction and, at the same time, produce enough rotational friction to prevent rotation of the indicator 16 relative to the bolt 2 when sufficient force is not present, thereby maintaining relative positioning between the indicator 16 and the bolt 2 unless sufficient force is applied.


For example, the rotational friction between the first interference member 134 and the second interference member 140 may be overcome to cause the indicator 16 to rotate relative to the bolt 2 when force is applied to the indicator 16 by, for example, an actuator 126 during suspension assembly compression, or to return the indicator 16 to a starting position by force applied by a tool or a finger after suspension assembly is complete. By allowing the indicator 16 to rotate relative to the bolt 2 during suspension assembly compression, and by maintaining the indicator 16 rotational position relative to the bolt 2 when suspension assembly compression is complete, the indicator 16 provides a measurement of maximum suspension assembly compression for a compression event. The measurement may then be used by the rider to adjust suspension assembly characteristics to improve suspension assembly performance. While the first interference member 134 is illustrated as one or more protrusions and the second interface member 140 is illustrated as an annular channel, in other embodiments, the protrusions and the annular channel may be reversed, or other connection structures that produce rotational friction may be used. In some preferred embodiments, the indicator 16 comprises one or more of metal, plastic, composites, and compliant materials, such as natural or synthetic rubbers and urethanes. In other embodiments, the indicator comprises one or more of rubber, aluminum, steel, copper, other metals, fiberglass, carbon fiber, fiber reinforced thermoplastics, urethanes, foam, wood, and bamboo.


Turning now to FIGS. 11A-11C, the link 122 is illustrated in several views. Although referenced and illustrated in other figures, the bearing 110 and the pivot assembly 20 are not illustrated in FIGS. 11A-11C. As discussed above, the housing 114 may be part of the link 122. The actuator 126, which in the illustrated embodiment as a peg extending outward from the housing 114, and the scale 18 are also located on the housing 114. The housing 114 interfaces with or receives the bearing 110 and/or the pivot assembly 20. The bearing 110 may be press fit or slid into the central aperture 133 in the housing 114, and the pivot assembly 20 may then be press fit or slid into the central aperture 133 in the housing 114 as well. The scale 18 is attached to, or formed on an outer surface of the housing 114 proximate the central aperture 133. The scale 18 includes graduations or indications that line up with the pointer 130 of the indicator 16 subsequent to compression of the front wheel suspension assembly 12, thereby allowing the registering and measuring of a travel reading (e.g., suspension assembly compression) for a user after the front wheel suspension assembly 12 is compressed.


The indicator 16 comprises the first retention feature 134, which in the illustrated embodiment is a plurality of protrusions projecting inward into a center opening of the indicator, the pointer 130, which in the illustrated embodiment is a ledge that projects outward from a face of the indicator 16, and a stop member 128, which in the illustrated embodiment is a shoulder that is formed along an outer edge of the indicator 16. The stop member 28 forms a stop or buttress that cooperates with the actuator 126 during suspension assembly compression. The first interference member 134 is sized and shaped to cooperate with the second interference member 140, the protrusions seating within the channel of the second interference member 140. The seating of the first interference member 134 in the second interference member 140 allows rotation of the first interference member 134 relative to the second interference member 140 when sufficient force is applied to overcome the rotational friction between the first interference member 134 and the second interference member 140, which allows rotation of the indicator 16 relative to the bolt 2 (and thus relative to the scale 18) when force is applied to the indicator 16. The frictional interaction between the first interference member 134 and the second interference member 140 also provides enough resistance to hold the indicator 16 in place relative to the bolt 2 (and thus relative to the scale 18) when not being acted upon by outside forces.


The central aperture 165 of the indicator 16 has a center point that is coincident with a central axis of the pivot assembly 20. The pointer 130 is generally linear in shape and when viewed on the face of the indicator 16 forms a chord, intersecting the outer circumference of the indicator at two locations without passing through the center. In other embodiments, the indicator may or may not intersect the outer circumference of the indicator 16. The pointer 130 is offset a distance from the center point of the indicator 16, when viewed face-on. This offset distance 44 allows the user to easily and accurately read the suspension travel.


The link 122 rotates in an arc 164 about the central axis of the pivot assembly 20 during suspension travel (e.g., compression). As illustrated in FIG. 11A, the indicator 16 is in a resting position where the actuator 126 and stop member 128 are in contact at 146. The contact at 146 between the actuator 126 and stop member 128 is illustrated with a dashed circle in FIG. 11A. The link 122 has a first link axis 160 that is defined by a line that passes through the rotational axes of the pivot assemblies 20 in the link 122. The pointer 130 has a first indicator direction 170 that is defined by a line that passes through the center of the pointer 30 when being viewed in a direction axial to the central axis of the pivot assembly 20 (e.g., face-on to the indicator 16).


As illustrated in FIG. 11B, as the front wheel suspension assembly 12 compresses, the link 122 rotates in the arc 164. As the link 122 rotates, the actuator 126 remains engaged with the stop member 128 and the actuator 126 pushes the stop member 128 in the direction of rotation (counterclockwise in FIGS. 11A-11C) because the actuator 126 is rotating with the link 122. The pointer 130 rotates as the link 122 rotates due to the interaction between the actuator 126 and the stop member 128 described above. The maximum angular displacement 167 of the pointer 130 is equal to the maximum angular displacement 164 of the link 122. Thus, as the link 122 rotates, the contact at 146 between the actuator 126 and the stop member 128 causes the indicator 16 and thus the pointer 30 to rotate in relation to the pivot assembly 20, more specifically relative to the bolt 2.


As illustrated in FIG. 11C after the front wheel suspension 12 is compressed, it returns to an uncompressed state where the link 122 rotates back to its original position when the cycle suspension is at full extension. Because the actuator 126 moves in a direction away from the stop member 128 (e.g., in the clockwise direction in FIGS. 11A-11C) during extension of the front wheel suspension assembly 12, the actuator 126 separates from the stop member 128 and there is no longer a force significant enough to produce relative movement between the indicator 16 and the bolt 2. More specifically, the friction produced by the protrusion 134 on the indicator and the channel 140 on the bolt 2 is sufficient to prevent any further relative movement between the indicator 16 and the bolt 2. The separation 148 between the actuator 126 and stop member 128 is illustrated with a dashed oval in FIG. 11C. When the link 122 returns to its original (uncompressed) position, the angular relationship between the first link axis 160 and indicator alignment 172 is different than the angular relationship between the first link axis 160 and indicator direction 170 prior to suspension displacement (FIG. 11A) and as explained in further detail herein is reflective of the travel distance measurement that occurred during displacement. As the link 122 returns to its uncompressed original position, the scale 18 rotates (clockwise in FIGS. 11A-11C) with the link 122, thus changing a relative position between the scale 18 and the pointer 130. With the suspension fully extended, the user can view the pointer 130 and the scale 18, which indicates the amount of suspension travel that occurred during the compression event of the suspension assembly. For example, in the embodiment illustrated in FIGS. 11A-11C, the pointer indicates that 20% of suspension travel has been used during prior suspension displacements, as indicated by the pointer 130 being aligned with the 20% mark on the scale 18.


Turning now to FIG. 12, in one embodiment, the pivot assembly 20 includes various subcomponents that are arranged to connect links 122 to each other or to connect a link to a frame member, such as the fork arm 24. The pivot assembly 20 includes a pivot body 4 and a bolt 2. The bolt 2 can form a cap 232 of the pivot assembly 20. The second retention feature 140 may be formed on one or both of the pivot body 4 and the bolt 2. In certain embodiments the pivot body 4 may include a slot 236 that can be used for purposes other than interfacing with an indicator. The cap 232 may be removably joined to the pivot body 4 by a threaded connection located at an end of the pivot body 4. The bolt 2 can likewise include a threaded connection such that when connected to the pivot body 4 by the threaded connection, an axial clamping force is produced. In other embodiments the pivot body 4 may include threads at both ends which can connect to bolts 2 at each end, such that when assembled to a pivot body 4 by threading, the cap 232 of the first bolt 2, and the cap 232 of the second bolt 2 produce an axial clamping force. The pivot body 4 and the bolt 2 can include one or more tool interfaces that can be used to connect with a tool to provide a means of rotating the pivot body 4 and/or the bolt 2 during assembly.


In alternate embodiments, threads can be either internal or external on the pivot body 4 or on the bolt 2. In other embodiments, the slot 236 can be fully formed about the diameter of the pivot body 4, or formed as a partial slot 236. In yet other embodiments, the slot 236 may be formed in the bolt 2.


As illustrated in the figures, the first and second retention features 134, 140 provide a captured mounting mechanism for the indicator 16, which locates the indicator 16 axially on the bolt 2 while allowing rotational movement between the indicator 16 and the bolt 2 when sufficient force is applied to overcome rotational friction. In certain embodiments, the first retention feature 134 may be any one or more of a tab, a slot, a bump, a hole, a protrusion, a depression, a boss, a flap, or any other type of feature that can mate or interface with a corresponding second retention feature 140. In certain embodiments, the second retention feature 140 may be any one or more of a tab, a slot, a bump, a hole, a protrusion, a depression, a boss, a flap, or any other type of feature that can mate or interface with a corresponding first retention feature 34. Interference features 134, 140 may cooperate with other surfaces or other parts such as the pivot bodies 4, the bolts 2, the links 122, and/or the frame members to allow rotation of the indicator 16 and at the same time allow for enough rotational interference friction that the indicator 16 can be rotated back to an original position by the actuator 126 or by a human finger if registration of a new travel displacement measurement is desired, and also allow for enough rotational interference friction to hold the indicator 16 in place when not being acted upon outside forces, such as the actuator 126 or the human finger, such that a prior travel displacement measurement can be observed and registered.


In certain embodiments, the actuator 126 may be any one or more of a tab, a slot, a bump, a hole, a protrusion, a depression, a boss, a flap, or any other type of feature that can mate or interface with the stop member 128. In certain embodiments, the stop member 128 may be any one or more of a tab, a slot, a bump, a hole, a protrusion, a depression, a boss, a flap, or any other type of feature that can mate or interface with the actuator 126. The actuator 126 and the stop member 128 may cooperate with other surfaces or other parts such as the pivots bodies 4, the bolts 2, the links 122, and/or the frame members to cause rotation of the indicator 16 when there is contact 146 between the actuator 126 and stop member 128.


Turning now to FIGS. 13 and 14, another embodiment of a front wheel suspension assembly 312 is illustrated. Any feature discussed above with respect to FIGS. 1-12 may be included in the embodiment of FIGS. 13 and 14, even if not illustrated. Likewise, any feature of the embodiment of FIGS. 13 and 14 may be included in the embodiment of FIGS. 1-12, even if not illustrated.


Similar to the embodiment of FIG. 2, the front wheel suspension assembly 312 includes a fork arm 324, a shock link 350, a wheel carrier 360, and a control link 370. The links are pivotably connected by pivots 320, as discussed above. The rotation sensor (not illustrated in FIGS. 13 and 14) may be connected to the front wheel suspension assembly 312, for example, at one of the pivots 320. The fork arm 324 may include one or more adjustment levers or ports for adjusting the setup (or ride characteristics) of the front wheel suspension assembly 312. For example, an adjustment lever 390 may be used to change the volume of the gas spring (for example by moving a piston within the gas chamber), which changes the gas volume or gas pressure within the gas chamber. A gas port 392 may be located on the fork arm 324, and allows access to a valve that is fluidly connected with the gas chamber, to allow addition or subtraction of gas molecules from the gas chamber, which thereby changes the gas pressure within the gas chamber.


Turning now to FIG. 15, a logic diagram 400 is illustrated for a method of using rotational data from the rotation sensor to adjust a setup of a front wheel suspension assembly. Sensed measurements from the rotation sensor may be used to adjust and/or modify riding characteristics of the front wheel suspension assembly. A first angular relationship between a first link and a second link may be measured by the rotation sensor 101 when the front wheel suspension assembly is in an uncompressed state at 410. The first angular relationship is output to the processor 102 at 420. The front wheel suspension assembly 312 is moved into a partially compressed state at 430. Partially compressed state, as used herein, means any state of compression other than completely uncompressed. A partially compressed state includes full compression. A second angular relationship between the first link and the second link is measured by the rotation sensor 101 in the partially compressed state at 440. The second angular relationship is output to the processor 102 at 450. The processor calculates a difference between the first angular relationship and the second angular relationship at 460 to determine a setpoint value for a component of the front wheel suspension assembly 312. In one embodiment, the component is the gas spring of the shock absorber and the setpoint value is a gas pressure in the gas chamber. In another embodiment, the component is the damper in the shock absorber and the setpoint value is a size of the opening in the damper piston. Optionally, the setpoint value from the processor may be output to a display. Finally, the component is adjusted based on the setpoint value at 470.


The step 470 of adjusting the component may include changing a characteristic of a shock absorber, a damper, or a combination of a shock absorber and a damper, based on the setpoint value. The characteristic may be a fluid flow rate through the opening in the damper piston, which requires changing a size of the opening based on the setpoint value. In other embodiments, the step of adjusting the component may include changing a characteristic of one of a gas spring or a coil spring. More specifically, the spring constant of the gas or coil spring may be changed by changing the gas pressure in the gas spring, or by changing a spring force produced by a coil spring. The spring force may be changed by changing a spring constant. In the gas spring, the spring constant may be changed by varying gas pressure in the gas spring and/or by changing a gas volume of the gas spring.


By changing a component characteristic of the front wheel suspension assembly based on angular measurements taken by a rotation sensor, a user can quickly and accurately change the setup of the front wheel suspension assembly to suit his or her needs.


The rotation sensor may be connected to any pivot, fixed or floating, or any link in the suspension assembly. Additionally, in other embodiments, the rotation sensor may be one of a magnetic sensor, an optical sensor, an electrical sensor, an accelerometer, a potentiometer, or a resistive sensor. In other embodiments, the rotation sensor may be one of an optical reflective sensor or an optical interrupter sensor. In yet other embodiments, the rotation sensor may be one of a variable reluctance sensor, an eddy current killed oscillator sensor, a Wiegand sensor, or a Hall effect sensor.


Elements in the figures are illustrated for simplicity and clarity and have not necessarily been drawn to scale. For example, the dimensions and/or relative positioning of some of the elements in the figures may be exaggerated relative to other elements to help to improve understanding of various embodiments of the present invention. Also, common but well-understood elements that are useful or necessary in a commercially feasible embodiment are often not depicted in order to facilitate a less obstructed view of these various embodiments. The same reference numbers may be used to describe like or similar parts. Further, while several examples have been disclosed herein, any features from any examples may be combined with or replaced by other features from other examples. Moreover, while several examples have been disclosed herein, changes may be made to the disclosed examples within departing from the scope of the claims.


A variety of modifications, alterations, and combinations can be made with respect to the above described embodiments without departing from the scope of the invention, and that such modifications, alterations, and combinations are to be viewed as being within the scope of the inventive concept.

Claims
  • 1. A suspension assembly for a cycle, the suspension assembly comprising: a first link having a first pivot;a second link movably connected to the first link by the first pivot; anda rotation sensor operably connected to the first pivot at the first pivot,wherein the rotation sensor measures angular displacement of the first pivot that directly corresponds to angular displacement between the first link and the second link, andwherein the rotation sensor is one of a variable reluctance sensor, an eddy current killed oscillator sensor, a Wiegand sensor, or a Hall effect sensor.
  • 2. The suspension assembly of claim 1, further comprising a shock absorber operably connected to one of the first link or the second link.
  • 3. The suspension assembly of claim 1, wherein the first pivot is a fixed pivot.
  • 4. The suspension assembly of claim 1, wherein the first pivot is a floating pivot.
  • 5. The suspension assembly of claim 1, wherein the first link is a fork arm.
  • 6. The suspension assembly of claim 1, wherein the first link is one link in a front wheel cycle suspension assembly.
  • 7. The suspension assembly of claim 1, wherein the rotation sensor comprises a Hall effect sensor.
  • 8. The suspension assembly of claim 1, wherein the first link is a frame member.
  • 9. The suspension assembly of claim 1, wherein the first pivot is part of a front wheel suspension assembly.
  • 10. The suspension assembly of claim 1, wherein the first pivot is part of a rear wheel suspension assembly.
  • 11. A suspension assembly for a cycle, the suspension assembly comprising: a first link having a first pivot;a second link movably connected to the first link by the first pivot; anda rotation sensor operably connected to the first pivot at the first pivot,wherein the rotation sensor measures angular displacement of the first pivot that directly corresponds to angular displacement between the first link and the second link, andwherein the rotation sensor comprises a Hall effect sensor.
  • 12. The suspension assembly of claim 11, wherein the first pivot is a fixed pivot.
  • 13. The suspension assembly of claim 11, wherein the first pivot is a floating pivot.
  • 14. The suspension assembly of claim 11, wherein the first link is a fork arm.
  • 15. The suspension assembly of claim 11, wherein the first link is one link in a front wheel cycle suspension assembly.
  • 16. The suspension assembly of claim 11, wherein the first link is a frame member.
  • 17. The suspension assembly of claim 11, wherein the first pivot is part of a front wheel suspension assembly.
  • 18. The suspension assembly of claim 11, wherein the first pivot is part of a rear wheel suspension assembly.
  • 19. A suspension assembly for a cycle, the suspension assembly comprising: a first link having a first pivot;a second link movably connected to the first link by the first pivot; anda rotation sensor operably connected to the first pivot at the first pivot,wherein the rotation sensor measures angular displacement of the first pivot that directly corresponds to angular displacement between the first link and the second link, andwherein the first pivot is a floating pivot.
  • 20. The suspension assembly of claim 19, wherein the rotation sensor comprises one of a magnetic sensor, an optical sensor, an electrical sensor, an accelerometer, a potentiometer, or a resistive sensor.
  • 21. The suspension assembly of claim 19, wherein the rotation sensor is one of an optical reflective sensor or an optical interrupter sensor.
  • 22. The suspension assembly of claim 19, wherein the rotation sensor is one of a variable reluctance sensor, an eddy current killed oscillator sensor, a Wiegand sensor, or a Hall effect sensor.
  • 23. A suspension assembly for a cycle, the suspension assembly comprising: a first link having a first pivot;a second link movably connected to the first link by the first pivot; anda rotation sensor operably connected to the first pivot at the first pivot,wherein the rotation sensor measures angular displacement of the first pivot that directly corresponds to angular displacement between the first link and the second link, andwherein the rotation sensor is one of an optical reflective sensor or an optical interrupter sensor.
US Referenced Citations (424)
Number Name Date Kind
389200 Clegg Sep 1888 A
393387 Norton Nov 1888 A
400727 Baudreau Apr 1889 A
412322 Copeland Oct 1889 A
414048 Hunter Oct 1889 A
423471 Easthope Mar 1890 A
426402 Torkelson Apr 1890 A
435477 Blackledge Sep 1890 A
441649 Dunlop Dec 1890 A
443266 Bell Dec 1890 A
444639 O'Neill Jan 1891 A
447234 Donnelly Feb 1891 A
467794 Ellis Jan 1892 A
468643 Clement Feb 1892 A
524389 La Casse Aug 1894 A
602354 Ohlgart Apr 1898 A
638723 Kelly Dec 1899 A
739476 Becker Sep 1903 A
783236 Ashburn Feb 1905 A
848324 Sager Mar 1907 A
913961 Levedahl Mar 1909 A
927989 Meiser Jul 1909 A
940245 Gates Nov 1909 A
946143 Levedahl Jan 1910 A
953697 Kuebodeaux Apr 1910 A
973071 Redmond Oct 1910 A
979674 Kittle et al. Dec 1910 A
980999 Pommer Jan 1911 A
989638 Pilgrm Apr 1911 A
1000115 Oquist Aug 1911 A
1036263 Kittle Aug 1912 A
1042480 Ridgway Oct 1912 A
1077105 Stewart Oct 1913 A
1096417 Ekstrom May 1914 A
1101614 Bramham Jun 1914 A
1132829 Cobb Mar 1915 A
1144753 Budroe Jun 1915 A
1166156 Shimmin Dec 1915 A
1189874 Schickel Jul 1916 A
1203927 Stagni Nov 1916 A
1213995 Anderson Jan 1917 A
1223572 Drew Apr 1917 A
1227634 Lake May 1917 A
1251992 Drew Jan 1918 A
1254798 Harley Jan 1918 A
1273179 Perry et al. Jul 1918 A
1298958 Johnston Apr 1919 A
1333449 Russell Mar 1920 A
1365524 Mellantine Jan 1921 A
1397850 Yoxall et al. Nov 1921 A
1432376 Wolff Oct 1922 A
1452436 Pullin Apr 1923 A
1475044 Bloom Nov 1923 A
1517146 Bloom Nov 1924 A
1527133 Harley Feb 1925 A
1605680 Merkel Nov 1926 A
1834308 Harley Dec 1931 A
1924363 Kanai Aug 1933 A
1924586 Zerk Aug 1933 A
1999394 Burnett Apr 1935 A
2038011 Spiegler et al. Apr 1936 A
2063704 Slack Dec 1936 A
2073736 Duffy Mar 1937 A
2087299 Pribil Jul 1937 A
2160034 Schwinn May 1939 A
2170565 Macbeth Aug 1939 A
2203342 Sloman Jun 1940 A
2233313 Hazelroth Feb 1941 A
2271304 Mulholland Jan 1942 A
2376788 Latscher-Latka May 1945 A
2462711 Barnett Feb 1949 A
2463310 Probst Mar 1949 A
2464326 MacGregor Mar 1949 A
2475774 Benson Jul 1949 A
2485484 Dean Oct 1949 A
2486430 Moore Nov 1949 A
2489821 Ryder Nov 1949 A
2504452 Rostan Apr 1950 A
2525171 Franks Oct 1950 A
2537679 Kraeft Jan 1951 A
2540585 Kranz Feb 1951 A
2543991 Schuricht Mar 1951 A
2550876 Spencer May 1951 A
2561156 Thorkildsen Jul 1951 A
2588889 Sherwood Mar 1952 A
2596411 Jordan May 1952 A
2636567 Landrum Apr 1953 A
2649312 Miller Aug 1953 A
2660455 Douglas et al. Nov 1953 A
2664644 Tyerman Jan 1954 A
2708112 Seddon et al. May 1955 A
2729465 Torre Jan 1956 A
2751991 Mennesson Jun 1956 A
2752167 Propst et al. Jun 1956 A
2756070 Torre Jul 1956 A
2756832 Dalrymple Jul 1956 A
2855212 Houser Oct 1958 A
2918306 Lewandoski Dec 1959 A
2953395 Turner Sep 1960 A
2969992 Hahn Jan 1961 A
2976056 Henry Mar 1961 A
3083038 Moulton Mar 1963 A
3133748 Gunnerson May 1964 A
3188072 Wustenhagen et al. Jun 1965 A
3433318 Packard Mar 1969 A
3673608 Voorman, Jr. Jun 1972 A
3694004 Siebers Sep 1972 A
3701544 Stankovich Oct 1972 A
2303568 McWhorter et al. Dec 1972 A
3730553 Harman May 1973 A
3774935 Aldrich Nov 1973 A
3942821 Bock Mar 1976 A
3944254 Inui Mar 1976 A
3954284 Phillips et al. May 1976 A
3989261 Kawaguchi Nov 1976 A
4030641 Bailey et al. Jun 1977 A
4057264 Suzuki et al. Nov 1977 A
4058903 Wilkerson Nov 1977 A
4147371 Morita et al. Apr 1979 A
4153237 Supalla May 1979 A
4159123 Petty Jun 1979 A
4162797 McBride Jul 1979 A
4170369 Strutman Oct 1979 A
4179135 Slater Dec 1979 A
4180280 Doveri Dec 1979 A
4184695 Roe et al. Jan 1980 A
4186936 Offenstadt et al. Feb 1980 A
4189168 Courtney Feb 1980 A
4212481 Ribi Jul 1980 A
4242481 Fannin Dec 1980 A
4265329 de Cortanze May 1981 A
4268055 Bell May 1981 A
4295658 Kashima Oct 1981 A
4367882 Alexander et al. Jan 1983 A
4388978 Fior Jun 1983 A
4401316 Miyakoshi et al. Aug 1983 A
4406475 Miyakoshi et al. Sep 1983 A
4408399 Darwood et al. Oct 1983 A
4410196 Ribi Oct 1983 A
4421337 Pratt Dec 1983 A
4422662 Inoue et al. Dec 1983 A
4433850 Miyakoshi et al. Feb 1984 A
4433851 Miyakoshi et al. Feb 1984 A
4437678 Schultz Mar 1984 A
4438909 Matsumoto Mar 1984 A
4444406 Isono Apr 1984 A
4455032 Kajikawa Jun 1984 A
4480711 Satoh et al. Nov 1984 A
4482264 Kodera Nov 1984 A
4520892 Satoh Jun 1985 A
4526249 Parker Jul 1985 A
4531755 Isono et al. Jul 1985 A
4533153 Tsunoda et al. Aug 1985 A
4540190 Moulton Sep 1985 A
4542910 Watanabe Sep 1985 A
4561669 Simons Dec 1985 A
4570963 Isono Feb 1986 A
4572534 Heyl Feb 1986 A
4576393 Moulton et al. Mar 1986 A
4585245 Rose Apr 1986 A
4616810 Richardson et al. Oct 1986 A
4625985 Nakano et al. Dec 1986 A
4629205 Haynes Dec 1986 A
4650027 de Cortanze Mar 1987 A
4660683 Hayashi et al. Apr 1987 A
4685694 Kouyama Aug 1987 A
4702338 Trema Oct 1987 A
4703839 Yasuo et al. Nov 1987 A
4723621 Kawano et al. Feb 1988 A
4732241 Yoshida Mar 1988 A
4738468 Baron Apr 1988 A
4741545 Honma et al. May 1988 A
4742884 Ishikawa May 1988 A
4744434 Miyakoshi et al. May 1988 A
4770434 Pietro et al. Sep 1988 A
4775163 McGowan et al. Oct 1988 A
4776609 Pan et al. Oct 1988 A
4789174 Lawwill Dec 1988 A
4807898 Huntly Feb 1989 A
4809802 Seino et al. Mar 1989 A
4815763 Hartmann Mar 1989 A
4828069 Hatsuyama May 1989 A
4834412 Trema May 1989 A
4878558 Asakura Nov 1989 A
4881750 Hartmann Nov 1989 A
4890857 de Cortanze Jan 1990 A
4971344 Turner Nov 1990 A
4993734 Trema Feb 1991 A
4997197 Shultz Mar 1991 A
5009451 Hayashi et al. Apr 1991 A
5042608 Horiike et al. Aug 1991 A
5050699 Savard Sep 1991 A
5064212 Yun Nov 1991 A
5069303 Fuller Dec 1991 A
5069467 Claudio Dec 1991 A
5088705 Tsai Feb 1992 A
5133223 Morri Jul 1992 A
5156231 Trema Oct 1992 A
5186481 Turner Feb 1993 A
5193832 Wilson et al. Mar 1993 A
5193833 Reisinger Mar 1993 A
5195766 Dohrmann et al. Mar 1993 A
5219211 Tsuchida et al. Jun 1993 A
5248159 Moore Sep 1993 A
5249650 Tanaka Oct 1993 A
5269549 Wilson et al. Dec 1993 A
5284352 Chen Feb 1994 A
5299820 Lawwill Apr 1994 A
5308099 Browning May 1994 A
5310203 Chen May 1994 A
5320374 Farris et al. Jun 1994 A
5328196 Ohma Jul 1994 A
5350185 Robinson Sep 1994 A
5354085 Gally Oct 1994 A
5359910 Chang et al. Nov 1994 A
5361864 Tanaka Nov 1994 A
5380026 Robinson Jan 1995 A
5403028 Trimble Apr 1995 A
5405159 Klein et al. Apr 1995 A
5409248 Williams Apr 1995 A
5413368 Pong et al. May 1995 A
5417446 Pileggi May 1995 A
5427208 Motobu et al. Jun 1995 A
5427397 Chonan Jun 1995 A
5429380 Lawwill Jul 1995 A
5431426 Ijams et al. Jul 1995 A
5441291 Girvin, III Aug 1995 A
5449155 Mack Sep 1995 A
5456480 Turner et al. Oct 1995 A
5462302 Leitner Oct 1995 A
5474318 Castellano Dec 1995 A
5487223 Krane Jan 1996 A
D368054 Behrens et al. Mar 1996 S
5498013 Hwang Mar 1996 A
5509674 Browning Apr 1996 A
5509676 Fukuake et al. Apr 1996 A
5564534 Toyoda et al. Oct 1996 A
5599034 Brigden Feb 1997 A
5615756 Grundei et al. Apr 1997 A
5709399 Smith, Jr. Jan 1998 A
5720473 Thomas Feb 1998 A
5743547 Voss et al. Apr 1998 A
5743574 Kohn Apr 1998 A
5749590 Roerig May 1998 A
5782313 Kurawaki et al. Jul 1998 A
5799963 Berkmann Sep 1998 A
5810102 Stewart Sep 1998 A
5813684 Baron Sep 1998 A
5829773 Rajaee Nov 1998 A
5855388 Brewer Jan 1999 A
5899478 Woodside May 1999 A
5908200 Stewart Jun 1999 A
5927741 Chi Jul 1999 A
5931487 Koppelberg et al. Aug 1999 A
5931489 Damman et al. Aug 1999 A
5951033 Winter et al. Sep 1999 A
6017047 Hoose Jan 2000 A
6036211 Nohr Mar 2000 A
6047981 Burrows Apr 2000 A
6089585 Theobald Jul 2000 A
6149173 Bynoe Nov 2000 A
6152472 Woodside Nov 2000 A
6155370 Iwai et al. Dec 2000 A
6161858 Tseng Dec 2000 A
6164424 Girvin et al. Dec 2000 A
6164675 Pickering Dec 2000 A
6199885 Seidl Mar 2001 B1
6241391 Hoose Jun 2001 B1
6244609 Wilson Jun 2001 B1
6260869 Hanlon et al. Jul 2001 B1
6260870 Fan Jul 2001 B1
6263994 Eitel Jul 2001 B1
6311961 Julia Nov 2001 B1
6336647 Iwai et al. Jan 2002 B1
6357775 Iwai et al. Mar 2002 B1
6371263 Hoose Apr 2002 B1
6382374 Iwai et al. May 2002 B1
6386567 Schonfeld May 2002 B1
6402175 Jansson Jun 2002 B1
6457732 Ito et al. Oct 2002 B2
6485043 Ito et al. Nov 2002 B2
6488300 Ito et al. Dec 2002 B2
6517095 Lansac et al. Feb 2003 B1
6517096 Yih Feb 2003 B2
6533305 Falk Mar 2003 B1
6783140 Huang Aug 2004 B1
6789810 Strong Sep 2004 B2
6896276 Sparrow May 2005 B1
6908092 Kofuji et al. Jun 2005 B2
6910702 Hals Jun 2005 B1
6918605 Wada et al. Jul 2005 B2
6994365 Kofuji Feb 2006 B2
7011325 Kinzler et al. Mar 2006 B2
7047831 Reynolds et al. May 2006 B2
7140627 Wimmer Nov 2006 B2
7159883 Mydiarz Jan 2007 B2
7210695 Griffiths May 2007 B2
7331594 Wimmer Feb 2008 B2
7350787 Voss Apr 2008 B2
7364178 Wimmer Apr 2008 B2
7425008 Pokrywka Sep 2008 B2
7425009 Namazue et al. Sep 2008 B2
7434823 Robinson et al. Oct 2008 B2
7441622 Costa Oct 2008 B2
7635141 O'Connor Dec 2009 B2
7699330 Chen Apr 2010 B2
7708296 Becker et al. May 2010 B2
7744107 Chen Jun 2010 B2
7887077 Thiers Feb 2011 B2
7896379 Nagao et al. Mar 2011 B2
8333528 Oertley et al. Dec 2012 B2
8448970 Vardon May 2013 B1
8534692 Trebichavsky Sep 2013 B2
8939458 Nesbitt, III Jan 2015 B2
9194456 Laird et al. Nov 2015 B2
9248883 D'Aluisio Feb 2016 B2
9278598 Galasso et al. Mar 2016 B2
9592838 Mecklenburg et al. Mar 2017 B1
9682741 Fioravanzo et al. Jun 2017 B2
9707817 Arnott et al. Jul 2017 B1
9724701 Harney et al. Aug 2017 B2
10053166 Moriguchi Aug 2018 B2
10094683 Przykucki et al. Oct 2018 B1
10099743 Walthert et al. Oct 2018 B2
10196106 Weagle Feb 2019 B1
10300979 Weagle May 2019 B2
10308312 Weagle Jun 2019 B2
D859125 Weagle et al. Sep 2019 S
D860061 Weagle et al. Sep 2019 S
D860062 Weagle Sep 2019 S
D861542 Weagle Oct 2019 S
10518836 Weagle Dec 2019 B2
10518839 Weagle Dec 2019 B2
10526039 Weagle Jan 2020 B2
10526040 Weagle Jan 2020 B2
10537790 Galasso et al. Jan 2020 B2
10549812 Weagle Feb 2020 B2
10549813 Weagle Feb 2020 B2
10549815 Weagle Feb 2020 B2
D880369 Weagle Apr 2020 S
D880370 Weagle Apr 2020 S
D880371 Weagle Apr 2020 S
D880372 Weagle Apr 2020 S
10689061 Weagle Jun 2020 B2
10894572 Przykucki et al. Jan 2021 B2
10906601 Aoki et al. Feb 2021 B2
11084552 Weagle Aug 2021 B2
11117635 Przykucki, Jr. et al. Sep 2021 B2
11208172 Weagle Dec 2021 B2
11230346 Weagle Jan 2022 B2
11230347 Weagle Jan 2022 B2
11230348 Weagle Jan 2022 B2
11273887 Weagle Mar 2022 B2
11345432 Weagle May 2022 B2
11524744 Weagle Dec 2022 B2
11945539 Weagle Apr 2024 B2
20010019197 Ito et al. Sep 2001 A1
20020005066 Tanner et al. Jan 2002 A1
20020079670 Yih Jun 2002 A1
20020084619 Odom Jul 2002 A1
20040036250 Kofuji Feb 2004 A1
20050248119 Callahan et al. Nov 2005 A1
20080023934 van Houweling Jan 2008 A1
20080041681 Shipman Feb 2008 A1
20080060863 Iizuka Mar 2008 A1
20080258424 Paul Oct 2008 A1
20080277848 Davis Nov 2008 A1
20080296863 Heyl et al. Dec 2008 A1
20080303242 O'Connor Dec 2008 A1
20090001684 McAndrews et al. Jan 2009 A1
20090033009 Kirchner et al. Feb 2009 A1
20090266656 Murakami Oct 2009 A1
20100010709 Song Jan 2010 A1
20100244340 Wootten et al. Sep 2010 A1
20110012321 Chen Jan 2011 A1
20110083930 Laird et al. Apr 2011 A1
20110093930 Bartel-Kurz et al. Apr 2011 A1
20110156728 Sato et al. Jun 2011 A1
20110313568 Blackwell Dec 2011 A1
20120228850 Tseng Sep 2012 A1
20120248666 Debruler et al. Oct 2012 A1
20140061987 DeBruler et al. Mar 2014 A1
20140202809 Ozaki et al. Jul 2014 A1
20140316652 Ericksen et al. Oct 2014 A1
20150183440 Jackson Jul 2015 A1
20150317065 Meriaz et al. Nov 2015 A1
20150375823 Fioravanzo et al. Dec 2015 A1
20160288867 Murakami Oct 2016 A1
20160339987 Walthert et al. Nov 2016 A1
20160339989 Walthert et al. Nov 2016 A1
20170043818 Moriguchi Feb 2017 A1
20170087932 Winshtein et al. Mar 2017 A1
20170198779 Batsch et al. Jul 2017 A1
20170219041 Debruler et al. Aug 2017 A1
20170284493 Smith Oct 2017 A1
20180281878 Aoki et al. Oct 2018 A1
20180297435 Brady et al. Oct 2018 A1
20180304952 Krugman et al. Oct 2018 A1
20180334219 Walthert et al. Nov 2018 A1
20190031275 Weagle Jan 2019 A1
20190031276 Weagle Jan 2019 A1
20190031277 Weagle Jan 2019 A1
20190039681 Weagle Feb 2019 A1
20190047657 Weagle Feb 2019 A1
20190047658 Weagle Feb 2019 A1
20190061865 Weagle Feb 2019 A1
20190061866 Weagle Feb 2019 A1
20190061867 Weagle Feb 2019 A1
20190061868 Weagle Feb 2019 A1
20190092116 Magnus et al. Mar 2019 A1
20190168838 Weagle Jun 2019 A1
20200079462 Weagle Mar 2020 A1
20200079463 Weagle Mar 2020 A1
20200094908 Weagle Mar 2020 A1
20200094910 Weagle Mar 2020 A1
20200354012 Pelot Nov 2020 A1
20210323632 Weagle Oct 2021 A1
20210323633 Weagle Oct 2021 A1
20220097792 Przykucki, Jr. et al. Mar 2022 A1
20220153381 Zawistowski et al. May 2022 A1
20220204123 Weagle Jun 2022 A1
20220363335 Weagle Nov 2022 A1
20220363336 Weagle Nov 2022 A1
20230023390 Weagle Jan 2023 A1
Foreign Referenced Citations (130)
Number Date Country
507753 Dec 1951 BE
474575 Jun 1951 CA
63758 Feb 1914 CH
1309053 Aug 2001 CN
2846274 Dec 2006 CN
201198348 Feb 2009 CN
302966622 Oct 2014 CN
303438302 Nov 2015 CN
303584666 Feb 2016 CN
303604532 Mar 2016 CN
304240449 Aug 2017 CN
304327156 Oct 2017 CN
1084599 Jun 1960 DE
1122392 Jan 1962 DE
3133576 May 1983 DE
3223728 Dec 1983 DE
8906328 Nov 1989 DE
3833880 Apr 1990 DE
4119339 Jan 1992 DE
9404873 May 1994 DE
9403640 Jun 1994 DE
9414705 Feb 1995 DE
19503047 Aug 1996 DE
19635939 Jun 1997 DE
19633692 Feb 1998 DE
102013004788 Sep 2013 DE
49600 Dec 1934 DK
0032170 Feb 1986 EP
0030306 Apr 1986 EP
0125244 Jan 1987 EP
0399615 Nov 1990 EP
0336891 Jul 1992 EP
420610 Feb 1996 EP
726198 Aug 1996 EP
0744562 Nov 1996 EP
0731017 Oct 1997 EP
0941916 Sep 1999 EP
0992374 Apr 2000 EP
1049618 Sep 2003 EP
728093 Nov 2005 EP
02000398 Dec 2008 EP
01884455 Apr 2009 EP
2096024 Sep 2009 EP
2100807 Sep 2009 EP
2357098 Aug 2011 EP
02001733 Dec 2012 EP
2483141 Nov 2013 EP
02913257 Sep 2015 EP
347724 Mar 1905 FR
353990 Sep 1905 FR
350269 Dec 1905 FR
376759 Aug 1907 FR
467213 Jun 1914 FR
547006 Nov 1922 FR
559088 Sep 1923 FR
28240 Jan 1925 FR
636211 Apr 1928 FR
902973 Sep 1945 FR
972653 Feb 1951 FR
1030006 Jun 1953 FR
1032268 Jun 1953 FR
1059922 Mar 1954 FR
1064265 May 1954 FR
1067221 Jun 1954 FR
1082316 Dec 1954 FR
2418742 Sep 1979 FR
2494208 May 1982 FR
2687976 Sep 1993 FR
3004415 Oct 2014 FR
166065 Jul 1921 GB
223638 Oct 1924 GB
238069 Aug 1925 GB
239848 Dec 1925 GB
258141 Sep 1926 GB
264003 Jan 1927 GB
279630 Nov 1927 GB
302026 Dec 1928 GB
322370 Dec 1929 GB
469697 Jul 1937 GB
585122 Jan 1947 GB
585904 Feb 1947 GB
586372 Mar 1947 GB
691551 May 1953 GB
717259 Oct 1954 GB
720093 Dec 1954 GB
824866 Dec 1959 GB
841523 Jul 1960 GB
1540824 Feb 1979 GB
1545403 May 1979 GB
2038736 Jul 1980 GB
2052407 Jan 1981 GB
2073680 Oct 1981 GB
2106843 Apr 1983 GB
S60-110588 Jun 1985 JP
S61-124683 Feb 1986 JP
S61-160380 Jul 1986 JP
S62-187608 Aug 1987 JP
63-112191 Jul 1988 JP
649887 Jan 1989 JP
1204884 Aug 1989 JP
5069875 Mar 1993 JP
05-020635 May 1993 JP
1999-091671 Apr 1999 JP
2000159170 Jun 2000 JP
2000159171 Jun 2000 JP
2000159177 Jun 2000 JP
2000159178 Jun 2000 JP
2000168666 Jun 2000 JP
10-2009-0117921 Nov 2009 KR
416920 Jan 2001 TW
484570 Apr 2002 TW
568054 Dec 2003 TW
596028 Jun 2004 TW
D111693 Jul 2006 TW
M335458 Jul 2008 TW
M354565 Apr 2009 TW
D140125 Apr 2011 TW
D149623 Oct 2012 TW
2017-22777 Jul 2017 TW
WO 198200445 Feb 1982 WO
WO 198400526 Feb 1984 WO
WO 198701670 Mar 1987 WO
WO 199523728 Sep 1995 WO
WO 199746443 Dec 1997 WO
WO 199910224 Mar 1999 WO
WO 2000013961 Mar 2000 WO
WO 2002038437 May 2002 WO
WO 2019046039 Mar 2019 WO
WO 2019046040 Mar 2019 WO
WO 2021066819 Apr 2021 WO
Non-Patent Literature Citations (7)
Entry
Anubi et al., “Variable stiffness suspension system”, Mechanical Sciences, vol. 4:139-151 (2013), www.mech-sci-net/4/139/2013.
Black and white photograph of Greeves trials machine, Applicant Admitted Prior Art, Applicant's internal files.
Black and white photograph of Scorpion motorcycle, Applicant Admitted Prior Art, Applicant's internal files.
Black and white photograph of Silencer motorcycle, Applicant Admitted Prior Art, Applicant's internal files.
Color photograph of a cotton TC-70 motorcycle, Applicant Admitted Prior Art, Applicant's internal files.
Color photograph of Armstrong bicycle, Applicant Admitted Prior Art, Applicant's Internal Files.
Color photograph of Armstrong motorcycle, Applicant Admitted Prior Art, Applicant's internal files.
Related Publications (1)
Number Date Country
20230271670 A1 Aug 2023 US
Continuations (1)
Number Date Country
Parent 16379386 Apr 2019 US
Child 18060721 US