PIEZOELECTRIC SHOCK ABSORBERS

Abstract: A shock absorber for a vehicle includes a fluid-filled cylinder having a closed end, a shaft extending partially into the cylinder, a valve attached to the first end of the shaft, and a power supply. The valve includes a valve piston and a bender. The valve piston includes at least one orifice extending therethrough. The bender is seated adjacent the orifice in the piston. The bender includes a piezoelectric material embedded therein. The piezoelectric material includes sides with conductive material disposed thereon. The power supply is attached to the conductive material across the piezoelectric material in the bender to apply a voltage across the piezoelectric material to change the stiffness of the bender. A sensor is also included for monitoring the displacement and velocity of the piston within the fluid-filled cylinder. The biasing force on the bender is changed on sensor readings according to predetermined logic sequence.

Description: PIEZOELECTRIC SHOCK ABSORBERS Field of the Invention The present invention relates to shock absorbers for vehicles, such as bicycles and motorcycles, and more particularly, to a dampener valve for a shock absorber to regulate the flow of damping fluid based on feedback regarding velocity and displacement of the shock absorber shaft relative to the shock absorber body. Background of the Invention Front and rear suspensions have improved the performance and comfort of mountain bicycles. Over rough terrain the suspension system can improve traction and handling by keeping the wheels on the ground. A rider can more easily maintain control at higher speeds and with less effort when the suspension absorbs some of the shock encountered when riding. Ideally the suspension should react well to both (1) low amplitude, high frequency bumps and (2) high amplitude, low frequency bumps. However, these can be competing requirements for the damping systems in conventional shock absorbers. Higher rebound damping is desirable for high amplitude, low frequency bumps than for low amplitude, high frequency bumps. With high frequency, low amplitude bumps, such as may be encountered on a washboard gravel fireroad, minimal damping may be preferable so the spring can quickly recover from a minor impact before the next is encountered. However, with a large bump (such as the size of a curb) increased rebound damping aids the rider by keeping the bike from forcefully springing back too quickly, causing loss of traction and control on the rebound. Compression damping will also stop the bike from bottoming out with large bumps and make for a smoother absorption of the bumps. Some current shock absorbers that include springs and dampeners allow the rider to adjust rebound and/or compression damping before a ride. Other air shock absorbers include an on/off switch to disable the shock absorber all together. However, such preadjustment is at best a compromise; the rider must select better damping in one scenario at the expense of the other. A typical off-road mountain bike ride will include small bumps, medium, and large bumps, as well as possibly jumps, drop-offs, and tight descending to ascending transitions. If the rider significantly reduces the damping to ride smoothly over high frequency, low amplitude bumps then the bike may lose traction and control when a large bump is encountered or may "bottom out" the shock absorber. If the rider increases the damping force of the shock absorber, then the system will not recover fast enough to quickly absorb high frequency bumps, the rider will be rattled, and the bike will lose traction. Another limitation of current shock absorbers is evidenced by rider-induced bobbing: suspension movement caused by rider movement during pedaling. Related to this is pedal-induced suspension action: the cyclic forces on the chain pulling the rear swingarm up or down relative to the frame. If the damping in the shock absorber is greater, these influences will not be felt as much by the rider. However, a stiff suspension, especially at the beginning of the stroke of the shock absorber, can decrease the ability of the suspension to absorb small bumps well. Attempts to overcome the current limitations in suspension systems have focused on swingarm linkages and pivot arrangements. At a significant cost, some amelioration of rider- or pedal-induced suspension action has resulted, but much less progress has been made on the dilemma of large and small bump absorption. Summary of the Invention The present invention addresses the suspension challenges of both high frequency/low amplitude and low frequency/high amplitude shock absorption while also reducing rider- and pedal-induced suspension action. The present invention can be applied to most suspension configurations as it addresses these challenges with a unique, active damping shock absorber. The shock absorber is soft over small bumps and stiffens when encountering large shocks after the shock travels to a certain extent. The shock absorber stiffens further under extreme shock to avoid harsh bottoming out. Rebound damping may also be tuned independent of compression damping. The shock absorber changes damping during compression and rebound according to the speed and displacement of the shaft assembly relative to the housing during the suspension action. The present invention includes a dampener for a shock absorber. The dampener preferably includes a fluid reservoir, a piston, a channel, and a valve. The fluid reservoir contains fluid for damping action of the shock absorber. The piston is disposed at least partially within the reservoir. The piston is forced at least partially through the reservoir under the force of a shock acting on the shock absorber. The channel is in fluid communication with the reservoir. Fluid flows through the channel during at least a portion of the stroke of the piston through the reservoir. The valve at least partially obstructs the channel. The valve includes a mechanism and control for changing the flow through the channel based on at least one of the velocity and position of the piston relative to the reservoir. In the preferred embodiment, the valve includes a bender. The bender moves to affect the flow of fluid through the channel. The bender preferably includes a response material embedded within at least a portion thereof. In one preferred aspect of the invention, the valve includes a flow restriction member and a diaphragm attached thereto. The bender is moveable to direct a secondary flow of fluid to a side of the diaphragm to move the diaphragm. The diaphragm moves the restriction member. A primary flow of fluid passes through the channel as controlled by the flow restriction member. In the preferred embodiment of the invention, the response material includes a piezoelectric material. The valve further includes a power supply connected to the piezoelectric material for biasing the bender to affect the flow through the channel. In one aspect of this embodiment, a sensor is provided to detect shock compression conditions. The sensor changes the biasing force of the bender for flow change when the sensor signals predetermined conditions. In one aspect of the invention, the flow restriction member is moveable generally transverse to the direction of fluid flow through a portion of the channel adjacent the restriction member. Preferably, the flow restriction member is connected to the bender with movement of the bender controlling the flow restriction member. In one aspect of the invention, the reservoir is contained by a housing. The channel extends through inflow and outflow openings or channels within the housing. Preferably, the inflow opening is located within the housing in a location to be at least partially blocked by the piston upon extensive movement or stroke of the piston within the reservoir or housing. Preferably, the outflow opening is located within the housing in a location to be at least partially blocked by the piston during the initial portion of the stroke of the piston. Thus, during extensive stroke of the piston within the reservoir the inflow opening or channel is at least partially blocked to increase the damping force. During the initial portion of the stroke of the piston, the outflow opening or channel is either at least partially blocked or opens to the first end of the piston whereas with further stroke of the piston within the reservoir, the outflow opening or channel transmits fluid to the second end of the piston during compression of the piston within the reservoir. In a further aspect of the present invention, a dampener is provided for a shock absorber including a stanchion tube. The dampener includes a fluid chamber defined at least partially within the stanchion tube and which contains a fluid. A piston is disposed within the fluid chamber for longitudinal movement within the fluid chamber under the force of a shock acting on the shock absorber, the piston having a first side and a second side. A bypass channel is provided in fluid communication with the fluid chamber on the first side of the piston and with the fluid chamber on the second side of the piston. The bypass channel permits fluid to bypass the piston while flowing from the first side of the piston to the second side of the piston. A valve is disposed within the stanchion tube and is operable to control the flow of fluid through the bypass channel. In a still further aspect of the present invention, a dampener is provided for a telescoping suspension strut of a vehicle having a ground engaging member, such as a wheel, and a frame. The dampener includes a stanchion tube having an end securable to the ground engaging member or the frame, and defining an internal fluid chamber. A piston assembly includes a piston disposed within the fluid chamber and a shaft extending therefrom that is securable to the other of the ground engaging member or frame. The piston has a first side and a second side, and moves within the fluid chamber under a force acting on the suspension strut. A bypass channel is provided in fluid communication with the fluid chamber on the first side of the piston and with the fluid chamber on the second side of the piston, bypassing the piston therebetween. A valve is disposed in fluid communication with the bypass channel to automatically control the flow of fluid through the bypass channel during movement of the piston assembly relative to the stanchion tube. The phrase "bypassing the piston" is used in this sense to mean a fluid path which flows from one side of the piston to the other side of the piston without the necessity of flowing through compression dampening passages and/or rebound dampening passages that are preferably provided within the piston. Brief Description of the Drawings The foregoing aspects and many attendant advantages of this invention will become more readily appreciated as the same becomes better understood by reference to the following detailed description, when taken in conjunction with the accompanying drawings, wherein: FIGURE 1 is a side elevational view of the shock absorber of the present invention secured in the rear suspension of a bicycle; FIGURE 2 A is a cross-sectional view of the shock absorber illustrated in FIGURE 1; FIGURE 2B is a partial cross-sectional view of the shock absorber illustrated in FIGURE 2A during a compression stroke; FIGURE 2C is a partial cross-sectional view of the shock absorber during a rebound stroke; FIGURE 3 A is an exploded view of the dampener valve assembly; FIGURE 3B is an isometric view of the piston body; FIGURES 4A and 4B are a plan view and partial cross-sectional view, respectively, of the piezoelectric disk that is seated against the valve body; FIGURE 5 is a plan view of an alternative embodiment of the valve disk illustrated in FIGURES 4A and 4B; FIGURE 6 is a schematic diagram of the logic circuit used to control the piezoelectric disk illustrated in FIGURES 4 A and 4B; FIGURE 7A graphically illustrates damping force versus shaft velocity for three levels of damping; FIGURE 7B graphically illustrates damping force during damping piston travel within the shock absorber of the present invention; and FIGURE 8 is a cross-sectional view of the alternate preferred shock absorber having a bypass valve; FIGURE 9 is an exploded isometric view of the bypass housing and valve of the shock absorber illustrated in FIGURE 8; FIGURE 10A is a cross-sectional view of the bypass shock absorber with the piston in a partially compression position; FIGURE 10B is a cross-sectional view of the bypass shock absorber in a nearly fully compressed position; FIGURE 11 A is a partial cross-sectional view of a first alternate bypass valve arrangement for the shock absorber; FIGURE 1 IB is a plan view of a portion of the bypass valve arrangement of FIGURE 11 A; FIGURE 12A is a partial cross-sectional view of a second alternate bypass valve arrangement for the shock absorber; FIGURE 12B is a top view of a portion of the valve arrangement of FIGURE 12A; FIGURE 12C is a top cross-sectional view of a lower portion of the valve arrangement of FIGURES 12A and 12B; FIGURE 13 provides a front plan view of a telescoping front fork suspension assembly incorporating an alternate embodiment of a bypass valve arrangement of the present invention; FIGURE 14 provides a longitudinal cross sectional view of the bypass valve arrangement taken along line 14-14 of FIGURE 13; FIGURES 15 and 16 provide partial longitudinal cross sectional views of the bypass valve and piston areas, respectively, of the bypass valve arrangement of FIGURE 13; FIGURE 17 provides a longitudinal cross sectional view of a still further alternate embodiment of a bypass valve arrangement of the present invention; and FIGURES 18 and 19 provide partial longitudinal cross sectional views of the bypass valve and piston areas, respectively, of the bypass valve arrangement of FIGURE 17. Detailed Description of the Preferred Embodiments The shock absorber damping system of the present invention may be employed in a multitude of different applications. However, the system disclosed and described herein is particularly well suited to vehicles, especially bicycles of the mountain bike variety. The system is also well suited to motorcycle suspension systems, especially off-road motorcycles. Mountain bicycles will be referred to throughout this detailed description. However, it should be understood that mountain bikes are simply the preferred application and the same concepts and basic constructions can be used in other shock absorber applications. The damping system of the present shock absorber is particularly advantageous with mountain bikes since large, medium, and small bumps, drops, and shock-producing surfaces are encountered during mountain bike riding. Typically, low amplitude bumps occur at a high frequency. For example, a washboard gravel road may have numerous, close together small bumps that create high frequency, low amplitude shocks at the wheels of the bicycle. Conversely, high amplitude bumps have a relatively lower frequency, since the size of the bump itself dictates that the bumps be somewhat spaced apart. A street curb is an example of a high amplitude, low frequency bump. Numerous rocks, bumps, roots, and other obstacles are encountered when mountain biking off-road. The shock absorber of the present invention is designed to handle all these bumps. Further, the shock absorber may also be programmed to reduce other undesirable cycling effects such as pogo action or bobbing, as well as chain-induced suspension action. FIGURE 1 illustrates a mountain bike with the shock absorber of the present invention. Bicycle 10 includes a frame 12, wheels 14, a front suspension 16, and a rear suspension 18. Front suspension 16 is attached to the head tube portion of frame 12 and includes forks 20 that extend downwardly from linkages 22 connecting forks 20 to the frame head tube. A front shock absorber 24 is disposed between linkages 22 to provide front suspension action. Both shock absorption and damping are provided by front shock absorber 24, as is described in detail below. Front suspension 16 may have many alternative configurations, such as telescoping forks, other linkage mechanisms, or shock absorbing stems. The same damping concepts discussed herein can be applied to these other arrangements. Rear suspension 18 includes a rear swing arm 26 pivotally attached to frame 12 about a pivot 28. A rear shock absorber 30 is also attached at one end to frame 12. Shock stays 32 extend upwardly from the rearward end of swing arm 26 to the lower end of rear shock absorber 30. Thus, when swing arm 26 pivots upwardly about pivot 28, shock absorber 30 is compressed such that the rear wheel 14 is allowed to move relative to frame 12 to absorb and dampen shock. Again, alternative rear suspension systems can be employed with rear shock absorber 30. Other systems may include unified rear triangles, unified swing arm and chain stay arrangements, and other linkage assemblies. Leverage ratios on the shock absorber may change, for example, while still using the same core damping technology. The concepts herein can also be applied to pull shock absorbers. In all of these systems, damping of the suspension action is advantageous. Bicycle 10 also includes a drive system 34. Drive system 34 is preferably constructed as is known in the art. Drive system 34 includes a chain 36 that extends around chain rings 38 that are attached to frame 12 via the bottom bracket. Cranks 40 are also secured to chain rings 38 with pedals 42 at the outer ends. Rear sprockets 44 are secured to the rear wheel 14 with a rear derailleur 46 for shifting the chain from one sprocket to another. Drive system 34 is relevant to shock absorption, particularly in the arrangement illustrated in FIGURE 1, since the upper drive line of chain 36 extends beneath pivot 28 such that as force is applied to pedals 42, chain 36 slightly pulls suspension 18 downwardly. This can be advantageous as it helps to increase traction of rear wheel 14 on the riding surface. However, if the rider does not have smooth pedaling action, then cyclic forces on chain 36 may cause cyclic bobbing of rear suspension 18 as the bicycle is ridden. As will be explained in more detail below, the damping system of rear shock absorber 30 can help eliminate such chain-induced suspension action. Referring now to FIGURES 2A-C, the details of the inner construction of shock absorber 30 will now be discussed . Note that while shock absorber 30 refers to the shock absorber used with the rear suspension of the bicycle illustrated in FIGURE 1, the same or similar shock absorber can be employed on the front suspension. Externally, shock absorber 30 appears much like standard shock absorbers currently on the market. Many details of the shock absorber are much like those manufactured by Noleen Racing of Adelanto, California. Shock absorber 30 includes a shaft 48 extending into a reservoir housing 50. A spring 52 extends along shaft 48 and over a portion of reservoir housing 50. Spring 52 absorbs shock and provides rebound while shaft 48, extending into reservoir housing 50, provides damping as explained below. Reservoir housing 50 encloses hydraulic reservoir 54 and gas chamber 56. Hydraulic reservoir 54 is separated from gas chamber 56 by a chamber seal 58. In the preferred embodiment of the invention, both gas chamber 56 and hydraulic reservoir 54 are contained within the same cylindrical reservoir housing 50. Chamber seal 58 includes an O-ring to separate gas chamber 56 from hydraulic reservoir 54 and to allow chamber seal 58 to move within reservoir housing 50 as needed. Gas chamber 56 preferably holds nitrogen gas such that additional damping is provided when the gas is compressed due to a large shock. Alternatively, a gas chamber may be mounted outside reservoir housing 50 in its own chamber with an interconnecting channel as is well known in the art. The outer end of reservoir housing 50 opposite shaft 48 includes a housing end mount 60 for mounting the end of rear shock absorber 30 either to a bicycle frame or to other suspension components. A shaft end mount 62 is provided on the opposite side of shock absorber 30 at the end of shaft 48. Note in FIGURE 1 that shaft end mount 62 is mounted to frame 12 while housing end mount 60 is secured to shock stays 32. Spring 52 is held on shaft 48 and reservoir housing 50 with spring stop 64 secured to shaft 48 at the end of shaft end mount 62 and preload wheel 66 at the opposite end of spring 52. Preload wheel 66 is threadably engaged on reservoir housing 50. Thus, by turning preload wheel 66, the preload in spring 52 can be adjusted. An electronics housing 68 is also provided on shock absorber 30. Housing 68 holds the power supply and circuitry, as well as the sensor necessary to control the damping action of shock absorber 30. Housing 68 is secured to reservoir housing 50 with housing clamp 70 extending around the outside thereof between preload wheel 66 and housing end mount 60. Hydraulic reservoir 54, when manufactured, includes an opening at only one end through which shaft 48 is inserted. A reservoir seal 72 (including the seal head, the scraper seal, and the O-ring) extends around shaft 48 and is held tightly within the open end of reservoir housing 50 in order to create an enclosed reservoir 54. A reservoir cap 74 is also included on the outside of reservoir seal 72. Reservoir cap 74 and reservoir seal 72 ensure that no hydraulic fluid escapes from hydraulic reservoir 54. O-rings are employed at critical locations to ensure adequate sealing. Should shaft 48 extend all the way into reservoir 54, reservoir cap 74 will abut a bottom out bumper 76 held on shaft 48 adjacent spring stop 54. As with standard Noleen Racing shock absorbers, an adjustment needle 78 is housed within shaft 48, shaft 48 being hollow. Adjustment needle 48 regulates the bypass flow of hydraulic fluid within hydraulic reservoir past the piston 86. An adjustment wheel 80 is provided to move adjustment needle 78 longitudinally within shaft 48 in a conventional manner. An element not included in conventional shock absorbers, wire 82, extends from housing 68 through a wire seal 84 in shaft end mount 62. Wire 82 then extends through a hollowed central core of adjustment needle 78 to near the tip thereof. This wire electrically links the electronics within housing 68 to the dampener valve for control thereof. Since wire 82 extends out the side of adjustment needle 78, rotation of adjustment needle 78 must be kept in check. Therefore, pin 96 extends through the side of shaft 48 into a recess in the side of adjustment needle 78 such that wire 82 may be properly channeled to the side of bender 94. As will be explained below, wire 82 actually includes multiple wires within a tough, flexible housing. The piston assembly of shock absorber 30 is seen in its assembled configuration in FIGURES 2A-C and in an exploded view in FIGURE 3 A. FIGURE 3B illustrates an enlarged view of a piston 86. As seen in FIGURES 2A-C and FIGURE 3 A, a band 88 constructed of a Teflon material is secured around piston 86. In the preferred embodiment of the invention, shim washers 90 are stacked against the innermost end of piston 86 (shim washers 90 are shown all together in FIGURES 2A-C such that they appear to be a single truncated cone). Shim washers 90 function in a conventional manner to regulate the flow of fluid through piston 86, especially during rebound as shaft 48 moves away from reservoir housing 50. A nut 92 is threadably engaged on the innermost end of shaft 48 to hold shim washers 90 securely against piston 86. Nut 92 thus holds the entire piston assembly on the end of shaft 48. A bender 94 is secured on the opposite side of piston 86 from shim washers 90. Bender 94 will be discussed in more detail below in connection with FIGURES 4A and 4B. Bender 94 includes piezoelectric material that is connected to wire 82 in order to apply a voltage across bender 94. Bender 94 is preferably arranged on the shaft side of piston 86 in order to control the compression damping of the piston assembly when it travels through reservoir 54. As seen in FIGURES 2A-C and 3A, bleed spacer 98 is held on the shaft side of bender 94 and is seated on the shoulder of shaft 48 to hold the piston assembly between the shoulder of shaft 48 and nut 92. Bleed spacer 98 allows the bypass of fluid flow past adjustment needle 78, allows a conduit through which wire 82 extends to the side of bender 94, and rests on the shoulder of shaft 48 for holding the piston assembly in place. A flexible top out bumper 100 is force-fit onto shaft 48 below bleed spacer 98. Top out bumper 100 is useful when shaft 48 is pushed all the way out to the end of its stroke by spring 52 such that bumper 100 contacts reservoir seal 72. In the preferred embodiment of the invention, a sensor assembly is provided to detect both the displacement of shaft 48 and the piston assembly relative to the reservoir housing 50 as well as the velocity of shaft 48 and the piston assembly. In the preferred embodiment of the invention a giant magnetorestrictive sensor (GMR) is employed. Other sensors may alternatively be used to detect either the displacement or velocity of shaft 48 relative to housing 50. For example, proximity sensors, variable reluctance sensors, or other magnetic or mechanical sensors may be used. GMR sensors are also referred to as magnetoresistive sensors. (Description of such sensors can be found in prior art, such as in U.S. Patent No. 5,450,009 to Murakami, and in multiple journal articles. Examples of articles discussing such sensors include "Magnetic Field of Dreams," by John Carey, Business Week, Apr. 18, 1994; "The Attractions of Giant Magnetoresistance Sensors" by Ted Tingey, Electrotechnolog , Vol. 7, part 5, pgs. 33-35, Oct.-Nov. 1996; and in "High Sensitivity Magnetic Field Sensor Using GMR Materials With Integrated Electronics," by Jay L. Brown, Proc. IEEE International Symposium on Circuits and Systems Vol. 3, pgs. 1864-1867, 1995.) The sensor and control arrangement preferably employed in the present invention includes a magnet 102 secured about nut 92 on the end of the piston assembly. A sensor 104 is secured within housing 68 adjacent reservoir housing 50 near the closed end thereof. Sensor 104 can alternatively be mounted at the end of housing 50. Sensor 104 is connected to circuit board 106. Circuit board 106 (or alternatively a microprocessor chip that includes the microprocessor logic to control bender 94 based on the detection signal from sensor 104. Circuit board 106 is then in turn connected to wire 82 for connection to bender 94. The operation of circuit board 106 will be explained in more detail in connection with FIGURE 6. A battery 108 is also held within electronics housing 68 in order to provide power to sensor 104 and to bender 94. Preferably, a conventional 9- volt battery is used within electronics housing 68 to provide the power required for the bender and the sensor. Referring now to FIGURE 3B, further details of the functioning of the piston and valve assembly will be described. Piston 86 is the type sometimes used with shim washers 90. Piston 86 includes a shaft bore 110 that slides over the end of shaft 48 to be held thereon. Shaft bore 110 is disposed in the center thereof and is circular in cross-section. A circumferential recess surrounds the outer curved side of piston 86. Circumferential recess 112 is sized to secure Teflon band 88 therein. The face of piston 86 that is turned toward shaft 48 is illustrated in FIGURE 3B. The large openings in piston 86 are the compression flow channels 114. These channels extend entirely through piston 86 and actually begin within recesses on the opposite side of piston 86 from that shown in FIGURE 3B. Thus, during compression (when shaft 48 is being pressed into reservoir 54, see FIGURE 2B) fluid easily enters channels 114 since the recesses allow the flow to go beneath shim washers 90 into channels 114. However, bender 94 is secured adjacent the shaft side of piston 86 so as to obstruct the flow of fluid through channels 114 at their exit ends. By controlling the stiffness or bias of bender 94, the flow through compression flow channels 114 (see FIGURE 2B) can be effectively controlled to increase or decrease the damping. Rebound flow channels 116 also extend through piston 86. Note that these channels are held within rebound flow recess 118 so that bender 94 does not significantly obstruct the flow of fluid back through rebound flow channels 116 (see FIGURE 2C). However, note that the size of these channels is somewhat smaller than that of compression flow channels 114 such that rebound damping is generally greater than compression damping. The flow through rebound flow channels 116 extend from the face shown in FIGURE 3B to the opposite face as the piston assembly moves in the direction of shaft 48. Flow in this direction is obstructed by shim washers 90 which are deflected by the flow through rebound flow channels 116 and by some flow through compression flow channels 114. Rebound flow recess 118 not only extends around the entrance of rebound flow channels 116, but includes arms that extend between compression flow channels 114 such that flow may move around bender 94 for rebound action. In an alternate embodiment of the invention, shim washers 90 may also be replaced by a bender such as bender 94 to more completely control rebound damping, as well as compression damping with the piston assembly. In another alternate embodiment of the present invention, the flow channel or channels are disposed in the side of a modified reservoir housing. In this embodiment, the bender is positioned to regulate the flow of fluid from one side of the piston to the other through the channel in the housing as the piston is forced through the reservoir. Control of the bender then affects the level of damping. Referring now to FIGURES 4A and 4B, the construction of bender 94 will be described. Bender 94 includes a disk 120 preferably constructed of a polyimide material. A Polyimide polymer is preferably used due to its toughness and electric insulating characteristics. Disk 120 includes a center aperture 122 which slides over the end of shaft 48 between piston 86 and bleed spacer 98. Note that the top of bleed spacer 98 includes a small cylindrical projection to space the outer portion of disk 120 from the remainder of bleed spacer 98 to allow bender 94 to flex downwardly toward bleed spacer 98. Within disk 120 a piezoelectric top layer 124 and piezoelectric bottom layer 126 are held. Top layer 124 and bottom layer 126 are spaced from one another. Alternative embodiments of the invention include only a single piezoelectric layer or more than two piezoelectric layers. Piezoelectric layers 124 and 126 are also disk- shaped in parallel planes to one another and parallel to the plane of disk 120. First and second electrodes 128 and 130 contact the upper and lower faces of top layer 124. Electrodes 128 and 130 are connected to circuit board 106 such that a voltage can be applied across piezoelectric top layer 124. As seen in FIGURES 4A and 4B, first and second connectors 136 and 138 are provided for connection to wires held within wire 82. Third and fourth electrodes 132 and 134 are likewise secured above and below piezoelectric bottom layer 126 such that a voltage can be applied thereacross. Note that third electrode 132 is adjacent second electrode 130, but does not come in contact therewith. Thus, voltages may be independently applied across top layer 124 and bottom layer 126. Referring to FIGURES 4A and 4B, third and fourth connectors 140 and 142 are coupled to third and fourth electrodes 132 and 134. When a voltage is applied across piezoelectric top layer 124, the material bends in one direction depending on the polarity of the applied voltage. The piezoelectric layer will always be biased to flex such that the concave side of the layer is the positive polarity, whereas the convex side is the negative polarity. Therefore, if a voltage is applied across top layer 124 in the same direction as across bottom layer 126, then both piezoelectric layers will bend or at least be biased in the same direction and bias bender 94 in the same direction. Since bender 94 bears against compression flow channels 114 of piston 86, then if first electrode 128 and third electrode 132 have the negative polarity as the voltage is applied across top and bottom layers 124 and 126, the damping will be increased since bender 94 will tend to be biased strongly toward piston 86. Thus, increased damping results since the fluid flow through compression flow channels 114 is more highly restricted by bender 94 essentially having a higher spring rate under the applied voltage. Alternatively, if first and third electrodes 128 and 132 have the positive polarity and second and fourth electrodes 130 and 134 have a negative polarity, then bender 94 is biased slightly away from compression flow channels 114 to decrease the compression damping as piston 86 is forced through reservoir 54. With no voltage applied across layers 124 and 126, the normal stiffness of disk 120 then affects the flow with a medium level of damping. Alternatively, differing levels of damping may be accomplished by changing the voltage applied across top layer 124 and bottom layer 126 rather than simply changing the polarity of the voltage applied. In the preferred embodiment of the invention, amplifiers increase the voltage from the 9-volt battery to 200 volts to be applied across the layers of piezoelectric material. In still other alternative embodiments, a different "bender" may be used. For example, and alternate bender 94' is illustrated in FIGURE 5. The bender 94' utilizes alternately shaped electrodes 128', but functions similarly to bender 94. All corresponding components of bender 94' are numbered the same as for bender 94, but are noted with a prime. As a further example, instead of utilizing a piezoelectric material to move the bender valve, other primary movers could change the biasing force of a bender covering a fluid channel. For example, an electromagnet could be employed to change the force of a bender against a flow orifice. Likewise, if shim washers 90 are replaced with a bender valve such as has been described with regard to bender 94, rebound damping can be controlled by applying voltage to piezoelectric material within a disk. FIGURE 6 illustrates in a schematic diagram the basic logic to drive the two piezoelectric layers 124 and 126 within bender 94. As the shock moves, the position and velocity sensor 104 sends signals through an instrumentation amplifier to the microprocessor. The logic in the microprocessor, at predefined conditions, sends signals to the amplifier such that the power is provided through the amplifier across the piezoelectric top and bottom layers in a desirable fashion to either increase or decrease the damping level by changing the bending bias of bender 94. The amplifier changes the voltage applied across the piezoelectric material from 9 volts to preferably 200 volts. While in FIGURE 6 piezos A and B are shown connected together, it should be noted that this is simply a schematic diagram and piezos A and B may be independently switched on and off of applied voltages across them in one direction or another. The specific electronics for such a circuit which would selectively apply voltages to piezoelectric top and bottom layers 124 and 126 may be readily accomplished by those skilled in the electronics arts. Alternatively, instead of a 9-volt battery, other battery or power supplies may be employed. For example, if the present system were employed on a motorcycle, the power supply could come from the motorcycle power supply (e.g., battery or magneto). The damping force versus shaft velocity of the shock absorber for each of the three basic scenarios of bender 94 is illustrated in FIGURE 7A. The line representing the "MID" damping force is the condition in which no voltage is applied across top and bottom layers 124 and 126 of the piezoelectric material. In this condition, bender 94 acts much like a metal shim that is deflected away from the flow through piston 86 as piston 86 is forced through hydraulic reservoir 54. With an increase in shaft velocity, the damping force naturally increases. However, if a voltage is applied across piezoelectric top and bottom layers 124 and 126 such that the negative polarity is applied to the first and third electrodes 128 and 132, a condition of maximum damping is achieved such that the damping follows the "MAX" curve shown in FIGURE 7 A. However, if the polarity is reversed such that bender 94 is biased away from piston 86, the damping force follows the "MDSP' curve illustrated in FIGURE 7A. Thus, without changing the amount of applied voltage, but just by changing the polarity of the voltage or whether the voltage is applied at all, three discreet levels of damping can be achieved. In each of these levels the damping increases with shaft velocity. The "MID" level of damping is constructed so that the bender reacts the same as a current dampener piston assembly with shims being used instead of bender 94 such that if no power is applied to the piezoelectric layers, then the shock absorbers still provide good shock performance. This would be the case, for example, if the battery were dead or in case of some other electrical breakdown. Referring now to FIGURE 7B, a preferred programming of the dampener will be described. With a rider's weight on bicycle 10, shock absorber 30 will move to about 20% of travel. At this point, the compression damping will be at the nominal level (MID curve of FIGURE 7A) to provide resistance to pogo action of the suspension system due to rider bobbing or chain-induced suspension action. Alternatively, maximum damping may be applied at this point to further reduce pogo action. However, preferably the MID level of damping is provided until approximately 25% of the travel. As soon as the shaft moves beyond the 25% point, the system switches to minimum damping by applying the proper voltage with the proper polarity across piezoelectric layers 124 and 126. Thus, when the rider encounters low amplitude, high frequency shock, the damping is at a minimum level to be able to respond quickly to the shock and absorb it without the shock being transferred to the rider through the bike frame 12. If the shaft goes past 50% of travel, its velocity is computed by the sensor and chip. If the velocity is greater than about 30 inches per second the system switches to the MED level of damping. This would be the case when a larger bump is encountered. If the velocity of the shaft is greater than 60 inches per second, the damping would switch directly to the MAX damping level to deal with extremely large bumps. At 70% of travel, the shaft velocity will be recomputed and, if greater than 30 inches per second and not already in the stiff MAX level, then it would be switched to that level. Thus, the system will avoid the suspension completely bottoming out by providing increased compression damping to handle the large shocks. When the shaft returns to a position less than 50% of travel, the system switches to the MED stiffness level, if it is not already there. The above is just one possible scenario that may be programmed into the logic circuit in the circuit board or chip such that the suspension damping actively and instantaneously responds to shocks encountered. The FIGURES above for velocity and displacement are simply one set that could be used. Depending on how the shock is arranged with a given suspension system and the desired attributes of the shock, these numbers can be changed and the chip or circuit board can be programmed accordingly. Thus, the level of damping is automatically and instantaneously changed during riding so that low amplitude, high frequency bumps are easily absorbed with minimal damping while large high amplitude low frequency bumps are absorbed with higher damping so as to not bottom out the suspension and to avoid the shock from springing back too quickly. Both velocity and displacement of the shaft relative to the reservoir housing 50 are important to proper damping. If the travel passes 50%, but the velocity is very slow, then increased damping is not required. However, if the travel passes 50% with a very high velocity, then increased damping can be effective in improved shock absorber performance. Nevertheless, alternative embodiments may also be employed where velocity by itself or displacement by itself are measured and the damping level is adjusted based on a single input. Further, other sensor input may also be employed to control damping levels. Referring now to FIGURES 8 - 12, a preferred embodiment of a bypass valve arrangement of the present invention will now be described along with two alternate embodiments of the bypass valve arrangement. The bypass valve utilizes many of the same concepts and features discussed above, especially in the preferred embodiment. Thus, the above discussion of the operation of the electronic circuitry to increase or decrease the damping forces during certain portions of the stroke of the piston or travel of the suspension substantially applies to the embodiments discussed below. Furthermore, the advantages discussed above also apply to these embodiments. The last two digits of the numbering is the same as above for similar or identical elements designated below. The bypass valve preferred embodiment of the invention will now be discussed with FIGURES 8 - 10. The bypass valve functions with a shock absorber arrangement very similar to that discussed above in that the shock absorber includes a shaft 148 having a spring 152 thereabout, the shaft connected to a piston 186 that is slidably disposed within a hydraulic reservoir 154. Hydraulic reservoir 154 is formed with a reservoir housing 150. In this particular embodiment of this invention, reservoir housing 150 includes a housing flange 249 to secure the bypass valve arrangement. Piston 186 may include piezo disks at the end thereof to control the flow through piston 186 as described above. However, in the preferred embodiment of the shock absorber 130 with the bypass valve arrangement, conventional rebound shim washers 190 and compression shim washers 191 are employed against the forward and trailing sides of piston 186. Piston 186 includes a magnet 202 secured about nut 192 to provide a preferred method of sensing the position and displacement of piston 186 relative to housing 150 in combination with a sensor 104 secured near the housing end mount 160 of shock absorber 130 as described above. Shim washers 190 and 191 are preferably a stack of thin metallic washers that can be arranged and adjusted to preset characteristics for compression and rebound damping. With the bypass valve arrangement, shim washers 190 and 191 may be arranged and constructed such that higher damping through piston 186 is achieved due to the extra damping allowed through the bypass valve assembly as described below. The bypass valve assembly is best illustrated in FIGURES 8 and 9. Reservoir housing 150 is specially constructed so as to include housing flange 249 to secure the elements of the bypass valve assembly. Reservoir housing 150 includes the standard housing to create hydraulic reservoir 154. Within the sides of reservoir housing 150 inflow openings 256 and outflow channel 276 extend therethrough into inflow chamber 258. Orifice plate 254 separates inflow chamber 258 from outflow channel 276. Orifice plate 254 covers inflow openings 256 and channels the fluid that enters inflow openings 256 to an orifice 260. Orifice plate 254 has a generally parallelepiped outer shape with a lower recess to form inflow chamber 258 between orifice plate 254 and reservoir housing 150. Orifice 260 is a slot with upwardly projecting lips within one end of orifice plate 254. The lips extend upwardly from the upper surface of orifice plate 254. Bender 252 is seated on top of orifice plate 254. The lower surface of bender 252 is protected with a valve shim 264. Bender 252 is generally rectangular in shape and includes a layered construction such as that described above for use with the piezo disk embodiment. Bender 252 includes a bender cable 266 that extends upwardly from the rearward end of bender 252 to provide electrical interconnections in order to apply voltages across the various layers of bender 252. Valve shim 264 is preferably constructed of a brass material and is secured to the rearward ends of both orifice plate 254 and bender 252. Valve shim 264 is generally coextensive with the bottom surface of bender 252 to protect the bottom surface thereof. Valve shim 264 is thus sandwiched between bender 252 and orifice plate 254 and rests immediately on top of the lips of orifice 260 to restrict the flow thereof with bender 252. Bender 252 may alternatively be comprised of another response material that may be variably biased based on magnetic or electrical or other forces. Alternatively, bender 252 may simply be a passive bender, such as spring steel, to simply have a constant spring rate or variable spring rate depending on the stacking of shims, for example, to affect the flow through orifice 260. A bender clamp 268 with screws secures the bender, valve shim, and orifice plate assembly to the top of reservoir housing 150. A substantially rectangular bypass cover 250 with a recess in the lower side thereof is secured to housing flange 249 to secure the entire valve assembly in place. Bypass cover 250 includes cable opening 269 to allow bender cable 266 to project therethrough for interconnection with a wire ribbon 274 leading to the electronics circuit board within electronics housing 168 as described above. The cable O- ring 270 and cable seal clamp 272 secure to the top of cable opening 269 to seal bender cable 266 such that no fluid escapes bypass cover 250. Electronics housing 168 covers the top of bypass cover 250 and includes the circuit board, battery, and wire ribbon to control the biasing of bender 252 to actively control the flow through the bypass valve assembly; the electronics may activate the bender, as described above with regard to the disk-shaped bender. Thus, the biasing force supplied by bender 252 onto orifice 260 may be varied based on input received from sensor 204 and transmitted to the circuit board. Referring now to FIGURES 8, 10A and 10B, the basic functioning of the bypass valve assembly will now be described. Shock absorber 130 illustrated in FIGURE 8 is in an initial position before being compressed either by rider weight or by forces acting on shock absorber 130, such as bumps or other shocks to the bicycle or other apparatus to which shock absorber 130 is secured. The following description will refer to shock absorber 130 for use in its preferred application on a mountain bike. However, it should be understood that shock absorber 130 could be used for other articles, including other vehicles, machines, or other devices. In the initial position illustrated in FIGURE 8, note that piston 186 is below both inflow openings 256 and outflow channel 276 such that compression of piston 186 within hydraulic reservoir 154 will not yield any bypass flow. Thus, the initial stroke of piston 186 is somewhat stiff due to not having this extra damping action. This is desirable at the beginning of the stroke to decrease rider-or pedal- induced suspension action on a mountain bike. This also is the general region in which the preload from the weight of the rider will act on shock absorber 130. Thus, it is desirable that shock absorber 130 not compress excessively under the preload of the rider, but retain most of its suspension action for actual shocks encountered while riding. Alternate embodiments of the invention, wherein initial soft damping is required, may include outflow channel 276 extending below piston 186 when in the no-stroke position illustrated in FIGURE 8. Note in this position that as force is applied to compress piston 186 within reservoir 154 that the pressures will be balanced and no substantial flow through the bypass valve assembly will occur. The only flow from one side of piston 186 to the other must occur through piston 186 itself. If no flow channels are provided in piston 186, movement could still be allowed due to the compression of the gas within gas chamber 156. This would be the case if particularly stiff damping is desired during the initial portion of the stroke of shock absorber 130. FIGURE 10A illustrates an intermediate stroke position of piston 186 within reservoir 154. In this position, piston 186 is beyond outflow channel 276 such that flow through the bypass valve assembly is allowed; as piston 186 pushes further within reservoir 154, fluid is forced through inflow openings 256 into inflow chamber 258. From inflow chamber 258, fluid proceeds to orifice 260 and is forced against the lower side of valve shim 264 held in place by bender 252. Note that bender 252 is biased against orifice 260 as controlled by the logic circuit of the circuit board housed within electronics housing 168 as described above. Alternatively, the variable biasing of bender 252 may be turned off such that the natural spring resilience of bender 252 simply operates in a constant bias against orifice 260 to control the flow. In another alternate embodiment of the electronics, bender 252 may be biased to a set condition by applying a constant voltage to the piezoelectric material sandwiched within bender 252. In any event, as the pressure of the fluid bears sufficiently against bender 252, the fluid passes between the orifice 260 and bender valve shim 264 to enter outflow channel 276 and fill in behind piston 186. Note that this region of piston 186 compression may be the lowest damping force in this preferred embodiment since flow is allowed through all of inflow openings 256 (preferably five) and out of outflow channel 276 to the back side of piston 186. In the position of piston 186 illustrated in FIGURE 10B, the flow through the bypass valve assembly is again somewhat restricted. This is due to the sides of piston 186 initially blocking the first holes of inflow openings 256 and then blocking all of inflow openings 256 such that no flow extends through the bypass valve assembly. Thus, shock absorber 130 becomes much stiffer. This can be very advantageous to avoid bottoming out shock absorber 130 during a heavy shock event. By having inflow openings 256 sequentially covered, the damping force increases the closer piston and shock absorber 130 come to bottoming out. Thus, three inflow openings 256 are first covered and then two additional openings are covered before flow is entirely stopped through the bypass valve assembly. Thus, even without electronic or other control of bender 252, significant advantageous properties of damping are achieved with the bypass valve arrangement illustrated and described above. The damping is higher at the initial portion of the stroke to deal with rider preload, as well as pedal- or rider-induced bobbing, and eliminate these negative effects on the shock absorber. As actual bumps are encountered, the damping goes to a moderate to low level to allow the shock absorber 130 to absorb the shock effectively. When large bumps are encountered, the damping progressively increases as the stroke increases to cover inflow openings 256. By further including an active piezo bender 252 combined with a sensor 204, the velocity of piston 186 can also be taken into account in addition to the displacement to change the damping force to an optimum level for the smoothest ride possible with the best connection of the wheels to the ground. The arrangement is also advantageous should the electronics or wiring fail in the piezoelectric embodiment; the shock absorber would still work better than standard shock absorbers if a given spring constant is inherent in bender 252 to provide damping by having a constant biasing force against orifice 260. An alternate embodiment of the bypass valve assembly will now be described in connection with FIGURES 11 A and 1 IB. In this embodiment, a valve body 378 is provided and moved by piezo bender 352. The valve body itself is balanced with respect to the fluid forces flowing through the bypass valve assembly such that piezo bender 352 does not have to bear as much against the full pressure of the flow of the fluid through the bypass valve assembly. During compression of the piston, flow enters inflow openings 356 and pushes upwardly on a flapper valve 388. Flapper valve 388 is preferably a thin sheet of stainless steel that may be easily bent upwardly by the pressure of the fluid flowing through inflow openings 356. Flapper valve 388 obstructs flow going in the opposite direction such that flow will not exit inflow openings 356. Fluid then enters inflow chamber 358 which is beneath and surrounds bender 352. Bender 352 is secured to chamber plate 354 with a bender clamp 368 secured to the bottom thereof. Thus, bender 352 is secured to the underside of chamber plate 354. The sides of chamber plate 354 are narrower than inflow chamber 358 such that flow is allowed to move above chamber plate 354 into upper channel 380 that extends to valve body 378. Valve body 378 is generally cylindrical in shape and moves in a direction transverse to the longitudinal axis of the shock absorber and transverse the longitudinal axis of bender 352. Thus, bender 352 moves up and down with valve body 378 without valve body 378 moving in a direction opposite the flow of fluid through the bypass valve assembly. Valve body 378 includes a valve recess at a lower portion thereof on the side of valve body 378 abutting bender 352. The end of bender 352 extends within valve recess 384. A bender clip 369 is secured to the end of rectangular-shaped bender 352 to engage within valve recess 384. Bender clip 369 is preferably C-shaped in cross-section and its inner portion is secured to the distal end of bender 352. The outer corner of bender clip 369 bears against the sides of valve recess 384 such that when piezo bender 352 is biased upwardly or downwardly due to an applied voltage across the layers thereof (as discussed above), bender clip 369 will push valve body 378 upwardly or downwardly to restrict or allow flow over the top of valve body 378. Valve body 378 includes a hollow core 382 such that valve body 378 is balanced. In other words, the pressure of the hydraulic fluid will not have as much effect on the position of valve body 378 since fluid is allowed to flow entirely through valve body 378. In order for flow to exit the bypass valve, and valve body 378 in particular, it must pass over the rim of valve body 378 into side channels 386. FIGURE 11B, illustrates flow over the top of valve body 378 into side channels 386 such that the flow can exit through outflow channel 376. The upper rim of valve body 378 is angled to further decrease the effect of the flow on biasing valve body 378 downwardly. Thus, with a substantially balanced valve body 378, the power requirements to move bender 352 are much lower. The embodiment described and illustrated in FIGURES 11A and 11B otherwise functions much the same as the preferred bypass valve arrangement described above with inflow openings 356 and outflow channel 376 positioned accordingly. A second alternate embodiment with a balance valve body will now be described in connection with FIGURES 12A - 12C. In this embodiment, a valve body 478 is provided that is also balanced somewhat to avoid the effect of the direct force of the fluid flowing through the bypass valve arrangement pushing the valve body 478 away from flow restriction and thus requiring less power. The embodiment illustrated in FIGURES 12A - 12C may require even less power than other embodiments due to its arrangement of secondary flow moving valve body 478 with a diaphragm 504. A bender 452 is provided clamped within a chamber plate 454 in a manner similar to that described above in connection with FIGURES 11A and B. However, bender 452 does not extend to a direct connection with valve body 478 . Bender 452 secures to chamber plate 454 with bender clamp 468, but extends toward valve body 478 only enough to cover a secondary flow orifice 460. Secondary flow orifice 460 provides a small opening adjacent cylindrical valve body 478, which allows a moderate flow of fluid to extend upwardly and be channeled into a secondary flow channel 490. Secondary flow channel 490 channels the secondary flow to the side of chamber plate 454 and then upwardly such that it may enter into a diaphragm chamber 492 disposed above cylindrical diaphragm 504. Diaphragm 504 is cylindrical in shape and is sealed to chamber plate 454 with seals 506 directly above valve body 478. Valve body 478 is cylindrical in shape and has a hollow core 482. Valve body 478 also includes a valve stem 494 projecting upwardly from the center thereof to engage the center of diaphragm 504. Diaphragm 504 is constructed of a thin elastically flexing material. Thus, when diaphragm 504 moves upwardly or downwardly, it moves valve body 478 upwardly or downwardly accordingly. A balance chamber 480 is provided below diaphragm 504 to allow for movement of diaphragm 504 and to balance the fluid forces on valve body 478 such that it can move transverse to the general primary flow of fluid through the bypass valve assembly. The primary flow proceeds through inflow openings 456 beneath flapper valve 488 and then into side channels 486, Side channels 486 are illustrated in FIGURE 12C and extend from the side of a lower plate 500 beneath valve body 478 to the sides of valve body 478. The exit of flow is allowed through the side of valve body 478, which includes a flow recess 498 to allow the flow to exit into outflow channel 476. Note that a balance orifice 496 extends through the top of valve body 478 to allow fluid to enter balance chamber 480 such that the pressure of the primary flow does not press valve body 478 upwardly and thus provides no valve action. The secondary flow that extends through or past bender 452, through secondary flow orifice 460, and secondary flow channel 490 and into diaphragm chamber 492, is allowed to exit diaphragm chamber 492 through a bleed channel 502. Bleed channel 502 is situated to the side of diaphragm 504 within chamber plate 454. Bleed channel 502 allows the flow to exit into outflow channel 476. The bypass valve assembly operates by controlling the amount of fluid allowed into and over diaphragm chamber 492, thus affecting the flex of diaphragm 502. Diaphragm 502 adjusts the position of valve body 478 upwardly or downwardly to cut-off the primary flow of fluid past valve body 478. The primary flow is cut-off when valve body 478 is pushed downwardly, thus restricting the flow through side channels 486. This embodiment is advantageous because less power is needed to move bender 452 since only a secondary flow must be controlled by bender 452. FIGURE 12B illustrates the flow of the secondary fluid. FIGURE 12B illustrates the arrangement with bypass cover 450 removed. FIGURE 12C is an illustration with a cross-section in a position as shown in FIGURE 12A. Attention is now directed to FIGURES 13-19, which illustrate two additional alternate preferred embodiments of a bypass valve arrangement of the present invention in which a fluid and piston dampener, piezoelectric bypass valve and bypass flow channels, and associated electronic circuitry and power supply are arranged longitudinally within a telescoping suspension strut including a stanchion tube and a slide tube. The bypass valve arrangements of the embodiments of FIGURES 13-19 share many features in common with the previously discussed embodiments, in particular the embodiments of FIGURES 8 and 11. The discussion above regarding operation of the present invention, and in particular the action of electronic circuitry to increase or decrease damping forces during certain portions of the compression and rebound strokes of the piston apply equally to the embodiments discussed below, and thus are not repeated to avoid redundancy. Further, those elements of the embodiments illustrated in FIGURES 13-19 that function identically or substantially the same as corresponding features or elements of the previously described embodiments are referred to by the same descriptor, and a detailed description of these is again not repeated to avoid redundancy. Referring to FIGURE 13, a front fork and suspension assembly 610 is illustrated. The front fork and suspension assembly 610 includes a stem 612 that has an upper end receivable within a frame head tube (not shown) and a lower end that supports vertically spaced upper and lower bridge members 614. Each bridge member 614 has a yoke shaped configuration and includes an aperture on either side that receives and is secured to downwardly depending stanchion tubes 616 and 617. Each stanchion tube 616, 617 slidably receives on the exterior of its lower end a slide tube 618. Each slidably coupled stanchion tube 616, 617 and associated slide tube 618 forms one of the telescoping front forks of a bicycle frame. The upper ends of the slide tubes 618 are secured together by another bridge member 620, which is configured in the shape of a downturned U, and each end of which defines a clamp secured about the corresponding slide tube 618. A hub dropout 622 is formed on the lower end of each slide tube 618 for purposes of detachably mounting the hub of a wheel. In the preferred embodiment of FIGURE 13, a spring pack and a dampener are mounted separately within the first and second stanchion tubes 616, 617. Thus the first stanchion tube 616 carries a dampener (FIGURE 14), while the second stanchion tube 617 carries a spring 624 that rides on a shaft 626. The shaft 626 can be secured to either the stanchion tube 617 or the corresponding slide tube 618, and the spring 624 is compressed between stops (not shown). The spring 624 may be alternately mounted, such as without a shaft 626, or on the outside of the stanchion tube 617. The spring 624 provides shock absorption which is dampened by a dampener (FIGURE 14) received within the opposite stanchion tube 616, as shall be described with reference to FIGURES 14-16, and also provides rebound force for the dampener. The two stanchion tubes 616 are rigidly coupled by the bridge members 614, and are further stabilized by the bridge member 620 that rigidly couples the slide tubes 618, such that balanced shock absorption and dampening occurs. While the preferred embodiment illustrates a spring mounted on a first stanchion tube and a dampener mounted on a second stanchion tube, it should be apparent that the present invention is well suited for other arrangements, such as a spring and dampener mounted within each stanchion tube, or a spring and dampener combination mounted in only one stanchion tube. Further, the spring could be mounted in the slide tube 618 associated with the stanchion tube 616. Likewise, while the front fork and suspension assembly 610 illustrated in FIGURE 13 is for the front suspension of a bicycle, the dampener embodiments illustrated in FIGURES 14-19 for use therein should be understood to be equally well suited for use in rear suspensions, and for other vehicles, such as motorcycles. Referring to FIGURE 14, all components of the dampener 628 of the embodiment of FIGURE 13 are mounted within the stanchion tube 616 and corresponding slide tube 618. The components are mounted linearly along a common longitudinal axis of the stanchion tube 616 and slide tube 618. The inner surface of the upper end of the slide tube 618 slidably receives the lower end portion 630 of the stanchion tube 616. An annular seal assembly 632 is mounted within the upper end of the slide tube 618 to prevent debris from lodging therebetween, and includes an oil seal 634 and scraper seal 636, as shown in FIGURE 15. Additional annular bushings 638 are received between mating surfaces of the lower end portion 630 and the slide tube 618, as shown in FIGURES 15 and 16. Referring to FIGURES 14-16, a tubular hydraulic fluid sleeve 640 is closely and coaxially received within the lower end portion 630 of the stanchion tube 616. The hydraulic fluid sleeve 640 is secured, such as by a threaded engagement or spring clip, or otherwise secured so that its longitudinal position within the stanchion tubes 616 is fixed. First and second annular seals 642, such as O-ring seals, are mounted on the exterior of the lower end, and adjacent the upper end, of the hydraulic fluid sleeve 640, and create a seal against the inner surface of the lower end portion 630 of the stanchion tube 616. The outer surface of the hydraulic fluid sleeve 640 is machined, cast or otherwise formed to define a reduced diameter portion 644 between the annular seals 642. An annular space is thus defined between the exterior of the hydraulic fluid sleeve 640 and the interior of the lower end portion 630 of the stanchion tube 616, to form a bypass flow channel 646, the purpose of which will be described subsequently. The bypass flow channel 646 extends longitudinally, surrounds the hydraulic fluid sleeve 640, and extends the majority of the length of the hydraulic fluid sleeve 640 between the annular seals 642. The interior of the hydraulic fluid sleeve 640 defines a hydraulic chamber 648 and a gas chamber 650, which are separated by a longitudinally floating chamber seal 652. In the preferred embodiment, the hydraulic chamber 648 receives a first fluid, preferably a hydraulic oil, while the gas chamber 650 receives a second, compressible fluid, such as nitrogen gas, air or other inert gas. The chamber seal 652 sealingly engages with the interior of the hydraulic sleeve 640, and slides upwardly or downwardly depending on pressure differentials exerted thereon. A piston shaft 654 is secured to the bottom of the interior of the slide tube 618, and projects centrally and upwardly therefrom. The piston shaft 654 carries on its upper end a piston assembly 656, which is slidably received within the hydraulic chamber 648 in the interior of the hydraulic fluid sleeve 640. The piston shaft 654 and the piston assembly 656 are suitably constructed identically to the previously described piston 186 and shaft 148 of the embodiment of FIGURE 8, except that a magnet is not mounted on the piston, being mounted elsewhere as described below. Thus briefly the piston shaft 654 includes an internal adjustment rod 658, adjustable by either disassembling the slide tube and stanchion tube, or alternately by adjusting an externally mounted adjuster such as a hexagonally keyed activator (not shown) extending from the lower end of the slide tube. The piston assembly 656 includes a piston 660 including longitudinal compression passages 662 and rebound passages (not shown), flow through which is modulated by compression shim washers 664 and rebound shim washers 666, respectively, all of which are retained by an axially secured nut 668. The flow of fluid from one side to the other of the piston 660 on the compression and rebound strokes is dampened by fluid flow restrictions through the compression and rebound passages, as modulated by the shim washers. Additional adjustable dampening is provided by way of a responsive bypass valve 670, best illustrated in FIGURE 15. A cylindrical valve platform 672 is secured within a recessed upper portion of the upper end of the hydraulic fluid sleeve 640. The valve platform 672 is secured in position by a spring clip 674, and is sealed at each end by first and second seals 676, such as O-ring seals, received on the exterior surface of the valve platform 672. The valve platform 672 is thus longitudinally aligned on the common longitudinal axis of the stanchion tube 616, and is disposed approximately midway within the length of the stanchion tube 616. One radial side of the valve platform 672 is recessed between the seals 676 to enable mounting of the remaining components of the responsive valve assembly 670. A longitudinally extending inlet bore 678 extends from a lower face of the valve platform 672, along an axis that is parallel to but offset from the central axis of the valve platform 672, approximately halfway into the length of the valve platform 672. The inlet bore 678 is offset on the opposite side of the recessed portion of the valve platform 672. A radial bore 680 is formed transversely through the valve platform 672, from the recessed side to connect with the upper end of the inlet bore 678. The inlet bore 678 and radial bore 680 thus define a fluid flow path from the lower surface of the valve platform 672 to the recessed side of the valve platform 672. Referring still to FIGURE 15, the chamber seal 652 includes on its lower side a central recess 682. A longitudinal aperture is formed through the remaining portion of the chamber seal 652, extending from the bottom of the recess 682 to the upper surface of the chamber seal 652, along an axis that is offset radially from the longitudinal axis of the chamber seal 652 and which is aligned with a longitudinal axis of the inlet bore 678 within the valve platform 672. An extension tube 684 has a lower end that is press fit or otherwise secured within this aperture of the chamber seal 652, and an upper end that is slidably received within the longitudinal inlet bore 678 of the valve platform 672. The extension tube 684 thus passes completely through the nitrogen gas chamber 650. An annular seal 686 is disposed within an annular recess formed about the lower end of the longitudinal inlet bore 678, to create a gas tight slidable seal with the extension tube 684. As the chamber seal 652 floats upwardly and downwardly during compression and decompression of the nitrogen gas within the gas chamber 650, the extension tube 684 remains in sliding sealed engagement within the inlet bore 678 of the valve platform 672. The extension tube 684 defines a hydraulic fluid flow path from the hydraulic chamber 648, through the chamber seal 652 and through the extension tube 684, into the inlet bore 678 of the valve platform 672. This arrangement thus provides for longitudinal passage of hydraulic fluid through the gas chamber 650 to the responsive valve assembly 670 without commingling of hydraulic fluid and gas. A longitudinal valve plate 688 is secured to the recessed side of the valve platform 672. The valve plate 688 has a recessed inner surface that cooperatively defines a cavity 690 with the recess surface of the valve platform 672, into which the radial bore 680 opens. The cavity 690 is bordered by a rim defined on the inside of the valve plate 688, which compresses a gasket against the valve plateform 672. The gasket includes a flap like extension that overlies the radial bore 680, and serves as a one way valve, which prevents backflow through the radial bore 680. The valve plate 688 also includes an annular valve guide 692 that projects radially outward from a lower portion of the valve plate 688, and which is oriented orthogonally to the longitudinal axis of the hydraulic fluid sleeve 640. The interior of the annular valve guide 692 slidably and closely receives a hollow cylindrical valve member 694. The valve member 694 has a relatively thin tubular wall. The inner facing end of the cylindrical valve member 694 is internally chamfered, presenting a knife-like edge that selectively abuts the recessed surface of the valve platform 672. When the valve member 694 is in a position such that it abuts the valve platform 672, the valve member 694 blocks the flow of hydraulic fluid, which enters through the inlet bore 678 into the cavity 690, from passing through the valve plate 688. However, when the valve member 694 is deflected radially outward, away from the valve platform 672 as shall be subsequently described, a space is created between the valve member 694 and the recessed surface of the valve platform 672, as illustrated in FIGURE 15. Hydraulic fluid can then flow from the cavity 690 and pass through the hollow interior of the valve member 694, flowing into a chamber 696 defined between the recessed side of the valve platform 672 and the inner wall of the hydraulic fluid sleeve 640. A radial aperture 698 is defined in the wall of the hydraulic fluid sleeve 640, below the uppermost seal 642, and provides a fluid path from the chamber 696 to the bypass flow channel 646 defined between the hydraulic fluid sleeve 640 and the interior of the extension tube 616. Thus, depending on the positioning of the valve member 694, hydraulic fluid can be selectively permitted to flow from the hydraulic chamber 648, through the extension tube 684, through the passages formed within the valve platform 672, through the thusly positioned valve member 694, out through the cavity 690 and aperture 698, and into the bypass flow channel 646, as indicated by the directional flow arrows shown in FIGURE 15. The hydraulic fluid then flows downwardly around the outer reduced diameter surface 644 of the hydraulic fluid sleeve 640 along the bypass flow channel 646. Referring to FIGURE 16, at the lowermost extremity of the bypass flow channel 646, several return apertures 700 are formed radially through the lower portion of the hydraulic fluid sleeve 640, above the annular seal 642. Hydraulic fluid thus passes from the bypass flow channel 646, through the return apertures 700, and into the hydraulic chamber 648 on the backside, i.e., lowermost side of the piston 660. This thus completes bypass flow of hydraulic fluid around the piston 660 when a lesser degree of dampening is desired. This return flow is indicated by the directional flow arrows shown in FIGURE 16. Referring still to FIGURES 15 and 16, positioning of the valve member 694, and thus control of hydraulic fluid through the bypass flow channel 646, is controlled by a responsive valve component. In the preferred embodiment of FIGURE 15, the responsive valve component is a piezoelectric bender 702. The piezoelectric bender 702 is constructed and operates similarly to the bender 252 of the previously described embodiment of FIGURE 8. Referring still to FIGURE 15, the bender 702 is mounted by a clamp 704 secured by a bolt or other fastener to the uppermost end of the valve plate 688. The bender 702 thus extends downwardly and parallel to the valve plate 688, and is oriented parallel to the longitudinal axis of the stanchion tube 616. The piezoelectric bender 702 has a width that is slightly less than that of the valve plate 688. A longitudinal recess is formed across the width of the outer surface of the valve plate 688, between the clamp 704 and the annular valve guide 692, such that the bender 702 in this region is spaced apart from the outer surface of the valve plate 688. This thus permits hydraulic fluid within the chamber 696 to surround all sides of the bender 702, preventing differential fluid pressure from being inserted thereon. The lowermost tip of the bender 702 is engaged with the valve member 694. Specifically, an aperture 706 is defined through the side of the valve guide 692 facing the bender 702. The valve member 694 includes a slot like internally projecting recess 708 in the sidewall thereof, again facing towards the bender 702. The bender 702 extends through the aperture 706 of the valve guide 692, and is received within the recess 708 of the valve member 694. The aperture 706 is wider than the width of the bender 702 such that the bender 702 can move inwardly and outwardly, i.e., in a direction transverse to its length, within the aperture 706. When power is provided to the bender 702 to cause it to flex, in the manner previously described with regard to earlier embodiments, the valve member 694 is caused to move along its longitudinal axis, i.e., orthogonally relative to the longitudinal axis of the stanchion tube 616. This flexure of the bender 702 thus can move the valve member 694 selectively between a closed position in which the valve member 694 is biased against the valve platform 672, and an open position, as shown in FIGURE 15, in which the valve member 694 is spaced away from the valve platform 672 to permit hydraulic fluid flow therethrough for bypass flow. Attention is now directed to FIGURES 14 and 15 to describe the mounting of additional components involved in activation of the bender 702. The stanchion tube 616 includes a plurality of cross braces 710 secured at spaced intervals across the width of the interior of the stanchion tube 616, above the valve platform 672. A circuit board 712 on which circuitry required to activate the bender 702 is mounted, is secured to the lowermost and intermediate cross braces 710. A tubular wire guide 714 is secured to the underside of the lowermost cross brace 710, and projects downwardly therefrom. Power leads from the circuit board 712 extend through the wire guides 714, through an aperture 716 formed through the upper end of the valve platform 672, and are connected to the bender 702 adjacent the clamp 704. As in previously described embodiments, the bender 702 is preferably activated in response to either or both of the distance of travel of the piston 660 during compression and rebound of the suspension system, or the velocity of piston 660 travel. To permit sensing of the distance and velocity, the dampener includes a magnet 718 mounted adjacent the upper end of the hydraulic chamber 648 within the bridge member 620, and a sensor 720 mounted a longitudinal distance spaced therefrom on the lowermost cross brace 710. The stanchion tube 616 further provides housing for a power supply such as a battery 722 housed within a battery chamber formed in the upper end of the stanchion tube 616 between the uppermost cross base 710 and a threaded cap 724 secured to the upper end of the stanchion tube 616. The cap 724 permits access to and replacement of the battery 722. Power leads (not shown) extend from the positive and negative poles of the battery 722 to the circuit board 712. Thus, all components of the dampener 628 are housed within the telescoping stanchion tube 616 and slide tube 618, in longitudinal linear array fashion. Alternately, the electronics could be mounted within a recess of the valve platform. As the telescoping strut formed by the stanchion tube 616 and slide tube 618 compresses, dampening is provided both by the hydraulic fluid in the hydraulic chamber 648. Compression of gas within the gas chamber 650 accommodates for a change in fluid chamber volume. The extent of dampening is automatically adjusted during compression and rebound for high frequency or low frequency dampening, by activation of the bender 702 to permit, block or modulate bypass hydraulic fluid flow through the responsive valve assembly 670. Various modifications can be made to the dampener arrangement 628 illustrated in FIGURES 14 through 16, such as those previously described with regard to other embodiments. Thus, other electrical and mechanical sensors can be utilized to activate the responsive valve assembly 670. Other arrangements of benders, such as piston mounted benders and flap-type benders, such as those described in previous embodiments, could also be incorporated into a telescoping suspension in accordance with the present invention. One such additional alternative for a telescoping suspension with responsive bypass dampening is illustrated in FIGURES 17 through 19. FIGURE 17 illustrates a dampener 730 that is similar in many regards to the previously described dampener 628, except that it includes chambers for only a first fluid, e.g., gas or oil, preferably a compressible gas, and includes no hydraulic sleeve, with all components instead being directly mounted within the interior of the stanchion tube 616. Further, a bypass flow channel around the piston is provided centrally through the piston and other components, rather than through an annular passage. The dampener 730 is illustrated in FIGURE 17 with the slide tube 618 removed, but would be included to interact with the stanchion tube 616 the same as in the embodiment of FIGURE 13. Just as in the previously described dampener 628, the dampener 730 includes a piston assembly 732 mounted on a piston shaft 734 that is secured to the slide tube (not shown). The piston assembly 732 is slidably received within a fluid chamber 736 defined within the interior of the lower end of the stanchion tube 616. An annular bearing and seal head assembly 738 and snap retaining ring is received within the lowermost end of the stanchion tube 616 and forms a slidable seal with the piston shaft 734 below the piston assembly 732. The fluid chamber 736 may contain either a compressible or incompressible fluid, and in a preferred embodiment illustrated contains a compressible gas such as air or nitrogen. For use with a gas, as is preferred, the piston preferably includes only rebound passages and rebound shim washers, with all compression stroke gas flow occurring through the bypass channel, to be described. Alternately, compression passages and shims may also be included, particularly if a hydraulic oil is utilized instead of gas. The upper end of the piston shaft 734 includes a central bore 740 (FIGURES 17 and 19) that slidably receives the lowermost end of an extension tube 742. The uppermost end of the extension tube 742 is fixably secured to a valve platform 744, as shall be described subsequently. The extension tube 742 is aligned on the longitudinal axis of the stanchion tube 616 and the piston shaft 734. As the piston shaft 734 and piston assembly 732 carried thereon move upwardly and downwardly during compression and rebound, the extension tube 742 slides through the piston assembly 732 and into the lowermost portion of the central bore 740. Referring to FIGURES 17 and 18, the cylindrical valve platform 744 is secured within and sealed to the interior surface of the stanchion tube 616, above the fluid chamber 736. The valve platform 744 again includes a recessed side 746. An outlet passage 748 is formed centrally into the lowermost side of the valve platform 744, extending upwardly and part way along the recessed side 746. The upper end of the extension tube 742 is press fit or otherwise secured to and sealed within this first passage 748. A fluid flow path is thus formed into the extension tube 742 from the recessed side 746 of the valve platform 744. A second longitudinal inlet passage 750 is defined longitudinally into the bottom side of the valve platform 744, offset radially from the outlet passage 748 on the side opposite of the recessed side 746. The second passage 750 terminates in a radial bypass reservoir bore 752, placing the inlet passage 750 in fluid flow communication with a chamber 745 defined by the recessed side 746. A fluid flow path is thus formed from the fluid chamber 736 through the valve platform 744 to the bypass reservoir chamber 745. Control of fluid flow through the inlet passage 750 and radial bore 752 is controlled by a bender 754. The bender 754 has an upper end mounted by a clamp 756 to the upper end of the valve platform 744. The bender 754 then extends downwardly through a passage 758 defined in the upper end of the valve platform 744, and extends into a secondary chamber 760 defined within the bypass reservoir chamber 745. The secondary chamber 760 is longitudinally oriented and centrally aligned with the outlet passage 748, and communicates at a lower end with the bypass reservoir chamber 745. The radial bore 752 extends into the secondary chamber 760 and is surrounded by a radially projecting, annular valve seat 762 defined by the valve platform 744. The secondary chamber 760 is dimensioned such that fluid which flows through the radial bore 752 can surround the bender 754 on all sides, and also freely communicate with the bypass reservoir chamber 745. Control of the flow of fluid, such as gas, through the inlet passage 750 and radial bore 752 into the chambers 760 and 745 is controlled by automatic adjustment of the biasing of the bender 754 respective to the valve seat 762 and radial bore 752. When power is provided to the bender 754 to flex it away from the valve seat 762, as shown in FIGURE 18, fluid can flow from the fluid chamber 736 through the inlet passage 750 and radial bore 752, into the secondary chamber 760 and the bypass reservoir chamber 745. Fluid is then free to flow down through the outlet passage 748 and into the extension tube 742, as illustrated by the directional flow arrows in FIGURE 18. Referring to FIGURE 19, fluid exits the extension tube 742 into the central bore 740 of the piston shaft 734. From there the fluid is free to continue through radial passages 764 defined in the wall of the piston shaft 734, into an annular chamber 766 surrounding the piston shaft 734, and through outlets 788, back into the fluid chamber 736 below the piston assembly 732. Bypass flow to the back side of the piston is selectively permitted depending on the operation of the bender 754. Operation of the bender 754 is controlled the same as in the previously described embodiment of FIGURE 13 for variable dampening in response to piston travel and/or velocity. Thus, the dampener 730 includes a circuit board 790 and battery 792 mounted on cross braces internally within the stanchion tube 616. Again, modifications of the dampener of FIGURES 17-19 can be made within the scope of the present invention, as previously described with regard to the other embodiments. While the preferred embodiments of the invention have been illustrated and described, it will be appreciated that various changes can be made therein without departing from the spirit and scope of the invention.

Claims: The embodiments of the invention in which an exclusive property or privilege is claimed are defined as follows: 1. A shock absorber for a vehicle comprising: (a) a fluid-filled reservoir; (b) an elongate member having a first end extending partially into said reservoir; (c) a piston secured to the first end of said elongate member and held within said reservoir for being forced through said fluid-filled reservoir to dampen the shock absorber; (d) at least one fluid channel in fluid communication with said reservoir through which fluid is forced when said piston is forced through said reservoir; and (e) a bender valve at least partially blocking the flow of fluid through said fluid channel, said bender valve having a response material embedded within at least a portion thereof; and (f) a power supply and a biasing means attached thereto, said biasing means affecting said response material for biasing the bender valve to affect the flow through said at least one fluid channel. 2. The shock absorber of Claim 1, wherein said at least one fluid channel is disposed through said piston, such that fluid flows through said piston when said piston is forced through said reservoir, and wherein said bender valve seats against said fluid channel to regulate the flow therethrough. 3. The shock absorber of Claim 2, wherein said response material comprises a piezoelectric material, said biasing means comprising said piezoelectric material having said power supply attached across said piezoelectric material for applying a voltage thereacross. 4. The shock absorber of Claim 3, wherein said bender valve is disk shaped, said piezoelectric material being connected to said power supply across the thickness of said piezoelectric material for bending of the disk shaped bender valve in one direction or the other depending on the polarity of the applied voltage. 5. The shock absorber of Claim 4, wherein said piezoelectric material layers are disk shaped within the disk shaped bender valve. 6. The shock absorber of Claim 3, wherein said fluid channel includes a first end into which fluid enters and a second end through which fluid exits as said piston is forced further into said fluid reservoir, wherein said bender valve is disposed adjacent the second end. 7. The shock absorber of Claim 6, wherein said bender valve is disk shaped, said piezoelectric material being connected to said power supply across the thickness of said piezoelectric material for bending of the disk shaped bender valve in one direction or the other depending on the polarity of the applied voltage. 8. The shock absorber of Claim 6, further comprising a sensor to detect shock compression conditions, wherein said sensor includes a means for changing the biasing force of said bender valve against the second end of said fluid channel when said sensor signals predetermined conditions. 9. The shock absorber of Claim 8, wherein said sensor signals said bender valve to at least two discreet biasing forces. 10. The shock absorber of Claim 9, wherein said piezoelectric material in said bender valve includes conductive material on the side faces thereof, the conductive material being connected to the power supply for applying a voltage across said piezoelectric material. 11. The shock absorber of Claim 10, wherein a first of said discrete biasing forces is obtained by applying a voltage across said piezoelectric material in one direction, a second of said biasing forces is obtained by applying a voltage across said piezoelectric material with reverse polarity to the first. 12. The shock absorber of Claim 11, wherein a third biasing force is obtained by applying no voltage across said piezoelectric material. 13. The shock absorber of Claim 1, further comprising a sensor to detect piston displacement within said reservoir, wherein said sensor includes a means for changing the biasing force of said bender valve against the second end of said fluid channel when said sensor detects predetermined displacement conditions. 14. The shock absorber of Claim 13, wherein said sensor detects velocity of said piston relative to said reservoir, said sensor including a means for changing the - biasing force of said bender valve against said fluid channel when said sensor detects predetermined velocity conditions. 15. The shock absorber of Claim 14, wherein said sensor signals said biasing valve to at least two discrete biasing forces. 16. The shock absorber of Claim 15, wherein said response material comprises a piezoelectric material, said biasing means comprising said piezoelectric material having said power supply attached across said piezoelectric material for applying a voltage across said piezoelectric material, wherein a first biasing force is obtained with voltage applied across the piezoelectric material with a first polarity and a second biasing force is obtained no voltage applied across the piezoelectric material. 17. The shock absorber of Claim 16, wherein a third biasing force is obtained with voltage applied across the piezoelectric material with a second polarity opposite to said first polarity. 18. The shock absorber of Claim 14, wherein said sensor increases the biasing force of said bender valve against said fluid channel once said sensor detects both a predetermined displacement and a predetermined velocity of said piston relative to said reservoir. 19. The shock absorber of Claim 13, wherein said vehicle is a bicycle for a rider and wherein said sensor increases the biasing force of said bender valve against said fluid channel in the region of piston displacement due to preload of the shock absorber from the rider's weight. 20. The shock absorber of Claim 19, wherein said sensor decreases the biasing force of said bender valve against said fluid channel once the piston is past the region of displacement due to preload of the shock absorber from the rider's weight. 21. The shock absorber of Claim 13, wherein said response material comprises a piezoelectric material, said biasing means comprising said piezoelectric material having said power supply attached across said piezoelectric material for applying a voltage across said piezoelectric material, wherein said sensor changes the biasing force on the bender valve by changing the applied voltage across the piezoelectric material, and wherein a mid level of biasing force is applied by the bender valve when no voltage is applied across the piezoelectric material. 22. The shock absorber of Claim 1, wherein said response material comprises a piezoelectric material, said biasing means comprising said piezoelectric material having said power supply attached across said piezoelectric material for applying a voltage across said piezoelectric material, wherein said piezoelectric material includes a top face and a bottom face, and wherein said piezoelectric material in said bender valve includes conductive material on the top and bottom faces thereof, the conductive material being connected to the power supply for applying a voltage across said piezoelectric material. 23. The shock absorber of Claim 22, wherein a first biasing force is obtained with voltage applied across the piezoelectric material with a first polarity. 24. The shock absorber of Claim 23, wherein a second biasing force is obtained with voltage applied across the piezoelectric material with a second polarity. 25. The shock absorber of Claim 24, wherein a third biasing force is obtained with no voltage applied across the piezoelectric material. 26. The shock absorber of Claim 25, further comprising a sensor to detect piston displacement and velocity conditions, wherein said sensor includes a means for changing the voltage applied across said piezoelectric material when said sensor detects predetermined conditions. 27. The shock absorber of Claim 23, wherein a second biasing force is obtained with no voltage applied across the piezoelectric material. 28. A dampener for a shock absorber comprising: (a) a fluid reservoir containing fluid; (b) a piston disposed at least partially within said reservoir, said piston being forced at least partially through said reservoir under the force of a shock acting on the shock absorber; (c) a channel in fluid communication with said reservoir through which fluid flows during at least a portion of the stroke of said piston through said reservoir; and (d) a valve at least partially obstructing said channel, said valve including means for changing the flow through said channel based on at least one of the velocity and position of said piston relative to said reservoir. 29. The dampener of Claim 28, wherein said valve includes a bender, said bender moving to affect the flow of fluid through said channel, said bender having a response material embedded within at least a portion thereof. 30. The dampener of Claim 29, wherein said valve includes a flow restriction member and a diaphragm attached to said flow restriction member, said bender being movable to direct a secondary flow of fluid to a side of said diaphragm to move said diaphragm, said diaphragm moving said restriction member, a primary flow of fluid passing through said channel as controlled by said flow restriction member. 31. The dampener of Claim 29, wherein said response material comprises a piezoelectric material, said valve further including a power supply connected to the piezoelectric material for biasing the bender to affect the flow through said channel. 32. The dampener of Claim 31, further comprising a sensor to detect shock compression conditions, wherein said sensor includes a means for changing the biasing force of said bender for flow change when said sensor signals predetermined conditions. 33. The dampener of Claim 29, wherein said valve includes a flow restriction member movable generally transverse to the direction of fluid flow through a portion of said channel adjacent said restriction member. 34. The dampener of Claim 33, wherein said flow restriction member is connected to said bender, movement of said bender controlling said flow restriction member. 35. The dampener of Claim 28, wherein said reservoir is contained by a housing, said channel extending through inflow and outflow openings within said housing. 36. The dampener of Claim 35, wherein said means for changing the flow through said channel includes a bender, movement of said bender affecting the flow - through said channel, said bender having a response material embedded within at least a portion thereof. 37. The dampener of Claim 36, wherein said response material comprises a piezoelectric material, said valve further including a power supply connected to the piezoelectric material for biasing the bender to affect the flow through said channel. 38. The dampener of Claim 35, wherein said inflow opening is located within said housing in a location to be at least partially blocked by said piston upon extensive movement of said piston within said reservoir. 39. The dampener of Claim 38, wherein said outflow opening is located within said housing in a location to be at least partially blocked by said piston during the initial portion of the stroke of said piston. 40. A dampener for a shock absorber including a stanchion tube, comprising: (a) a fluid chamber defined at least partially within the stanchion tube and containing fluid; (b) a piston disposed within the fluid chamber for movement within the fluid chamber under the force of a shock acting on the shock absorber, the piston having a first side and a second side; (c) a bypass channel in fluid communication with the fluid chamber on the first side of the piston and on the second side of the piston, the bypass channel permitting fluid to operably bypass the piston while flowing from the first side of the piston to the second side of the piston; and (d) a valve disposed within the stanchion tube and operable to control the flow of the fluid through the bypass channel. 41. The dampener of Claim 40, wherein the valve includes a bender having a response material embedded within at least a portion thereof, the bender moving during displacement of the piston to control the flow of fluid through the bypass channel. 42. The dampener of Claim 41, wherein the bender is operable to move in response to at least one of the extent of displacement of the piston and the velocity of piston displacement. 43. The dampener of Claim 42, wherein the response material embedded within the bender comprises a piezoelectric material. 44. The dampener of Claim 43, further comprising a sensor that detects a change in the compression of the shock absorber and a power supply electrically connected with the sensor and the piezoelectric material, to supply power to bias the bender in response to the sensor for control of fluid flow through the bypass channel. 45. The dampener of Claim 44, wherein the bender, sensor and power supply are mounted within the stanchion tube. 46. The dampener of Claim 41, wherein the bender coacts with a valve seat defined in the bypass channel. 47. The dampener of Claim 46, further comprising a valve body coupled to the bender, wherein movement of the bender moves the valve body relative to the valve seat to control the flow of fluid through the bypass channel. 48. The dampener of Claim 46, wherein at least a portion of the bypass channel and the valve seat are defined by a valve platform mounted within the stanchion tube. 49. The dampener of Claim 41, wherein the response material embedded within the bender comprises a piezoelectric material. 50. The dampener of Claim 40, further comprising a slide tube coaxially mounted with the stanchion tube for telescoping during compression and rebound of the shock absorber. 51. The dampener of Claim 48, wherein the fluid chamber, piston, bypass channel and valve are all housed within the assembled stanchion tube and slide tube. 52. The dampener of Claim 40, wherein the fluid chamber, piston and valve are disposed along a common longitudinal axis of the stanchion tube. 53. The dampener of Claim 40, further comprising a gas chamber defined at least partially within the stanchion tube and containing a compressible gas, wherein the gas chamber is separated from the fluid chamber by a floating chamber seal. 54. The dampener of Claim 53, wherein at least a portion of the bypass channel passes through the chamber seal. 55. The dampener of Claim 54, wherein the portion of the bypass channel that passes through the chamber seal is defined within an extension tube having a first end perforating the chamber seal and a second end extending through the gas chamber to a valve platform, thereby permitting fluid to flow from the fluid chamber to the valve platform without fluid entering the gas chamber. 56. The dampener of Claim 40, wherein at least a portion of the bypass channel is defined within the stanchion tube and is disposed radially offset from the piston. 57. The dampener of Claim 56, further comprising a hydraulic fluid sleeve received within the stanchion tube, the fluid chamber being defined by an interior of the sleeve, wherein the bypass channel is defined at least partially between an exterior surface of the sleeve and the stanchion tube. 58. The dampener of Claim 40, further comprising a tube mounted within the fluid chamber and having a first end in fluid communication with the valve on the second side of the piston and a second end that is slidably received through an aperture defined in the piston, to permit the flow of fluid from the valve through the tube to the first side of the piston.

Inventors: GIRVIN ROBERT H, JONES EDWARD C JR, VANDERGRIFT JAMES A, GIRVIN, ROBERT, H., JONES, EDWARD, C., JR., VANDERGRIFT, JAMES, A.
Applicants: K2 BIKE INC, K2 BIKE INC.
Application year: 1998
Main classification: F16F
IPC codes: B60G17, B62K25, F16F9