A HIGH EFFICIENCY BICYCLE SUSPENSION

Abstract: A bicycle having an improved suspension system including rotary dampers (54, 73, 100, 125) and composite springs (52, 71, 72, 88, 89, 114, 115). The composite springs (52, 71, 72, 88, 89, 114, 115), which closely control the direction of allowable movement in the suspension, preclude rocking, twisting, or unwanted lateral deflections.

Description: A HIGH EFFICIENCY BICYCLE SUSPENSION The invention relates to a compact, high performance, lightweight, very low static friction suspension system for the seat, handlebar and front and rear wheels of a bicycle or other vehicle with positive geometry control of the suspended motion and utilizing an optional optimized low static friction rotary or linear liquid shock absorber design with variable fluid logic damping or a low static friction variable magnetic damping. The invention as applied to the saddle also allows for convenient vertical, horizontal and angular adjustment of the saddle without effect on the suspension movement itself. The invention as it applies to the handlebar can allow for convenient length and height adjustment of the handlebar. The saddle and handlebar devices further can fit on a standard existing bicycle frame without modification. A less expensive version of the invention also uses low static friction controlled movement, but instead of the rotary or linear hydraulic type shock absorbers uses a combination of springs and elastic polymer devices to control damping and travel of the unit. Similar articulations are applied. Even the suspension without oil damping performs in a superior manner to prior art. The suspension system including spring pivots, with very low static friction fluid logic shock absorbers, could be used to provide improved ride, stability, traction and noise control on all types of vehicles. The early prior art includes many examples of sprung saddles, sprung forks and sprung handlebars from many years back. Typically these consist of metal pivots and rubber, leather or metal spring elements. None of these are currently regarded as high performance or competition suspension devices. Generally the old designs are very heavy compared with the equivalent structure in a modern racing bicycle. More recent prior art includes a saddle suspension composed of a long double fiberglass or carbon fiber cantilever spring with a bonded rubber layer between the springs for damping, with weight of 1020 grams and a linear hydraulic shock absorber with internal spring built into a seat post for suspending the seat with a weight of 812 grams in steel, 625 grams in aluminum and 575 grams in titanium. Except for the one recent design, most seat post suspensions have about 2 to 4 cm of total suspension travel. By way of comparison, a typical high quality mountain bicycle seat post weighs about 250 grams, a road seat post less than 200 grams. So a weight penalty of 300 to 400 grams or more is the cost of a few cm of seat travel. The referred to recent design, although heavier, has substantial seat travel, on the order of about 8 cm (it is hard to tell exactly since there are no travel limits built into it) . Concerning handlebar suspensions currently on the market, there is a handlebar made of a rubber like material. This design flexes in all the wrong directions as well as the right one to a couple of handlebar stem designs which pivot off of the front of the steerer tube and allow the bars to pivot in a forward and downward motion. These use a polymer device, metal spring or combination of the two as both a load supporting spring and damping medium. Typical weights of these stems range from 580 grams for an all titanium model handlebar to 526 grams for a steel stem only. These units have less than 2 cm of usable travel. Some stems weigh 600 to 700 grams and have a travel of about 5 cm. For reference a Klein Mission Control" 1 , sold by the assignee hereof, has a ste length of 135 mm and an assembly weight of 355 grams. Front forks have seen more recent development from the ol Schwinn type leading or trailing pivot designs utilizing a metal spring. The more modern units make use of sliding tub construction, similar to a modern motorcycle. Some of these us dual sliding fork blades, with air or mechanical springs and hydraulic or mechanical friction damping. Some front forks use a sliding fit in the head tube again with an air or mechanical spring and a hydraulic or mechanical friction damping. One recent design incorporates a leading link design with 11 mechanical bushing pivots and a typical linear pressurized air / oil shock absorber unit mounted in front of the head tube. In another fork (using a leading link mechanism), the only mechanism tying the left side with the right is the standard front hub axle. This design requires the use of a relatively heavy front disc brake. In most of the above suspension forks, both high static friction and poor mechanism stiffness (in torsion and cantilever bending modes) result in poor suspension response, loss of steering and directional control loss of pedalling energy during climbing or accelerating. In the units with less static friction, but with poor stiffness, the result feels sort of like riding on a flat or partially deflated front tire, with a vague or sloppy steering response. Most of the front suspension forks have a total travel of less than 5 cm. One of the big problems with bicycle suspensions is the wear life of the suspension unit. The sliding type seal designs work and last well on a car or motorcycle by using a relatively high contact pressure seal. The sliding type seals are much more difficult to make work on a bicycle because the bicycle mass is so much less and the seal and bearing friction must be also proportionately low. For example, if the bicycle is 24 pounds, and the motorcycle is 350 lbs, the bicycle static friction would be .07 or 7% that of the motorcycle proportionately. So far many of th seal and bearing designs have either been short in longevity o have unacceptable static friction or both. One of the most popula forks has required frequent rebuilding due to wear an contamination. One prior art commercial seat suspension has a very sensitiv action in the desired direction, which feels and works very well o small bumps or.repetitive small bumps such as a rocked road. But the lack of adequate damping, geometry control and travel limits cause the rider to lose control under vigorous multiple bump conditions. Also the design does not adequately control the lateral, torsional and angular motions of the saddle, because of its extended flexible beam configuration: Furthermore, this configuration significantly reduces the rider clearance upon dismounting, which is not desirable. Another recent prior art saddle suspension design utilizes a telescoping spring and hydraulic device for energy absorption. This design was found to be very insensitive to the vibration response of the frame. The static friction from the sliding hydraulic seals and the sliding load supporting bushings require a substantial bump to cause any suspension movement. Furthermore, the nature of the sliding mechanism is such that it has considerable fore-aft and side to side play in it. The rider loses the feeling of control of the bike through the saddle. We have determined through testing and evaluation that any suspension or suspension component as relates to a bicycle needs the following features to be truly superior: * Lightweight in total * Lightweight on unsuspended portions * Durable * Wear resistant * Absence of "play" or looseness in the pivots * Rigid or resisting deflection in all directions except the desired direction of suspension travel. * Substantial amount of travel * Smooth, damping method which allows easy travel on small deflections, with increasing resistance as deflection and velocity increase. * Zero or substantially zero static friction, supple feel. * Adjustable damping curves, preferably while in use. * Fluid or damping medium with minimum temperature affects. * Damping resistance curve which increases at a smoothly diminishing rate at high velocities * Simplicity, minimum of components, fasteners and wear surfaces. * Minimize forward energy lost to bumps * Minimize pedalling energy lost by suspension resonance and absorption * Supple suspension at handlebars and seat * Firmer suspension at wheels * Return the tire tread to the ground quickly for best traction, or even better, keep it on the ground with consistent pressure. * Cushion the bike and the rider from stress and shock * Cushion and protect the tires and wheels from impacts. * Do nothing to cause the rider to lose control, steering or balance of the bike. The objects of the invention are to provide an improved lightweight suspension systems and components thereof, particularly useful for bicycles and applicable to all four isolation units in a bicycle suspension system: handlebar, saddle and front and rear wheels. The above and other objects, advantages and features of the invention will become more clear when considered with the following specification and accompanying drawings wherein: FIG. 1 is a diagrammatic illustration of an idealized bicycle suspension system, FIG. 2 is an exploded isometric view of the zero or low friction rotary damper or shock absorber employed in preferred embodiments of the invention, FIG. 3 is a diagrammatic sectional view of the rotary damper shown in Fig. 2, FIGS. 4a, 4b, and 4c are detailed illustrations of a DeLaval nozzle design according to the invention (dimensions given in each embodiment are exemplary), FIGS. 5a, 5b and 5c illustrate a modification of the wiper block flow control passage of Figs . 4a-4d wherein the DeLaval nozzle is provided with sharp orifices, FIGS. 6a f 6b, 6c, 6d and 6e illustrate details of a further modification wherein a vortex diode is incorporated with the DeLaval nozzle, FIGS. 7a, 7b and 7c illustrate details of a further modification wherein a mechanical check valve is incorporated with the DeLaval nozzle, FIG. 8 are curve plots of stroke velocity vs. damping force and illustrate the effect of the fluidic head-type on damping characteristics, FIGS. 9a and 9b illustrate stroke dependent damping characteristics, FIG. 10 illustrates damping force vs. stroke displacement curves for the preferred embodiment, FIG. 11a is an exploded diagrammatic illustration of the handlebar shock isolation system incorporating the invention; FIG. lib is a diagrammatic illustration of the assembled unit; and FIG. lie is a sectional view thereof, FIG. 12 is a diagrammatic illustration of a seat suspension incorporating the invention, FIG. 13 is a diagrammatic illustration of a rear wheel suspension incorporating the invention, and FIG. 14 is a diagrammatic illustration of a front wheel suspension incorporating the invention. DETAILED DESCRIPTION OF THE INVENTION Light weight is important on a bicycle. The complet suspension mechanism installed should not increase the weight of the bicycle appreciably. A top quality all terrain bicycle with full working suspension should weigh under 25 lbs. A top quality road bicycle should weigh in at under 21 lbs. A top quality tandem should weigh in at under 36 lbs (road), 40 lbs (all terrain). According to the invention: * Static friction (the amount of force necessary to begin movement) should be low enough to permit the suspension to work effectively in most all conditions. * The spring rate needs to be optimized to the load, suspension travel, excitation and damping conditions. It is generally desirable to have a relatively low spring rate in the normal working portion of the suspension, with progressively higher rates coming in at the top and bottom portions of the travel, to prevent bottoming out or over-travel under extreme bumps or rebounds. Typically, a suspended load in combination with a spring will oscillate at a resonant frequency F r . For a spring rate K expressed in pounds force per inch of travel and a load M in pounds, ^ , the F r = (K*384/M)'V(2*PI) . For bumps or excitations below this frequency, the load M will exhibit little isolation from the bump. In other words, the load will follow the bump. As the frequency (or speed) of the bump increases to the resonant frequency F r , the load-spring combination begins to resonate with the excitation frequency, traveling farther than the bump height, even to the condition of oscillating wildly out of control if insufficient damping is present. At frequencies (or speeds) higher than the square root of 2 times F r , the load begins to exhibit isolation from the bump. The suspension is working. Although a certain amount of damping is required to control and damp out repeated oscillations, in general, the higher the level of damping, the less isolation from bumps will result. The suspension system on a bicycle has some unique problems. The pedalling motion of the rider can also induce unwanted movement and/or oscillations. The bicyclist will typically pedal between 40 and 100 revolutions per minute, each revolution consisting of two pedal strokes. Thus the cyclist is normally inducing frequencies between 1.3 and 3.3 hertz. In a sprint, the competitive cyclist can spin up to 130 revolutions per minute for a very short duration, which is 4.3 hertz. The bumps, on the other hand, can range from about 5 hertz for a large bump at low speed to more than 50 or 60 hertz for a small bump at high speed. If we were dealing with a strictly mechanical spring system, the minimum F r would need to be substantially larger than 3.3 hertz in order that pedalling would not induce unwanted oscillations or movement of the suspension system. Designing F r substantially higher than 3.3 hertz would put it up into the low frequency portion of the bump range. This is not desirable either. The low frequency bumps could then induce oscillation into the suspension system. If F r were raised to be above the normal operating range of bump frequencies, it would not respond at all to the bumps we are trying to damp. Fortunately, there is a way around the problem. By using multiple suspension actions and both intelligent variable and human damping means, a very efficient and high performance suspension system can be created. For example, with suspension actions at the handlebar and front fork, we can tune the system to greatly reduce the possibility of oscillation. The handlebar is only affected by the weight on the hands, with a relatively small input of pedalling forces. Its F r can be tuned down close to or below the pedalling frequency range without ill effect. The front fork, on the other hand, takes a substantial amount of the pedalling forces, along with the hand forces of the handlebar. It is best tuned to a frequency above the pedalling frequencies. The same type of tuning works for the seat suspension and the rear wheel suspension. The seat will best be tuned to a lower frequency and the rear wheel will use a much stiffer spring rate to achieve a higher frequency. The rear wheel suspension requires special attention. The high compressive forces on the chainstays and particularly on the right chainstay created by the chain tension need to be designed for (see Klein patent #4,621,827). The chain tension varies with the pedal position significantly. Also, particularly when the rider is climbing out of the saddle, but even to some degree when the rider is seated, the rider has a tendency to pounce on each pedal stroke, or load the bike in a downward fashion. This up and down loading is not without purpose. It allows the rider to apply more impulse power to the pedal in its best position, and as the rider creates an impulse of pedal power, he also creates additional down force on the rear wheel, creating additional traction to accept the power impulse. Further, with the power impulse, the bike accelerates on each pedal stroke, also shifting weight to the rear wheel and enhancing rear traction. In a sprint, the rider will shift his or her weight forward over the front wheel, and may still experience the front wheel lifting off of the ground slightly at the peak impulse of each pedal stroke. For a specific gear ratio, road condition, pedal impulse, bike geometry and rider down force impulse, there will be a vector angle such that the chain tension will balance the downloads on the rear wheel. If the suspension linkage to the rear wheel in the equilibrium condition is at that angle, there will be no net suspension movement due to that pedal impulse. If the angle is too flat, the bike will compress, if the angle is too steep, the chain tension will (using some of the rider's energy) lift the bike. Unfortunately, this balance angle does not stay the same for all conditions. It varies directly with the front and rear gears used. It varies with the angle of the road or trail. It varies with the geometry of the bike and with the rider's position on the bike. If the rear spring rate used is very high, then even if the applied force to the linkage is off angle slightly, it will result in very little added deflection. Also, if the pedal or chain forces are low, and the applied force angle is very different than O the linkage, the low forces will result in little added deflection. So the linkage angle is best tuned so as to be in the region of most likely high pedal impulse use, with a relatively high spring rate, in order to minimize lift or dive of the bike under pedal loads and keep to a minimum the pedalling energy absorbed by the rear wheel suspension. The angle of impulse force, measured from the ground, ranges from about 10 to about 22 degrees for most conditions with substantial power output. Road bikes are most likely to be in the 10 to 16 degree range and mountain bikes will more likely be in the 14 to 22 degree range. The optimum linkage angle for a road racing bike is about 13 degrees under normal resting load. The optimum linkage angle for an off-road bike is about 18 degrees under normal resting load. Some of the suspension mountain bikes on the market have achieved angles close to or within the desired range. They have pivoted the rear chainstays in a vertical plane from the seat tube, and in order to clear the tire and the front derailleur, have placed the pivot above or in front of the front derailleur, achieving an angle of about 13 degrees, and 20 to 30 degrees for most others. The prior art bikes with steeper angles, such as at 26 degrees, do not provide suspension under power. Chain tension lifts the bike until the suspension linkage hits its upper stop, locking it out. Most of the pivoted chainstay bikes have poor lateral and torsional rigidity between the head tube and the rear wheel. The invention uses rigid spring pivots to effect an articulation of the rear dropouts without creating loss of torsion and lateral stiffness or play in the frame. Rigid spring pivots are available commercially in a cylindrical package constructed with stainless steel cross springs. The available springs in an appropriate size package for a bicycle are either too weak to take the loads involved or too limited in rotation angle to provide the movement desired or both. The commercial spring pivot takes less JJ and less radial or axial torque load as it is deflected at increasing angles. The invention incorporates spring pivots as part of the structure of the suspension or bike frame. By eliminating the cylindrical package, size and weight are reduced. By starting in the unloaded condition with a spring with small reverse curve, when deflected the spring straightens out and has full radial and axial load capability at its normal working deflection position, or when the radial loading will be at its maximum. A multiple beam spring can be designed with springs of varying reverse curvature to provide essentially constant load capability over a range of deflection. The commercial spring pivots are straight in the unloaded condition where their load carrying capability is highest. The invention also incorporates springs designed with composite fiber construction to provide more energy storage for a given size and weight, and much greater combination of deflection angle and load capability than the commercially available metal spring pivots. Glass fiber composite has about one fourth the modulus of steel, with comparable flexural strength. S-2 glass fiber epoxy composite has flexural strength up to 220 ksi with modulus in the fiber direction of 7,900,000 psi. Compared to the modulus of steel at 30,000,000, the fiberglass can deflect 3.8 times as far as the steel without failure, storing in the process 3.8 times as much energy. Thus, the fiberglass spring more efficient than steel on an energy storage per weight basis. The best metallic spring material may be high strength titanium alloy. It achieves a strength of about 150 ksi with a modulus of about 15-16 ksi and a density about half that of steel. The fiberglass spring as above is only 2.8 times more efficient on an energy storage volume basis, and is more efficient on an energy storage per weight basis. A further advantage can be obtained by utilizing multi modulus composite spring construction. For example, the fiberglass beam when deflected has its outermost layers in the highly stressed condition, and the inner layers are stressed proportionately less as they approach the center of the spring thickness. The inner layers are kind of loafing, and the outer layers are doing most of the work. If we use a higher modulus material such as carbon or boron fiber in the middle plies of the spring, the middle layers will store more deflection energy than the glass they replaced, because of their higher modulus. In addition, some materials such as the carbon fiber, are much lower density than the glass fiber they replaced. By using a multi modulus spring, both the energy storage in a given volume of spring, and also the energy storage per weight can be improved. In the case of the preferred embodiment, this results in a spring with a higher energy storage and a lighter weight over a straight glass fiber spring. The glass fiber, carbon and boron as used in the preferred embodiment are merely indicative of the type of advantage which can be achieved. Other fibers such as Spectra™, Kevlar™, silicon carbide and so forth could also be incorporated to advantage. However, in most cantilever and beam spring designs, the material used must be able to handle compressive and tensile loads. Some of the fiber composite materials are not especially strong in compression, such as the Kevlar and Spectra. According to the invention, when materials are used, they are placed in areas which see predominately tension stress. The springs can be optimized for a particular applied load direction by lengthening and thickening the spring member oriented in the direction of load only. This creates an extra strong spring in a particular direction. This can be used to advantage fo example on the chainstay structure which has a high compression component along the length of the chainstay, due to the high tension loading in the bicycle chain under hard pedalling forces. The strong spring pivot pair linkages are located in back of an slightly above the bottom bracket. The relatively horizontal spring members are much more substantial in order to take th compression stresses of the chainstay than the vertical stabilizing spring members . This is an important feature of the rigid spring pivots, that they can be optimized for a particular stress direction. The spring pivots and chainstay assembly is tucked in out of the way of the riders feet, yet clears the bicycle wheel and chain. The linkage then extends downward and backward toward the rear dropouts at an angle from the center of the forward spring pivot to the center of the rear spring pivot of about 18 degrees with the cyclist sitting on the bike for a mountain bike or about 13 degrees with the cyclist sitting on the bike for a road bike. The dropout is connected to a lightweight seatstay assembly which is connected at the top to either another spring assembly or preferably the optimized rotary shock. In some applications a leaf or beam type spring or springs will provide suitable locating stiffness and geometry control and may be desirable for other reasons such as space limitations, cost to manufacture or assemble or low air resistance (aerodynamics) or aesthetic considerations. This will generally be true when torque forces will not be transferred through the spring but supported in some other manner. For example, if a single direction beam type spring is used for the rear wheel suspension, then each chainstay will have two flex springs oriented so as to flex in the vertical plane, but with the connecting link between them at the appropriate said angle to the ground. The chain side springs and linkage could be made stronger than the non-chain side in order to optimize the structure and minimize weight. The in-plane orientation of the rear wheel would be maintained by a specially designed shock absorber or other spring or linkage assembly up on top of the seat stays, which in turn are rigidly connected to the rear dropouts, keeping the wheel straight with the rest of the frame. There are some problems with composite springs which do not ordinarily show up on normal metal springs . They are the result of the anisotropic nature of the fiber composite material . Composite springs have to be carefully designed so as not to create large delaminating loads between plies. Also, a composite spring with fibers oriented only in the axial or zero degree direction will not have much resistance to side loadings, torsion or other splitting types of failure. If the spring is designed so that it has a significant reverse curvature under a high deflection loading condition, it will be difficult to keep the plies from delaminating. A moderate reverse curvature is used on the preferred embodiment springs in their unloaded condition, at which point they are under little or no stress, such that as load is applied, the springs straighten out and go into forward curvature, which forces the plies into each other. The combination of loading stress and reverse curvature is never high enough to cause delamination of the springs. Where the fiber composite may have a tensile or compressive strength of 250 ksi or higher (for carbon), the interlaminar bonding strength of the matrix resin may be only 15 ksi for example. Another way in which the composite springs are strengthened is by reinforcement in other fiber directions. For example, the spring can be wrapped with a unidirectional fiber 90 degrees to the axis of the spring, to help maintain the springs shape and keep it from splitting apart under varying loads. The 90 degree orientation will not provide any appreciable increase in the energy storage capability of the spring as the fiber is oriented orthogonal to the bending stress . We have also found it useful to incorporate in the very center layers of a composite spring plus and minus 45 degree layers of typically a high modulus high strength carbon fiber material to provide shear strength and stiffness under lateral loadings of the springs. This type of loading is very important in some of the suspension structures utilizing the rigid spring pivot concept. It provides lateral and torsional rigidity for the front fork suspension assembly, the handlebar suspension assembly, the seat suspension assembly and the rear wheel suspension assembly. The shear layer in the center is not critical with respect to 45 degrees, but could range from 30 to 60 degrees without adverse affect. Another feature of the invention as incorporated into the > springs is the method of handling the spring stress at the ends. Typically springs can fail where they are clamped or fastened into a structure due to the high strain in the clamped spring and stress riser resulting from the spring end configuration. For example, the composite spring clamped between two pieces of steel is not a J ιl happy long life spring, unless it is operating well below its maximum stress capabilities. The glass fiber outer layers of the spring are subjected to large strain rates, up to and including the ends. The steel is 3.8 times more rigid than the glass fiber composite, and concentrates and increases the loading on the fiber 15 layer in direct contact with it. This can be buffered by incorporating a thin tapered metal sleeve to reduce the structural stiffness of the metal clamping joint, and further compensated for by bonding the outer layer of glass fiber to the metal structure with a tough but flexible adhesive such as 3M company film 20 adhesive. These measures will reduce the stress concentration of the end joint and improve the life of the spring, but the best method of supporting the spring at its ends is by supporting the highly stressed outer layers with additional fiber material of similar or lower modulus in order to distribute the shear stress 25 between the layers so as not to create any undo stress risers or fail the binding matrix material. The preferred form of this end joint involves a gradual increasing of the fiber layers supporting the basic spring layers, creating a tapered thickened end shape. After sufficient layers of the equal or low modulus fiber material 30 to distribute and buffer the high stress areas of the spring, the remainder of the reinforced end joint can be made with higher modulus material such as carbon fiber or reinforced with metal structure as appropriate. Suspension travel is very important. The suspension devices with one eighth or one quarter inch of real usable travel do no provide any real advantage. The suspension function of the tire is much greater than that. Any suspension travel less than one-half inch for the road or 1 inch for off road or all terrain is not ver desirable. The invention contemplates about one inch of travel fo each member in road configuration except maybe less for the rea wheel and about double that for off road. Damping means is extremely important. Preferably, dampin should be able to be tuned to the particular application and eve to the particular rider. It should be proportioned to the degre of velocity or severity of bump. It should also vary with th position of the suspension. It should be smooth. It should no exhibit static friction. Damping devices disclosed herein hav extremely low friction. In some cases it is advantageous for th damping mechanism to have different damping curves for compressio than rebound. It should be relatively constant with varyin temperature. The damping mechanism should be able to dissipate th energy it absorbs without detrimental temperature rise. Th damping mechanism should be sealed or protected in such a manner s as not to be subject to rapid deterioration by dirt and th environment or leaking of its internal fluid. Optionally th damping means could have a bypass passageway, controlle externally, for adjusting the shock to varying conditions as th rider would like it. For example, when climbing up hill, it is most efficient i the front and rear wheels can move relatively freely in order t follow the ground contour and maintain best traction. If the shoc is damping the movement significantly, it is eating the energ needed to climb with, and not really helping traction either. I the suspension can be freed up so that the shock provides minima or only a small amount of damping, the bike will climb even bette than an unsuspended bike (currently regarded as the best to clim with). Conversely, when descending, the shock absorber is necessary to control the motion and rebound of the suspension action, otherwise, the suspension oscillates and rebounds out of control. The ideal suspension function is to keep the tire in even pressure contact with the ground, or as close to even pressure contact as possible. On the bicycle with a very limited power plant, another function is to keep as much of the forward momentum energy from becoming wasted bump energy as possible. The suspension system must have a restoring force so as to return it to its balanced, static or equilibrium position after being pushed or disturbed. When the wheel rolls onto a bump, at first, the tire deflects and begins to accelerate the wheel and everything attached rigidly to it upwards. The force and duration of the acceleration are determined by the height and slope of the bump, the forward velocity of the bike, the deflection verses force behavior of the tire, and the weight of the wheel and everything attached rigidly to it. The energy to accelerate the tire, wheel, etc. upwards has to come out of the forward momentum of the bicycle. The invention seeks to minimize this energy loss in most cases for a bicycle. The second thing that happens is that the accelerating unsuspended mass attached to the wheel begins to compress the suspension components, and due to the spring rate and compression damping forces, the suspended mass begins to be accelerated by the additional force above the static force in the suspension members. The third event occurs as the bicycle frame and fork are being accelerated upwards by the combination of the increase in suspension spring force due to displacement from neutral position and the damping force due to suspension travel velocity in the frame and fork suspensions. For small or medium displacements the secondary acceleration of the bicycle frame will be much lower than that of the wheels. For large displacements, which reach the travel limits of the suspension device, the acceleration of th bicycle frame will increase with displacement and velocity and will reach the acceleration of the wheels at the upward travel limits of the primary suspension, i.e. when the suspension has bottomed out. The accelerating bicycle frame will, in turn, begin to accelerate the handlebars and saddle through their respective suspensions. Again, the acceleration will be dependent upon the increased spring force from compression of the handlebar and seat springs combined with the damping force generated by the damping mechanism. As these two members will use relatively low spring rates compared to the frame and fork suspensions, they provide a great deal of isolation from the small and medium bumps, and take the harshness out of the larger bumps. Note that the typical bicycle saddle itself is in effect a suspension device. The relatively thin nylon or polyethylene shell with a thin foam cover and light weight wire saddle support frame all contribute to suspension function. The rails, shell and foam all flex under an applied load, even a so called hard racing saddle can flex where the cyclist sits about one half inch under a hard bump condition. This was very evident in a carbon fiber / epoxy saddle shell, which although it was very light, was also much more rigid than a typical racing saddle shell. The carbon fiber shell gave an extremely harsh ride on a standard bicycle and seat post. The first way to reduce the energy loss is to provide a very supple lightweight tire with a large deflection capability. This will reduce the upward accelerating force on a small bump and delay the maximum upward accelerating force on a large bump. The tire selection has to be balanced between suspension function, traction, weight, rolling resistance, and wind resistance. The next way to reduce the energy involved in the upwar motion of the bump is to reduce the mass of the components bein accelerated upwards. The invention at each place does an excellen job of this. In each case, there is the weight of the tire an wheel, and a minimum weight structure and the least number an lightest weight of necessary components rigidly attached to the wheel (in the direction of suspension action). Wherever possible, the unsuspended portion of the bike is made as light as possible, and any component which can be functionally located in a suspended configuration is so located. For instance, on the suspension saddle, the preferred embodiment has the saddle clamping, along with the front to back and tilt adjustments, and the major mass of the suspension springs, and the body and major mass of the rotary shock and its linkage connected to the suspended portion of the device. Only the lightweight seat post and mounting pivots are completely unsuspended in this device. Similarly, in the preferred embodiment suspension handlebar, the major mass of the rotary shock and linkage is mounted up inside the handlebar stem to minimize the unsuspended mass . The tuned suspension system needs to be able to respond at a high speed in order to effectively cushion the rider and return the tire to the ground as quickly as possible. Some of the prior art polymer damped suspension systems seem to have a sluggish response in returning the tire to the ground. The suspension system should allow the suspension motion to occur only in the plane of the bicycle or motorcycle, or in the case of the front wheel or handlebars, only in the plane containing the wheel and the steering axis. The rigidity in all other directions should be very high for a high performance handling and feel. Many prior art suspension systems perform poorly in this respect. The un-suspended portion of the bicycle should be as light as possible, for low energy absorption upon hitting a bump and fast return of the wheel to the ground after clearing the bump. Some prior art suspension systems with cast shock absorber bodies and other heavy hardware attached to the wheel dropouts have a relatively high degree of un-suspended weight. As a result, the tire tends to bounce off the ground and provides poor traction. The invention in the preferred configuration as it relates to the seat comprises a composite cantilever spring, with a separate linkage to a rotary hydraulic fluid logic shock absorber. The combination of spring and rotary shock results in a very low static friction design, exhibiting the desirable properties of the Alsop in this regard, but with automatic fluid controlled variable damping, variable spring rate, positive geometry control and travel limits. The result is more than an order of magnitude improvement in efficiency and rider control. The rotary shock uses anti¬ friction sealed ball bearings for the pivot, and the small diameter rotary seals have greatly reduced friction compared to the sliding seals of a conventional linear shock absorber. Because of the small diameter of the seal surface compared to the relatively long moment arm of the shock actuator, the force required at the end of the lever arm to move the seal on the small diameter shaft is a small fraction of the seal drag at the shaft. This, combined with the very low friction pivots, results in an almost friction-less design. SHOCK ABSORBER DESCRIPTION As indicated earlier, an important part of this invention is the shock absorber. Without a shock absorber, the suspension system becomes much less effective as a vibration and shock isolator over a broad frequency range. At near-resonant conditions, with inadequate damping, the suspension system can actually become an amplifier, introducing large displacements and forces to the suspended mass. To avoid this, an energy absorbing device is introduced into the system to smooth out the responses over a broad range of excitation frequencies. A shock absorber is basically a device that dissipaf vibrational energy. This energy dissipation can be a function displacement, velocity, stress, and combinations of these and factors. Typically, the damping forces are generated by the hydraulic action of a fluid passing through an orifice or a series of orifices, usually pressurized by a piston that is activated by the displacement of the suspension system. For automotive applications where the suspended mass is relatively large and the natural suspension frequency relatively low, good shock isolation can be achieved even with relatively poor damping characteristics . However, for bicycle applications where the rider is more directly coupled to the structure (both in an active and passive sense), the damping characteristics are more critical. One claim of this invention is an advanced shock absorber device for bicycle and other lightweight vehicle applications . The following sections describe this device and discuss how the device can be made to achieve the desired energy absorbing characteristics for application in bicycle suspension systems. DESIRED SHOCK ABSORBER CHARACTERISTICS The bicycle suspension system is basically made of up to four isolation units. These are: the handle-bar, the saddle, and the front and rear wheels. In a fully suspended bicycle, the frame actually "floats" between the rider contact points (handle-bar and saddle) and the wheel isolation units, as illustrated in Figure 1. The degree of isolation is dependant on the number of isolation units active in the system. The quality of ride and the effectiveness of the suspension system in shock isolation will depend on the spring and damping characteristics of the active isolation units. There are several primary design goals for bicycle suspension systems. These design goals may be categorized under five main headings, namely: 1. Vehicle stability and control 2. Riding comfort 3. Minimize structural damage to vehicle 4. Minimize weight and cost 5. Reliability and low maintenance VEHICLE STABILITY AND CONTROL: For competition cycling, stability and control are critical considerations in a suspension design. A key design requirement here is to keep the wheels on the ground (prevent tire hop). It is difficult to accelerate, steer, brake or control the bike in any other manner while the wheels are airborne. The damper is a critical item in the suspension system to accomplish this. Tire "hop" in bicycles can occur from several sources. It can occur from too little or too much damping in the wheel isolation units and it can occur from too little damping in the rider isolation units (or both). To illustrate, consider for the moment the idealized suspension system in Figure 1. Assume that the idealized suspension is completely frictionless (i.e., no dampers in the system) . From a suspension design point of view, the shock loading of a bicycle frame occurs when the front and rear tires encounter a series of bumps in a roadway. Generally, the loading from the front and rear tires do not occur simultaneously but a time lag exists between a bump impact with the front tire and the same bump impacting the rear tire. This time delay is a function of the vehicle speed and the vehicle wheel base (Lwb - Figure 1). Because of this time delay, the general motion of the bicycle frame will be a combined rotational (rocking) and vertical (pogo) action where the frame oscillates between the ground and the rider contact points. Without friction in the system this movement can become dangerously out of control if the speed of the bicycle and the spacing of the bumps are such that the impulse energy occurs at or near a fundamental frequency of the suspension system. In this mode, the wheels will be off the ground a great deal of the time (tire hop) and the control capability of the bike will be extremel compromised. The purpose of the shock absorber is to reduce the oscillatory movement of the frame by dissipating some of the stored energy in the shock isolation units. If the damper units are properly "tuned" the movement of the frame can be minimized thus reducing the tire "hop" problem. However, it is necessary to consider all of the active isolation units for optimum wheel control. For example, adding damping only in the wheel isolation units will help the tire "hop" problem but the frame (plus wheels) can still oscillate undamped between the rider contact springs and the pneumatic tires (which are basically undamped springs). The key point to be raised here is that the ideal damper design must be one that can be "fine- tuned" (adjusted) for optimum wheel control over a given range of vehicle speeds and riding terrains. RIDING COMFORT CONSIDERATIONS: Riding comfort for bicycles and other lightweight vehicles is considerably more limited than for automobiles. The most that can be hoped for in bicycle suspension design is to minimize the acceleration response of the rider for a given riding environment. This can be done by optimizing the spring and damping characteristics of the shock isolation units. Impacts with large bumps as well as the harsh vibrational environment induced by rough road conditions must be considered in the suspension design. Impacts by large bumps are best isolated by large sprin displacements and high damping rates whereas isolation from hig frequency vibrations (much higher than the fundamental frequency of the suspension) is best handled with a small amount of damping. This seemingly conflicting requirement can be accommodated by stroke dependant damping unit, where a small amount of damping i provided for small oscillations (around the equilibrium point) bu progressively higher damping provided for larger oscillations. Ou invention accommodates this requirement. How this is accomplished is discussed in a later section. Another consideration for riding comfort is the suppleness of the suspension during normal, smooth operations. Static friction in a suspension system gives an undesirable rough "feel" to the system. Static friction is generally introduced into the system by damper seals and mechanical tolerances that cause rubbing of adjacent parts. In this invention, steps are taken to minimize static friction. For the rotary damper, discussed later, this is somewhat inherent in the design due to the mechanical advantage of the driving linkage. A linkage with a mechanical advantage of 10, for example, will experience a net reaction load of 1/10 of the static friction load. For linear dampers special low friction seals must be used to minimize the effects of static friction. Our linear damper design is discussed in a later section. STRUCTURAL CONSIDERATIONS: High structural loading of a bicycle frame occurs when the front and/or rear tires impact discontinuities in the roadway. They can also occur from a hard landing following a jump. The detrimental effects of these loadings can be minimized by an experienced rider who can anticipate and react to these conditions. However, there are situations where a cyclist (experienced or not) cannot react quickly enough to prevent overloading of the frame (e.g., rough road at high speeds). In these situations, the frame, handle-bar and fork loads can build rapidly if the bicycle is inadequately suspended. Even if suspended, high frame loads can be introduced if near-resonant conditions exist (with an inadequate amount of damping) or if there is not enough damping in the system to prevent the suspension springs from "bottoming-out" during a hard landing. The damper unit is thus an important force limiting device for suspended bicycle frames. The optimum damper characteristics required for single and multiple bump impacts are not the same. For single impacts, a minimum amount of damping is desirable to allow full excursion of the suspension system without "bottoming" the suspension springs and to allow the springs to return their energy back to the ground on the downhill side of the bump and recover the otherwise lost forward energy. However, for multiple impacts a higher amount of damping is needed to prevent uncontrolled resonance. These requirements point to the need for an adjustable damper unit that can be externally adjusted by the rider "on-the-fly" to accommodate the riding environment. WEIGHT AND COST CONSIDERATIONS FOR BICYCLE SUSPENSION SYSTEMS: Weight and cost are extremely important design considerations for bicycle suspension systems. Important factors here include material selection, fabrication methods and simplicity of design for ease of manufacturing and assembly. DESIGN CONSIDERATIONS FOR RELIABILITY AND LOW MAINTENANCE: The majority of the bicycle suspensions currently on the market are not adequately designed for high reliability and low maintenance. Some of these systems provide a level of shock isolation for a period of time but are unable to withstand the less than ideal off-road conditions involving rough terrains and harsh environmental conditions (mud, water, snow) and the hard, rough handling by the competition cyclist. The shock absorbing units are the most critical parts of the suspension system, from the standpoint of reliability and low maintenance. Linear shocks are susceptible to fluid leakage because of the highly exposed seal surfaces and their tendency to pit over time. Our invention utilizes a rotary damper for the preferred design. Rotary dampers have less tendency to entrap foreign debris and the seal surfaces are much more protected than the linear damper design. As a consequence, the rotary damper is inherently more reliable from the standpoint of fluid containment. Our rotary damper design is discussed in the next section. We also have an improved linear damper concept which will minimize the leakage problem. This damper design is discussed later. THE ROTARY SHOCK ABSORBING DEVICE General Description: The rotary shock absorbing device is the preferred shock absorbing unit for this invention. Figure 2 is an exploded view of the device, showing its key working parts. The rotary shock includes of a housing assembly 20 and 21, a wiper blade unit 22, several "o-ring" seals 23 (3) and two sealed, precision ball bearings 25 and 26. The damper housing 20 and 21 form the oil cavity or chamber 27 when the device is assembled. The left 20 and right 21 halves of the unit are aluminum forgings with some machining required to form the "o-ring" surfaces 24 and the bearing pockets 28. These parts could also be made of reinforced plastic materials reinforced for added weight savings . It should be noted that the geometry of the housing in Figure 2 is for the seat shock absorbing device. Other applications (e.g., handle-bar, front and rear wheel shock isolation units) require a similar housing but with a different exterior geometry to accommodate the specific attachment points. The housing is assembled by installing the wiper blade unit 22, the "o-ring" seals 23 (3) and bonding the right and left sides of the housing using a carbon/epoxy material. A filler hole 29 is provided on the damper housing for filling the device with dampin fluid. The wiper blade unit 22 is the moving part of the damper tha generates the damping force and it is actuated by one or mor shafts 30 and 31 in bearings 25 and 26. The damping force i generated by the wiper unit displacing fluid in front of the blade and forcing the fluid into the lower pressure area behind the blade. This part is an aluminum forging with precision machining required to form the fluidic head 32 and the bearing/seal shafts 30 and 31. The wiper blade unit rotates in two sealed, precision ball bearings 25 and 26. The housing may include a needle valve NV controlled by-pass passage BP may be used for adjustment purposes. This passage may be controlled remotely for active damping control. Needle valve NV can have a knurled handle for grasping between thumb and finger to rotate same. Alternatively, the handle can be in the form of a pinion NVP which is rotated by rack NVR, which is remotely translated by control cable NVC, which extends to a convenient position for the bicyclist. Figure 3 illustrates how the rotary damper works. The figure is a section through the damper housing 20. The wiper or blade unit 22 is shown rotating counter-clockwise, giving a high pressure zone 34 in front of the wiper blade and a low pressure zone 35 behind the blade. The high and low pressure zones set up a flow of fluid through the device in the direction of the arrows. The flow consists of two parts, the primary flow through the fluidic head 32 and a secondary flow as leakage around the remaining parts of the wiper unit (see Figure 3). The amount of leakage is kept to a minimum by a close tolerance on the mating surfaces E-F-G AND E'- F'-G' (Figure 3) and the bottom and top surfaces of the wiper blade (not shown). The primary flow is through the fluidic head, designated by the mating surfaces A-B-C-D AND A'-B'-C'-D' (Figure 3). The net damping moment produced by the rotary damper unit can be expressed as, r r ^ p = PRESS h * J r*dA h - PRESS X * J r*dA x where , M d ^ p = Damping moment (in-lbf) PRESS h = High fluid pressure (psig) PRESSi = Low fluid pressure (psig) dA h = Differential Area, High pressure side (in Λ 2) dA x = Differential Area, Low pressure side (in~2) r = Distance of Differential Area Relative to Axis of Rotation of Wiper Arm (in) The pressure differential in the device (hence, the damping force) is controlled by the configuration of the fluidic head 32 and the geometry of the wiping surface of the housing unit, A-B-C-D (Figure 3) . The fluidic head 32 is an integral part of the wiper blade unit and is created by machining or molding of the wiper blade unit. The purpose of the fluidic head is to control the primary flow of fluid. The fluidic head is basically an arrangement of orifices and/or contoured and ramped surfaces to form the fluid duct connecting the high and low pressure zones of the damper. Four types of fluidic heads are: De Laval nozzle . Sharp edge orifice Vortex diode One-way mechanical check valve Figures 4 thru 7 are design details of these fluidic head types. De Laval Nozzle (Fiσ. 4): The De Laval nozzle is the preferred embodiment of the damper. The wiper blade design for this concept is shown in Figure 4. (The dimensions are merely exemplary in each of the embodiments shown in Figs. 4-7). This is a converging-diverging nozzle that can accommodate both subsonic and supersonic flows in the fluidic head. While compressible or incompressible fluids could be used, the De Laval nozzle used in conjunction with a compressible fluid described later herein, can produce a damping force v.s. velocity curve similar to Curve A in Figure 8. This curve represents the function, Fdamp = C * V Λ n where, C = damping coefficient V = stroke velocity n = velocity exponent In practice, the velocity exponent for De Laval nozzles can be around 0.7. This gives a rather "gentle" damping curve (even for high stroke velocities) due to the built-in force-limiting tendencies of the function. SHARP EDGE ORIFICE (Fig. 5): Complex automotive shock absorbers use one or moj u staged pressure relief valves to attempt to provide a similar type of damping response as the De Laval nozzle. The problem witl using a drilled hole in a piston as the fluid restriction is thai a sharp edged hole in a plate has a velocity exponent of 2 or greater. This means the shock does almost nothing on small bumps, πnd comes in strong on a large bump. Curve B in Figure 8 is characi eristics of this type of damper. Automotive shocks also typically provide more damping on the rebound than on the compression strol e. They use one way check valves to accomplish this. Again, .hey are protecting the shock absorber. While a vehicle may see a ery hard upward impulse, as from a large bump taken at high sj ied, the rebound force is limited to the force the vehicles springs exert on the unsuspended components, and the rebound rate is limit, d by how quickly the springs can accelerate the unsuspended compon. nts back down to the ground. An intermediate type of fluid restriction passage is the long tube with smooth ends. If the flow through the tube is laminar, the pressure velocity curve will be linear where the pressure drop (hence, damping force) is proportional to velocity. Curve F in Figure 8 illustrates this type of damper. The wiper blade design for the sharp-edge orifice concept is shown in Figures 5a, 5b and 5c. Two sharp edge orifices SE1 and SE2 are shown. As discussed above, this device will have pressure related to damping proportional to velocity squared or higher (see Curve B, Figure 8). The sharp edges create turbulence. This type of response will tend to provide nearly undamped motion in small displacements, and extreme damping in large displacements. This type of response by itself is not particularly useful, but used in conjunction with other damping means or controls, it can work to advantage. VORTEX DIODE (Fig. 6 ) '. The vortex diode is a fluidic device that functions as a check value, without moving parts. It uses an induced vortex to check the flow in one direction. Figure 6 shows the wiper blade design for the vortex diode concept. The vortex diode VD cannot stop the flow completely. It offers an increased resistance to flow in one direction. Used in conjunction with a De Laval nozzle, it can provide a means for fine tuning the shock curves in compression verses rebound. Curves E and D of Figure 8 show the anticipated response of a damper having a De Laval nozzle working in parallel with a mechanical check valve or vortex diode. MECHANICAL CHECK VALVE (Fig. 7 ) : A mechanical check valve concept for the wiper blade is show in Figure 7. This concept offers damping in the preferred directio with damping relief or reduction in the opposite direction (check valve open). The size of the orifice can be adjusted to provide appropriate restriction and since the orifice is generally going to be of the sharp edge variety, it will have approximately power of 2 damping response with increasing velocity. Again, used in parallel with the De Laval nozzle, it can be of benefit in fine tuning the rebound verses compression response. PASSIVE DAMPING CONTROL: As indicated earlier in our discussion, damper control is a desirable feature for bicycle suspension systems. For small bumps where the response of the frame is near the equilibrium point, a minimum amount of damping is desired, to maintain a supple "feel" and reduce the amount of forward energy lost. Energy stored in the spring on the up side of a bump can be returned to forward travel if the stored energy can be used to push down on the down side of the bump, re-accelerating the bike. For larger suspension movements (damper stroke) resulting from large bump impacts and near-resonant operations, a greater amount of damping is needed. Passive damping control is achieved by making the damping characteristics stroke dependant. This is accomplished by shaping the wiping surface A-B-C-D (Figure 3) so that the gap between this surface and the fluidic head changes with wiper rotation (stroke). Figure 9a illustrates several embodiments. In this figure, the fluidic head gap is plotted versus the wiper blade rotation. Curve A-B-C, for example, shows one design with the gap increasing toward the center (neutral) position of the damper blade and a smooth transition between the extremes. This configuration gives higher damping rates at the extremes of the stroke and lower damping rates near the neutral position, as indicated by Curve A-B-C in Figure 9b. This is the preferred concept for the preferred embodiment. Figure 10 shows the expected damping force v.s. displacement curve for this design. The opposite effect is illustrated by Curve A'- B'-C in Figure 9a. For this design, the gap is small near the neutral zone and maximum at the extremes. The resulting damping curve is illustrated by Curve A'-B'-C'in Figure 9b. The damping rates are now highest near the neutral point and lowest at the extremes. As one can readily see, virtually an infinite variety of damping characteristics can be designed into the damper unit for passive damping control. Active damping control is also an important optional feature for bicycle suspension systems. An active system is needed to adjust for rider size and/or riding terrain. ACTIVE DAMPING CONTROL: Active damping control can be provided by an adjustment screw or rotary or sliding valve assembly (not shown), manually or electrically operated, located in the shaft of the wiper blade unit or outside of the pressure cavity. The two ports of the valve, regardless of where the valve is situated, are each connected to the two pressure chambers of the pressure cavity, respectively and corresponds to the by-pass BP shown in Fig. 3. In the case of the valve mechanism being contained in the wiper shaft, the two ports could be drilled into the upper and lower faces of the wiper- piston, and angled toward the center of the wiper shaft, where the ports are separated by the adjustable valve assembly. This valve assembly is intended to operate as a bypass system for the De Laval nozzle. The nature of the preferred embodiment is such that the pressure verses velocity curves for the intended ports and valve structure would behave much like the sharp edged orifice with the power of 2 relationship (Curve B, Figure 8). The valve would be closed and the shock forced to operate in the De Laval mode (Curve C, Figure 8) for example for a rough, high speed descent, where shock control of rapid multiple large displacement bumps takes precedence over energy conservation. For climbing, the valve would be open (Curve D, Figure 8) to minimize the energy loss on th relatively small oscillations induced by the riders legs, allowin the springs to return as much energy as possible to the forwar energy. Even with the valve open, a high velocity bump will caus significant shock resistance, as the passageways and sharp edg configuration of the valve and porting will limit the amount o bypass, forcing the De Laval tip to work . Of course the valve ca also be partially closed (Curve E, Figure 8), to give a intermediate response as desired by the rider. Figure 3 is schematic of the damper adjustment assembly. OVER-PRESSURE SAFEGUARD: In the event of an excessive impact, the design of the shoc with the non-contacting wiper assembly allows for an unusua pressure relief device. Unlike a conventional shock absorber where flexible seal devices maintain contact with the sides of th container, under very high internal pressure generated by a extreme impact, the walls of the rotary shock will flex outward creating a larger clearance between the walls and the wiper. Thi in turn will allow for greatly increased leakage and increased flo through the De Laval nozzle which will in turn help to reduce th high internal pressure. APPLICATIONS: The rotary shock absorber may be used effectively in all fou isolation units in a bicycle suspension system, 1) handle-bar, 2 saddle, 3) front and 4) rear wheels. The following describes th various applications . Figures 11A and 11B illustrates the rotary damper in a handl bar shock isolation unit. The unit includes a monolithic composi handle-bar and neck structure 50, handle-bar stem 51, multiple le spring 52, rotary damper 54 and the damper linkage 55. The multiple leaf spring system 52 is comprised of an " spring integral with semicircular mounting base or stem portion 51 The X spring is comprised of two outer legs 52L and 52R, each o which is provided with a mounting arm or pad 52P for securement t the overhanging portion of neck 50N (shown in dotted section) whic also mounts and houses rotary damper assembly 54 and the actuatin linkage system 55 coupled thereto. Linkage system 55 includes pair of arms 55-1 and 55-2 which ends are secured to the outwardl extending shafts of the damper wiper and opposite ends secured t the coupler member 55CM. A link support member 57 has a bifurcate end 58 which is coupled to downwardly depending coupling membe portion 55CP. The base 57B of link support 57 is shaped to next i cavity 51C of stem 51, and has a lower edge which cooperates wit wedge 60 to secure the entire assembly in the steerer tube 61 of bicycle. Stem tightener 59 has bolt hole 59BH through which pas wedge tightener bolts 59WB to engage threaded bores 60B in wedg 60. When these bolts are rotated, they draw the wedge 60 upwardl to lock the assembly in the steerer tube 61 and at the same time draws stem tightener and base 57B in locking relation with stem 5 in head tube 61. In a preferred embodiment, head tube and bearin assembly shown in patent 5,002,297 is used. When a bump i encountered, the X spring 52 is loaded and the linkage 55 operate the rotary damper as described earlier. Figure lie is a partial sectional view of the handleba suspension system. The ends of vertical springs 52L and 52R ar secured (by adhesive or bolting) to the upper wall of neck 50N which is integrally formed with handlebar 50. And the horizonta spring components 52 is similarly secured to the lower wall o hollow neck 50N. Base 51' may include an integrally formed cabl guide CG. Figure 12 illustrates the rotary damper in a seat or saddl shock isolation unit. The saddle shock isolation unit includes th saddle 70, two spring sets 71, 72, the rotary damper 73, the dampe carrier linkage 74, overboard stop 75, the seat stem bracket 76 th seat stem 77, saddle clam 78. Spring 71 is bifurcated having fla spring legs 71A and 71B with pivot ends 71PA and 71PB, eac pivotally coupled to the clevises forward end 76C of seat ste bracket 76. The trailing or aft end of spring 71 includes a rigi saddle clamping area 71CA, one or more rigid bracket members 71BR and rotary damper coupler 71DC. Spring set 72 is formed with (o secured to) seat bracket 76 and has a pair of flat leaf springs 72 and 72B, which are banned in a direction opposite the low i springs 71A and 7IB and has pivot ends 72PA and 72PB which ar pivotally coupled to bracket 71BR. The outwardly extended shaft (30, 31) of the rotary damper 73 are secured to the rotary dampe coupler 71DC. In the illustration, a pair of brackets 71BR wit damper coupler portion 7IDC are formed with or secured to the sea clamp portion 71CA. Portions of the bracket are removed to reduc weight and also can form trademark indicia of the manufacturer The housing for damper 73 is secured to the end of damper linkag 74 with the opposite end of linkage 74 being pivotally connected t the downwardly depending pivot stub 76PS which is integrally forme with seat stem bracket 76. In order to avoid damage to the rotar damper 73 and other components, an overload stop member 79 extend upwardly from seat stem bracket to a position where on the botto of the most vigorous shock, the saddle mounting bracket 78 wil encounter the elastomeric padded upper surface 79US of overloa stop 79US. As shown in Fig. 13a, the rear suspension includes chainstay 80L and 80R, seatstay 81, rear dropout assembly 82, 83, which i formed of composite materials. Top tube 84 is welded to the uppe end of seat tube 85 and down tube 86 is welded or secured to botto bracket shell 87. The left and right chainstays, in thi embodiment, are constituted by fore and aft "X" springs 88, 8 joined by a channel member 90 having a section shown in Fig. 13 As shown in Fig. 13b, the channel has laterally extendi horizontal flat members 91 and 92 coupled to a flat base member 9 by a pair of vertical plate members 94 and 95. The fore "X" sprin section is constituted by extensions of the flat spring members 9 and 92 which are turned downwardly and fastened or adhered to th bottom bracket shell, and flat base spring member 93 is extended i a forward direction and turned upwardly crossing (e.g. forming a "X") between the two downwardly turned flat horizontal flat member 91 and 92 and is fastened to or adhered to the bottom bracket shel 87 and the down tube 85. Preferably, as shown in Fig. 13c, th trailing ends of the members 91, 92 and 93 are formed as a socke 90S to receive seatstay studs 96, 97 which are welded to the botto wheel bracket 87. The aft "X" spring section is similarly formed and secured t or formed with rear dropouts 82, 83. The seat stays 81 ar illustrated as a "U" shaped tubular member secured to rear dropout 82, 83. The "X" springs and channel members are very rigid t forces in a horizontal plane. Forces in the vertical plane ar operativeiy absorbed by action of the "X" springs and the rotar damper. The upper end of the seat stay assembly 81 includes pivot bracket 97 and a rotating damper link 98 has its aft end 9 pivotally connected to pivot bracket 97 and its fore end carryin the housing for rotary damper 100, the operating shafts 30, 3 being secured to clevis 101 which is welded to seat tube 85. Referring now to Fig. 14, a front wheel suspension system i disclosed. A rigid front fork 110 has a steerer tube in head tub 111. Downwardly depending legs 112 and 113 are coupled to th trailing ends of left and right composite spring members 114 an 115 which have wheel dropouts 116 and 117 formed with or secured t the forward ends thereof. A rigid front fork member 118 havin left and right legs 119 and 120 secured to dropouts 116 and 117 respectively, has bridge member 121 with a clevis 122 on th trailing side and a control cable guide 123 on the leading or fron side. A rigid link 124 (having left and right legs 124L and 124R has rotary damper 125 bonded or otherwise secured thereto. Th laterally extending shafts 30 and 31 (Fig. 3) of rotary damper 12 are secured in lugs 128 which are welded to fork 110. Composite springs 114 and 115 are similar. They include for and aft "X" springs 130 and 131 which are joined by an arm membe 132 which has an upper flat component 133 which turn downwardly a each end and a lower flat composite spring component 134 which i turned upwardly forming an "X" with the downwardly turned fla composite spring components 133. The trailing ends of thes components can be shaped into a stud or stub for reception an securement in the lower ends of rigid depending legs 112 and 113 o front fork 110. A similar arrangement can be used in the leadin "X" spring 130 and fork legs 119 and 120. In this arrangement fork 110 is fixed relative to moving fron fork 118. The "X" spring arrangement assures that the onl movement of the wheel relative to the bicycle frame due to a bum in the direction shown by arrow so that the shock energy thereo will not be transmitted to the rider. It is possible to incorporate plural cavities and wipers fo the damper unit. For example, in a double wiper configuration, th smaller cavity would provide progressive fluid resistance along th variable nozzle, while the large cavity would also provide variabl resistance during the compression stroke, but would incorporate one way valve to allow free rebound. Thus, the small cavity wit its distinct variable nozzle profile would be controlling th rebound, while both cavities would be used in controlling th compression stroke. The only sources of static friction in the isolation units ar the small diameter rotary seals in the damper unit. The seals ac at such a small lever arm that the net static friction i negligible. As the seal is rotary, the entrance and wear from dir is much lower than with a sliding linear seal such as on motorcycle front fork shock. This is a problem which has plague many of the bicycle suspension front forks and other suspensio pieces. Shock body incorporating the other components of th suspension, made in aluminum or molded plastic. Dow Corning 20 series silicone oil is compressible and has low viscosity chang with temperature (compared to other fluids). High temperatur resistance is available in viscosities from .65 cs to 100,000 c for virtually unlimited tuning. A preferred embodiment workin range of 50 to 200 cs is envisioned. If body is attached to other structure as mentioned, with goo thermal contact, a very small and light shock unit will be able t take both high forces, and to dissipate a high heat load whe necessary, without damage to the mechanism or fluid. As rotary shock generates no net displacement, there is n extra nitrogen pressure chamber, foam, or spring mechanism neede to take up the displacement as it sweeps, unlike a standard pisto type shock absorber. LINEAR SHOCK A linear shock can incorporate a number of the features of th rotary shock described above. Instead of a sliding seal, it ma utilize a rolling bellows type of diaphragm to contain the workin fluid and prevent contamination and wear without incurring stati friction. The piston and shaft move on linear ball bearing track to greatly reduce static bearing friction in the unit. As th rolling diaphragm is unable to resist high pressure, the unit i comprised of an outer chamber with an air or nitrogen chamber, foa or additional spring loaded rolling bellows to take up th displacement as the shock is traveled. The unit has an interna high pressure cylinder constructed with variable wall inne diameter to allow for different damping levels at differen portions of the stroke, a one way valve to allow higher compressio damping than rebound damping, a piston including one or more of th same features as the rotary shock, including: Dow Corning 200 series silicon oil, compressible fluid, lo viscosity change with temperature, high temperature resistance very low static friction, fluid logic, such as the preferred d laval nozzles, low exponent, fluid amplification, vortex diode, on way mechanical valve, no sliding contact resulting in zero or lo friction. LEAF SPRING The tapered leaf spring is a well known design. It has th advantage that in addition to providing a spring function in particular direction, unlike a conventional coil spring, it ca also assist in controlling motion in additional directions. As th typical cross section of a leaf spring is flat, that is, it is muc wider than it is tall, it is much more rigid in the side directio than in the spring direction. As such it can be used to contro lateral or side motion. The leaf spring can also be used t control motion or provide rigidity along its length, at the sam time. Thus it can provide not only the mechanical energy storag needed but also act as a portion of the articulation of th suspension. They are: light weight, simple design, multipl functions, and high energy capacity. If the tapered leaf spring is made of a composite materia utilizing high strength fibers, it can achieve a much higher energ storage for a given size than a conventional steel spring. Glas fibers oriented longitudinally with the leaf spring and retaine by a high strength matrix material such as epoxy, polyester polycarbonate, nylon (polyamide), or polyimide can substantiall outperform steel. If a spring is laminated with a center core a high modulus, high strength fiber such as boron, silicon carbi or carbon, then covered with glass fiber on the outer layers, i can exhibit even higher properties than the straight glass fib spring. This layering is set up so as to use each type of materi to its best advantage, staying below its elongation limit. T desire is to not stress each type of material beyond its fatig limit. Another consideration is the linear properties of the lea spring. As it is used for a linkage or articulation in th longitudinal direction, the spring properties in that directio should be addressed. One of the advantages of the layering of th different fiber materials has been that the linear properties o the spring can be improved substantially. Most of the energ storage of the spring occurs in the outer glass fiber layers, wit the contribution of the higher modulus core layers such as carbo or boron contributing less than the glass fiber. In the linea direction, however, the core layers of high modulus material do lot more. They can be a very important part of the springs linea stiffness and strength and stability. Carbon is especially stron for its weight in tension and boron is extremely strong and rigi in compression. Due to the composite structure of the preferred embodimen leaf springs, the matrix materials have to be considered ver carefully. A spring design that creates a high level of stres between adjacent layers of fiber in shear or in tension can caus them to separate. If the force between layers is less than th maximum that the matrix bond can hold, or if the stress i compressive in nature, then the spring can achieve the performanc levels predicted by the high properties of the fibers . An important feature of the leaf spring to the invention i that when it is used both as a spring and as an articulatin member, the static friction can be made very low. The spring wil be able to flex with very little hysteresis, and a small diamete pivot on the tip of the spring can provide a very low frictio connection. Because the moment of the static friction of the pivo is very small, especially when compared to the spring length o moment, and the pivot is rotating through only a small angle, th static friction of the pivot can also be negligible. X SPRING PIVOT The X spring pivot incorporated into the preferred embodimen is a modification of the leaf spring. The pivot is different i that it applies cantilever torque to each end of the spring member flexing the spring member in a uniform arc. The longitudina spring member is a flat beam, with reinforced areas at either end In order to keep the spring from moving out of position as it i being subjected to loads, there is at least one additional an usually two additional transverse springs (at approximately a 9 degree angle) to the first one adjacent to one or both sides. Th midpoint and center of all of the springs lie along a straigh line. Each set of springs keeps the other in proper orientation an allows the springs to resist compressive and off angle loads whic would otherwise not be possible. The set of springs allow rotatio essentially about the said straight line, as in a hinge. Th design is inherently rigid in directions other than the rotatin mode, and as there are no moving parts, there is no play or wear t compensate for. The preferred embodiment of the spring pivot also uses th composite type of construction mentioned in the leaf sprin description. The boron and or carbon core with a glass fiber oute layer greatly reinforces this spring against tension an compression loads. A given X spring pivot can be made lighter an more compact out of the preferred composite materials than fo example, titanium or spring steel. In order to resist tension and compression, as well a sideways bending loads to the best extent possible, it is desirabl to create springs such that they are about straight when in th normal level loaded condition, or loaded slightly more than th normal level loaded condition. This means the springs will hav optimum load capability and structural rigidity in the most commo and useful orientation. This in turn means that the springs ar made initially, under zero load, with a small reverse curve, tha is curved into the direction of force. It is an unfortunat property of polymer bonded continuous fiber composites that th interlaminar properties (shear, tension and peel) for a beam mad of sheets of unidirectional plies are a small fraction of th tensile and compressive properties of the composite. For example a unidirectional composite made of carbon epoxy may exhibit tensil strength of 450 ksi, compressive strength of 249 ksi, an interlaminar shear of 14 ksi. Thus if a small radius revers curved spring were to be highly loaded, the forces acting betwee each of the layers would simply tear the layers of the sprin apart. In order for the spring to withstand a high level of load it must be straight or curved in the direction of force. Thi places the inner layers of the spring into compression and th outer radius layers of the spring in tension, which works to hol the spring together. The composite leaf and X spring pivots use in the preferred embodiment have a small amount of reverse curv molded in (large radius) which becomes about straight as the sprin is loaded to normal position. At the low level of loading involve through this deflection, the interlaminar properties are adequate Typically, the maximum dynamic deflection of the composite sprin will be about 3 to 5 times the normal loaded resting deflection. The X spring pivot is most strong when the deflection is relatively low angle. For high angular deflections, the sprin must be made thinner, and the resulting high curvature in th highly deflected spring makes it geometrically less stable i addition to the reduced thickness of the spring plies. As result, the X spring pivot is used where the rotation angle i inversely related to the loads which will be applied to the pivot A highly loaded pivot should not be rotated a large amount, as large rotation pivot should not be highly loaded. Of course, b making the spring plates longer, wider and thicker, the loa bearing capacity of the X spring pivot will be increased for an particular rotation. As the spring pivot acts as both a torsio spring and as a rigid hinge pivot, it makes an excellent functio for articulation of the suspension mechanism. It provides a usefu suspension spring, and since there are no moving, rubbing o sliding parts, the static friction is essentially zero. This is a ideal characteristic for a superior suspension system. With th angular limitations of the X spring pivot, it can also be seen tha relatively long linkages or swing arms should be used to stil provide large suspension travel. It turns out this is just a well, as very short linkages give very non-linear suspensio movement and otherwise complicate suspension design. The development of the integral composite spring and pivot i useful in other area such as: 1) A cantilever brake set (not shown) using the X sprin pivot as both return spring and caliper pivot. The rigid frictionless design will provide a superior, chatter free stoppin action. It will also provide precise return and allow the use o small clearance between the brake pad and rim. Current brakes nee to use a relatively large spring force to overcome the variabl friction in the pivots and still center the brake pads, in additio to the cable friction in the housing. The X spring pivot is lower than the standard pivot, providin a more linear pad travel more perpendicular to the rim contac surface and reducing the tendency for the pads to "dive" or sli underneath the rim as the pads are used and wear occurs. This ne pivot position by itself will reduce the leverage acting on th brake pads. The cantilever arm is envisioned being constructed o lightweight composite material, integrally molded with the X sprin pivot. The arm will extend upward above the top of the tire, an the single actuating cable or other actuator will link the tw cantilever arms together. The net result can be increased leverag over a traditional straddle cable design. In fact, the increase leverage is anticipated to allow use of smaller and lighter typ derailleur cable and housing for the braking system. The key t using the lighter cable is increased leverage and increased cabl travel, coupled with reduced cable tension or force. Of course special brake lever needs to be incorporated in order to increas the cable travel and it could also use the X spring type of pivo for a smooth frictionless operation. The derailleur type of cabl is very desirable because the cable has been designed with a rigi type of housing consisting of essentially linear wire strand imbedded in a plastic material. The plastic material holds th wires in relation to each other and holds the housing shape i place. The essentially (the strands may have a slight spira twist) linear wire strands resist the compressive forces in th cable housing very rigidly, especially compared to the spira wrapped wire housing conventionally used for bicycle brakes. Th linear housing also includes a low friction plastic material line to reduce cable friction and wear. The linear cable and housing i much lighter in weight than conventional spiral wrapped in the sa size cable, and much lighter with the use of smaller cable. For quick release of the wheel, a snug fitting bushing piv in the standard cantilever pivot position with an adjustable inwa stop is used. In normal use, there is no play in the snug bushin and it rests against its inward stop. The bushing is not so sn that the cyclist cannot overcome its friction and after releasi the actuating device, swing the cantilever arm away from the ri providing clearance to remove the wheel and tire. To reinstal the cyclist just pushes the cantilever arm back up against t stop, and reattaches the actuating cable or hydraulic actuat mechanism. There are different ways to attach a cable to these n brakes. 1. Incorporate a housing stop into one brake arm, and exte the cable to the other one. 2. Incorporate a housing stop on the fork, handlebar ste frame, or suspension member and run the cable first to one bra arm or caliper and around a roller or other pivot assembly to t other brake caliper. 3. A conventional straddle cable will work. Either of these first two methods allow for the brakes to be installed in tight fitting places where it is currently difficult to install standard brakes currently. The second one also allows for the bare cable to actuate the brake from an off center position, while still balancing the brake forces. This is especially advantageous in places such as the rear brake on a small frame, where the straddle cable type or U-brake or Cam operated type of brake is running into the seat tube, and the cable cannot be routed through the seat tube because of the seat post inside. The preferred embodiment can come around the side of the seat tube and provide a powerful and balanced design. A different type of spring pivot brake is anticipated for the road version, replacing the traditional side pull type of brake. 2) Derailleurs designed around the X spring pivots can also offer the benefits of frictionless, precise performance. The springs will not be contaminated with dirt or moisture, and will not wear and develop play. Typical derailleurs currently work for about one season or less, before the many pivots wear to a point where the derailleur operation and performance is affected. The current derailleurs, like the brakes, must include sufficient spring force to overcome variable pivot friction, as well as operating the derailleur in the return direction. The X spring derailleur is envisioned as including both the derailleur spring and pivots in a one piece molded composite unit. There will be a hardened metal cage for wear resistance on the front derailleur, and bearing pulleys on the rear. All of these components being o one piece composite construction in the pivot areas, will be muc lighter, more rigid and more accurate than conventional linkages. The rear derailleur will probably still incorporate a conventiona pivot shaft and jockey cage assembly, as the X spring pivots do no easily lend themselves to large angular displacements. Th parallelogram mechanisms using X spring pivots will be designe with longer moment arms than conventional linkages in order t provide more linear movement and smaller angular displacements. While various preferred embodiments of the invention have bee shown and described, it will be appreciated that numerous othe adaptations and modifications of the invention will be readil apparent to those skilled in the art. WHAT IS CLAIMED IS:

Claims: CLAIMS 1. In a bicycle or other lightweight vehicle having a frame a handlebar steering, seat, front and rear ground engaging whee assemblies all attached to said frame of said bicycle, a suspensio unit including a linkage and as a part of said linkage at least on rotary, working fluid-filled shock absorber having an off cente cavity and a rotary shaft and vane element in said cavity so tha as said rotary shaft of the shock absorber is rotated, said van element sweeps the internal cavity causing the working fluid to b displaced through at least one fluid metering gap, orifice or flui logic device, and thus resisting the applied rotary displacemen and means mounting said suspension unit between said frame and a least one of said assemblies. 2. The invention defined in claim 1, said linkage comprisin one or more spring elements supporting the normal load on said sea assembly, for controlling the motion and travel of said seat. 3. The invention defined in claim 1 wherein said linkag includes one or more springs, said one or more springs having spring rate which provides positive centering force to repositio the assembly to an equilibrium position from any other position. 4. The invention defined in claim 3 wherein said linkag comprises pivots and lever arms constructed so as to provide a hig resistance to deflections out of vertical plane through the fron and rear wheel assemblies of the bicycle. 5. The invention defined in claim 1 wherein said rotary shoc absorber has a shaft protruding on both sides of said cavity rotary bearings supporting either side of the shaft, said bearin supported shaft being both the shaft supporting and operating th vane type element in the shock absorber and being one of the rigi pivots aiding in the control of the motion of the assembly an assisting in maintaining a predetermined orientation of th assembly through its suspension travel and keeping the seat fro rocking, twisting or deflecting laterally or in any other way no desirable. 6. The invention defined in claim 2 in which said one or mor spring elements are selected from cantilever or leaf spring types and in which the one or more springs are also acting as one or mor of the lever arms or linkage controlling the displacement of sai assembly. 7. The invention defined in claim 6 in which said one or mor spring elements constitute one or more of the pivots controllin the motion of said assembly. 8. The invention defined in claim 6 in which said one or mor springs are constructed of a high strength composite materia having center and exterior layers and wherein said composit material is selected from the group comprising, fiberglass, hig modulus fiber material, including boron or carbon fiber in th center layer of said spring and a high strength lower modulus fibe material in the exterior layers. 9. The invention defined in claim 7 in which said one or mor springs are constructed of a high strength composite material an wherein said composite material is selected from the grou comprising, fiberglass, high modulus fiber material, includin boron or carbon fiber in the center layer of said spring and a hig strength lower modulus fiber material in the exterior layers. 10. The invention defined in claim 3 wherein the flui metering gap between the walls of the internal cavity and th rotating vane of said rotary shock absorber changes cross sectiona area at different angles of rotation of said vane, in order t change the dynamic resistance of the shock absorber over it stroke. 11. The invention defined in claim 10 wherein the said gap i reduced in the region of the said equilibrium point, increasing i dimension as the vane is rotated away from said equilibrium point 12. The invention defined in claim 10 wherein the said ga decreases in dimension towards the maximum downward deflection o the seat . 13. The invention defined in claim 11 wherein the workin fluid of the shock absorber has significant compressibility and i of the silicone type. 14. A rotary shock absorber having a housing with an interna cavity, a vane type element sweeping said internal cavity an having lateral supporting shafts, anti-friction bearings in sai housing upon which said shafts and vane element pivot, sai internal cavity having a fluid metering gap between the van element and the wall of the cavity which gap varies significantl in dimension over the stroke of said vane. 15. The invention defined in 14 in which said shock absorbe uses a working fluid of compressible silicone type. 16. The invention defined in 15 in which the vane elemen contains a directional fluid device selected from one way reed typ valve, a vortex diode, a fluid amplifier, or a directional nozzle, in order to create a different dynamic resistance in th compression direction of the suspension than in the reboun direction. 17. The invention defined in claim 3 wherein said van element has a pair of laterally extending shafts, two anti-frictio bearings upon in which said shafts rotate, respectively, said off center cavity having wall a fluid metering gap between the van element and the wall of said off-center cavity which fluid meterin gap varies significantly in dimension over the stroke of the vane a working hydraulic fluid in said cavity, said vane element havin a shaft protruding on both sides and rotary bearings supportin said shaft, said shafts being both the shaft supporting means fo said vane and operating the vane type element in the shock absorbe and being one of the rigid pivots aiding in the control of th motion of said assembly and assisting in maintaining a correc orientation of said assembly through its suspension travel an keeping the seat from rocking, twisting or deflecting laterally o in any other way than in a single plane, in which the spring o springs are of the cantilever or leaf spring type, and in which th spring or springs are also acting as one or more of the lever arm or linkage controlling the displacement of the seat, said one o more springs are constructed of a high strength composite materia with a combination of high strength composite materials with a hig modulus fiber material selected from boron and/or carbon fiber i the center layer of the spring and a high strength lower modulu fiber material in the exterior layers. 18. The invention defined in claim 17 wherein said assembl is the seat assembly and incorporating a seat post so as to fi into and be adjustable vertically in a standard bicycle seat tub assembly. 19. The invention defined in claim 3 wherein at least one o said one or more spring elements is an "X" spring. 20. The invention defined in claim 3 wherein said at leas one of said one or more spring elements is a bifurcated flat lea spring. 21. The invention defined in claim 3 wherein said at leas one of said assemblies is a seat assembly and said spring elemen include a pair of flat leaf springs bowed in opposing directions 22. The invention defined in claim 1 wherein said rotar damper includes means for adjusting the rate of displacement o said fluid as said rotary vane sweeps in said cavity. 23. The invention defined in claim 1 wherein said fluid logi device is a De Laval nozzle. 24. A composite bicycle seat spring comprising a rigid bas member and at least a pair of spaced flat springs extendin generally parallel to each other to free ends thereof and a pivote mounting means in each said free end. 25. A bicycle spring comprising a rigid body member and pair of flat spring members extending therefrom, in directions suc that they cross each other to form an "X", said composite fla spring members having free ends adapted to be secured to an input spring loading member. 26. The invention defined in claim 25 wherein said spring is constructed and adapted to preclude rocking, twisting or unwanted lateral deflections. 27. The invention defined in claim 26 wherein said body member is a composite and has a pair of ends and has an "X" spring formed integral with each end. 28. The invention defined in claim 27 wherein said body member is "Z" shaped. 29. The invention defined in claim 27 wherein said body member is "U" shaped with flat composite extensions on each leg of said U-shaped body member. 30. The invention defined in claim 27 wherein said "X" spring is comprised of two or more fiber composite uniform beam flex springs, which are oriented at transverse angles to each other with a line midway between each uniform beam flex spring and in the center of the composite plies in line with each other. 31. The invention defined in claim 30 wherein said angle is between 20 and 160 degrees. 32. The invention defined in claim 30 wherein the width of said one or more springs is made narrow at the location where said springs cross. 33. The invention defined in claim 37 wherein said composite spring has inner layers comprised of carbon fibers, intermediate tension layers selected from carbon and boron fibers and inner compressive layers made from boron fibers. 34. The invention defined in claim 27 wherein said free ends are supported by metal reinforcements. 35. A rotary action shock absorber having a rotary shaft, a casing having one or more partitioned chambers, a wiper piston means attached to the rotating shaft in said one or more chambers, the tip and/or sides of the wiper or wipers, including converging-diverging nozzles. 36. The invention in claim 35 wherein said casing a profil adjacent to the wiper(s) top and sides so as to provide a variabl resistance action dependent on the position and velocity of th wiper with respect to the casing. 37. The invention defined in claim 36 wherein said profile i combination with the wiper tip creates a medium flow area in th static resting and rebound areas of the wiper position, changing t a larger flow area as the suspension mechanism is compressed as i a small bump, and then changing back to a small flow area as th suspension is compressed towards the maximum compression point. 38. For use in a suspension linkage and travel, energ absorption and return, and shock damping device, the sub combination of a cantilever spring and rotary shock absorber. 39. The invention defined in claim 38 wherein th articulation of the cantilever spring or springs constitutes one o more of the linkage or geometry control functions . 40. The invention defined in claim 38 wherein the pivotin axle of the rotary shock or shocks constitutes one or more of th linkage pivots. 41. The invention defined in claim 38 wherein said cantilev spring is integrated with the structure as part of the suspensi and is attached to the case of said rotary shock absorber. 42. The invention defined in claim 38 wherein said cantilev spring acts as one leg or side of a parallelogram or trapezoid linkage and the actuating lever of the rotary shock acts as anoth side allowing a basically pivoting suspension motion whi maintaining essentially parallel or level orientation between t suspended and unsuspended members between one or more of t following: a) the bicycle frame and the seat, b) the bicycle frame and the handlebars, and c) the bicycle frame and one or more of the wheels. 43. The invention defined in claim 38 wherein said cantileve spring acts as one side of a parallelogram or trapezoidal linkag and the actuating lever of the rotary shock acts as the opposit side. 44. The invention defined in claim 38 wherein said spring i made of a composite with small reverse curve in the cantileve spring in the unloaded condition. 45. A saddle suspension system comprising a composit cantilever spring member and a rotary shock absorber for providin a high efficiency, light weight suspension action with a travel o about 1 to 3 inches, and high resistance to lateral movement. 46. The combination of the cross pivot type spring with rotary shock absorber having a pivoting axle to provide suspensio linkage and travel, energy absorption and return, and shoc damping, including: the articulation of the cross spring pivot or pivots as one o more of the linkage or geometry control functions; and the pivoting axle of the rotary shock or shocks as one or mor of the linkage pivots, and where the cross spring pivot i integrated with the structure as part of the suspension, and wher the cross spring pivot acts as one articulating pivot for parallelogram or trapezoidal linkage and the actuating shaft of th rotary shock acts as another articulating pivot thereby allowing basically pivoting suspension motion while maintaining essentiall parallel or level orientation between the suspended and unsuspende members of one or more of the following: a) between the bicycle and the seat, b) between the bicycle and the handlebars, and c) between the bicycle and the front or rear wheel. 47. A seat support assembly for a bicycle, with tubular sea post the lower end of which fitting into and being verticall adjustable in a standard bicycle seat tube, the upper end of whic includes, in combination, a rotary shock absorber and lower sprin support, said rotary shock absorber including a housing having a eccentric cavity, a pivoted shaft mounted on anti-friction bearing in said housing and a vane element rigidly affixed to said pivote shaft and moving in said eccentric cavity, said vane elemen sweeping said eccentric cavity with close fitting surfaces to sai vane element, said cavity containing a viscous damping fluid. 48. The seat support assembly defined in claim 47 includin an overboard stop member secured to and extending upwardly predetermined distance from said seat post. 49. A bicycle having a frame, seat assemblies attached t said frame, front and rear ground engaging wheel assemblie attached to said frame, a steering assembly attached to said fron ground engaging wheel assembly, a suspension unit of a linkage o pivots and lever arms including as a part of the linkage at leas one rotary shock absorber having a fluid-filled cavity and a rotar blade element in said cavity for causing said fluid to be displace from one side of said rotary blade element to the other in substantially friction-free manner to resist any applied rotar displacement and means mounting said suspension unit between sai frame and at least one of said assemblies . 50. The invention defined in claim 49, said assembly bein the seat and including one or more spring elements supporting th normal load on said seat assembly, which also acts as one or mor of said pivots and/or lever arms necessary for controlling th motion and travel of the seat. 51. The invention defined in claim 49 wherein said spring o springs have a spring rate which provides positive centering forc to reposition the assembly at its normal equilibrium position fro any other position. 52. The invention defined in claim 49 wherein said linkag comprises pivots and lever arms constructed so as to provide a hig resistance to deflections out of the fore-aft vertical plane of th bicycle. 53. The invention defined in claim 49 wherein said rotar shock absorber has a shaft protruding on both sides of said cavity rotary bearings supporting either side of the shaft, said bearin supported shaft being both the shaft supporting and operating th vane type element in the shock absorber and being one of the rigi pivots aiding in the control of the motion of the assembly an assisting in maintaining a correct orientation of the assembl through its suspension travel and keeping the seat from rocking twisting or deflecting laterally or in any other way not desirable 54. The invention defined in claim 50 in which one or mor spring elements are selected from cantilever or leaf spring types and in which one or more spring elements are also acting as one o more of the lever arms of a linkage controlling the displacement o said assembly. 55. The invention defined in claim 54 in which the one o more spring elements constitute one or more of the pivot controlling the motion of said assembly. 56. The invention defined in claim 54 in which the one o more spring elements are constructed of a high strength composit material with a high modulus fiber material in the center layer o the spring and a high strength lower modulus fiber material in th exterior layers. 57. The invention defined in claim 55 in which the one o more spring elements are constructed of a a combination of hig strength materials including a high modulus fiber material in th center layer of the spring and a high strength lower modulus fibe material in the exterior layers. 58. The invention defined in claim 49 wherein the flui metering gap between the walls of the internal cavity and th rotating vane of said rotary shock absorber changes cross-sectiona area at different angles of rotation of said vane, in order t change the dynamic resistance of the shock absorber over it stroke. 59. The invention define din claim 58 wherein the said gap is reduced in the region of the same equilibrium point, increasing in dimension as the vane is rotated away from said equilibrium point. 60. The invention defined in claim 56 wherein the said gap decreases in dimension towards the maximum downward deflection of the seat. 61. The invention defined in claim 60 wherein the working fluid of the shock absorber has significant compressibility and is of the silicone type. 62. A low friction shock absorber having a housing with an internal cavity, a fluid sweeping fluidic element in said internal cavity, said fluid sweeping element being dimensioned to move in said cavity without contacting the walls thereof, and means for retaining fluid in said cavity. AMENDED CLAIMS [received by the International Bureau on 14 February 1994 (14.02.94); original claims 1, 3 and 4 replaced by amended 1; other claims unchanged but renumbered accordingly (11 pages)] 1. In a bicycle having a frame, a handlebar steering, seat, front and rear ground engaging wheel assemblies all attached to said frame of said bicycle, a suspension unit including a linkage and as a part of said linkage at least one rotary, working fluid- filled shock absorber having an off center cavity and a rotary shaft and vane element in said cavity so that as said rotary shaft of the shock absorber is rotated relative to said cavity, said vane element sweeps the off-center cavity causing said working fluid to be displaced through at least one fluid control path, and thus resisting the applied rotary displacement and means mounting said suspension unit between said frame and at least one of said assemblies, said linkage comprising pivots and lever arms constructed so as to provide a high resistance to deflections out of a plane through the plane of the bicycle and said linkage including one or more springs, said one or more springs having a spring rate which provides positive centering force to reposition the assembly to an equilibrium position from any other position. 2. The invention defined in claim 1, said linkage comprising one or more spring elements supporting the normal load on said seat assembly, for controlling the motion and travel of said seat. 3. The invention defined in claim 1 wherein said control path is selected from a metering gap, orifice or fluid logic device. 4. The invention defined in claim 1 wherein said rotary shock absorber has a shaft protruding on both sides of said cavity, rotary bearings supporting either side of the shaft, said bearing supported shaft being both the shaft supporting and operating the vane type element in the shock absorber and being one of the rigid pivots aiding in the control of the motion of the assembly and assisting in maintaining a correct orientation of the assembly through its suspension travel and keeping the seat from rocking, twisting or deflecting laterally or in any other way not desirable. 5. The invention defined in claim 1 in which the spring or springs are of the cantilever or leaf spring type, and in which the spring or springs are also acting as one or more of the lever arms or linkage controlling the displacement of said assembly. 6. The invention defined in claim 1 in which the spring constitute one or more of the pivots controlling the motion of said assembly. 7. The invention defined in claim 1 in which the spring or springs are constructed of a high strength composite material such as fiberglass or with a combination of high strength composite materials with a high modulus fiber material (such as boron or carbon fiber) in the center layer of the spring and a high strength lower modulus fiber material (such as fiberglass) in the exterior layers . 8. The invention defined in claim 6 in which the spring or springs are constructed of a high strength composite material such as fiberglass or with a combination of high strength materials with a high modulus fiber material (such as carbon or boron fiber) in the center layer of the spring and a high strength lower modulus fiber material (such as fiberglass) in the exterior layers. 9. The invention defined in claim 1 wherein the fluid metering gap between the walls of the internal cavity and the rotating vane of said rotary shock absorber changes cross sectional area at different angles of rotation of said vane, in order to change the dynamic resistance of the shock absorber over its stroke. 10. The invention defined in claim 9 wherein the said gap is reduced in the region of the said equilibrium point, increasing in dimension as the vane is rotated away from said equilibrium point. 11. The invention defined in claim 7 wherein the said gap also decreases in dimension towards the maximum downward deflection of the seat. 12. The invention defined in claim 10 wherein the working fluid of the shock absorber has significant compressibility and is of the silicone type such as Dow Corning 200. 13. The invention defined in claim 1 wherein said off-center cavity having a fluid metering gap between the vane element and the wall of the cavity which gap varies significantly in dimension over the stroke of said vane. 14. The invention defined in 13 in which said shock absorber uses a working fluid of compressible silicone type. 15. The invention defined in 14 in which the vane element contains a directional fluid device selected from one way reed type valve, a vortex diode, a fluid amplifier, or a directional nozzle, in order to create a different dynamic resistance in the compression direction of the suspension than in the rebound direction. 16. The invention defined in claim 1 wherein said rotary shock absorber having a vane type element sweeping an internal off- center cavity, including a pair of lateral extending shafts, two anti-friction bearings upon in which said shafts rotate, said internal cavity having a fluid metering gap between the vane element and the wall of the cavity which varies significantly in dimension over the stroke of the vane, said shock absorber uses a working hydraulic fluid, said rotary shock absorber has a shaft protruding on both sides, with rotary bearings supporting either side of the shaft, said bearing supported shafts being both the shaft supporting and operating the vane type element in the shock absorber and being one of the rigid pivots aiding in the control of the motion of said assembly and assisting in maintaining a correct orientation of said assembly seat through its suspension travel and keeping the seat from rocking, twisting or deflecting laterally or in any other way than in a fixed plane, in which the spring or springs are of the cantilever or leaf spring type, and in which the spring or springs are also acting as one or more of the lever arms or linkage controlling the displacement of the seat, said spring or springs are constructed of a high strength composite material such as fiberglass or with a combination of high strength composite materials with a high modulus fiber material (selected from boron and/or carbon fiber) in the center layer of the spring and a high strength lower modulus fiber material in the exterior layers. 17. The invention defined in claim 16 wherein said assembly is the seat assembly and incorporating a seat post so as to fit into and be adjustable vertically in a standard bicycle seat tube assembly. 18. The invention defined in claim 1 wherein at least one of said one or more spring elements is an "X" spring. 19. The invention defined in claim 1 wherein said at least one of said one or more spring elements is a bifurcated flat leaf spring. 20. The invention defined in claim 1 wherein said at least one of said assemblies is a seat assembly and said spring element include a pair of flat leaf springs bowed in opposing directions. 21. The invention defined in claim 1 wherein said rotary damper includes means for adjusting the rate of displacement of said fluid as said rotary vane sweeps in said cavity. 22. The invention defined in claim 1 wherein said fluid logic device is a De Laval nozzle. 23. The invention defined in claim 1 wherein said at least one of said assemblies is said seat assembly and includes a composite bicycle seat spring comprising a rigid base member and at least a pair of spaced flat springs extending generally parallel to each other to free ends thereof and a pivoted mounting means in each said free end. 24. The invention defined in claim 1 wherein said one or more springs includes a rigid body member and a pair of composite flat spring members extending therefrom, in directions such that they cross each other to form an "X", said composite flat spring members having free ends adapted to be secured to an input spring loading member. 25. The invention defined in claim 24 wherein said spring is constructed and adapted to preclude rocking, twisting or unwanted lateral deflections. 26. The invention defined in claim 25 wherein said body member is a composite and has a pair of ends and has an "X" spring formed integral with each end. 27. The invention defined in claim 26 wherein said body member is " Z " shaped. 28. The invention defined in claim 26 wherein said body member is "U" shaped with flat composite extensions on each leg of said U-shaped body member. 29. The invention defined in claim 26 wherein said "X" spring is comprised of two or more fiber composite uniform beam flex springs, which are oriented at transverse angles to each other with a line midway between each uniform beam flex spring and in the center of the composite plies in line with each other. 30. The invention defined in claim 29 wherein said angle is between 20 and 160 degrees. 31. The invention defined in claim 29 wherein the width of said one or more springs is made narrow at the location where said springs cross. 32. The invention defined in claim 29 wherein said composite spring has inner layers comprised of carbon fibers, intermediate tension layers selected from carbon and boron fibers and inner compressive layers made from boron fibers. 33. The invention defined in claim 26 wherein said free ends are supported by metal reinforcements. 34. The invention defined in claim 1 wherein said vane element has a tip and sides, and the tip and sides of said vane element including at least one converging-diverging nozzle. 35. The invention in claim 34 wherein said casing has a profile adjacent to the vane element tip and sides so as to provide a variable resistance action dependent on the position and velocity of the wiper with respect to the casing. 36. The invention defined in claim 35 wherein said profile in combination with the vane tip creates a medium flow area in the static resting and rebound areas of the vane position, changing to a larger flow area as the suspension mechanism is compressed as in a small bump, and then changing back to a small flow area as the suspension is compressed towards the maximum compression point. 37. The invention defined in claim 1 wherein said spring is a cantilever spring. 38. The invention defined in claim 37 wherein the articulation of the cantilever spring constitutes one or more of said linkage. 39. The invention defined in claim 37 wherein the pivoting axle of said rotary shock or shocks constitutes one or more of the linkage pivots. 40. The invention defined in claim 37 wherein said cantilever spring is integrated with the structure as part of the suspension and is attached to the case of said rotary shock absorber. 41. The invention defined in claim 37 wherein said cantilever spring acts as one leg or side of a parallelogram or trapezoidal linkage and the actuating lever of the rotary shock acts as another side allowing a basically pivoting suspension motion while maintaining essentially parallel or level orientation between the suspended and unsuspended members between one or more of the following: a) bicycle frame and the seat assembly, b) the bicycle frame and the handlebars assembly, and c) the bicycle frame and one or more of the wheel assemblies. 42. The invention defined in claim 37 wherein said cantilever spring acts as one side of a parallelogram or trapezoidal linkage and the actuating lever of the rotary shock acts as the opposite side. 43. The invention defined in claim 37 wherein said spring is a composite with small reverse curve in the cantilever spring in the unloaded condition. 44. A saddle suspension system where a composite cantilever type spring and a rotary shock absorber are used to provide a high efficiency, light weight suspension action with a travel of about 1 to 3 inches, and high resistance to lateral movement. 45. The invention defined in claim 1 wherein said spring is a cross pivot type spring, said rotary shock absorber having a pivoting axle to provide suspension linkage and travel, energy absorption and return, and shock damping, including: the articulation of said cross spring pivot or pivots as one or more of the linkage or geometry control functions; and the pivoting axle of the rotary shock or shocks as one or more of the linkage pivots, and where the cross spring pivot is integrated with the structure as part of the suspension, and where the cross spring pivot acts as one articulating pivot for a parallelogram or trapezoidal linkage and the actuating shaft of the rotary shock acts as another articulating pivot thereby allowing a basically pivoting suspension motion while maintaining essentially parallel or level orientation between the suspended and unsuspended members of one or more of the following: a) between the bicycle frame and the seat assembly, b) between the bicycle frame and the handlebars assembly, c) between the bicycle frame and the front assembly, and d) between the bicycle frame and the rear wheel assembly. 46. The invention defined in claim 2, said seat assembly including a tubular seat post the lower end of which fitting into and being vertically adjustable in a standard bicycle seat tube of said frame, the upper end of which includes, in combination, said rotary shock absorber and a lower spring support, being rigidly affixed to said pivoted shaft and moving in said off-center cavity, said vane element sweeping said ecdentric cavity with close fitting surfaces to said vane element, said off-center cavity containing a viscous damping fluid. 47. The seat support assembly defined in claim 46 including an overboard stop member secured to and extending upwardly a predetermined distance. 48. A bicycle having a frame, seat assemblies attached to said frame, front and rear ground engaging wheel assemblies attached to said frame, a steering assembly attached to said front ground engaging wheel assembly, a suspension unit comprised of a linkage of pivots and lever arms including as a part of the linkage at least one rotary shock absorber having a fluid-filled cavity and a rotary blade element in said cavity for causing said fluid to be displaced from one side of said rotary blade element to the other in a substantially friction-free manner to resist any applied rotary displacement and means mounting said suspension unit between said frame and at least one of said assemblies , said linkage comprising pivots and lever arms constructed so as to provide a high resistance to deflections out of a plane through the front and rear wheel assemblies of the bicycle and includes one or more springs, said one or more springs having a spring rate which provides positive centering force to reposition the assembly to an equilibrium position from any other position. 49. The invention defined in claim 48, said assembly being the seat and including one or more spring elements supporting the normal load on said seat assembly, which also acts as one or more of said pivots and/or lever arms necessary for controlling the motion and travel of the seat. 50. The invention defined in claim 50 wherein said rotary shock absorber has a shaft protruding on both sides of said cavity, rotary bearings supporting either side of the shaft, said bearing supported shaft being both the shaft supporting and operating the vane type element in the shock absorber and being one of the rigid pivots aiding in the control of the motion of the assembly and assisting in maintaining a correct orientation of the assembly through its suspension travel and keeping the seat from rocking, twisting or deflecting laterally or in any other way not desirable. 51. The invention defined in claim 50 in which the spring o springs are of the cantilever or leaf spring type, and in which th spring or springs are also acting as one or more of the lever arm or linkage controlling the displacement of said assembly. 52. The invention defined in claim 51 in which the sprin constitute one or more of the pivots controlling the motion of sai assembly. 53. The invention defined in claim 51 in which the spring o springs are constructed of a high strength composite material suc as fiberglass or with a combination of high strength composit materials with a high modulus fiber material (such as boron o carbon fiber) in the center layer of the spring and a high strengt lower modulus fiber material (such as fiberglass)) in the exterio layers. 54. The invention define din claim 52 in which the spring o springs are constructed of a high strength composite material suc as fiberglass or with a combination of high strength materials wit a high modulus fiber material (such as carbon or boron fiber) i the center layer of the spring and a high strength lower modulus fiber material (such as fiberglass) in the exterior layers. 55. The invention defined in claim 48 wherein the flui metering gap between the walls of the internal cavity and th rotating vane of said rotary shock absorber changes cross-sectiona area at different angles of rotation of said vane, in order t change the dynamic resistance of the shock absorber over it stroke. 56. The invention define din claim 55 wherein the said gap i reduced in the region of the same equilibrium point, increasing i dimension as the vane is rotated away from said equilibrium point. 57. The invention defined in claim 53 wherein the said gap also decreases in dimension towards the maximum downward deflection of the seat. 58. The invention defined in claim 57 wherein the working fluid of the shock absorber has significant compressibility and is of the silicone type such as Dow Corning 200.

Inventors: KLEIN GARY G, PAULS LONNEY, VOSS DARRELL W, KLEIN, GARY, G., PAULS, LONNEY, VOSS, DARRELL, W.
Applicants: KLEIN BICYCLE CORP, KLEIN BICYCLE CORPORATION
Application year: 1993
Main classification: B62K21
IPC codes: B62J1, B62K21, B62K25, F16F9