The current invention is directed to improvements useful in gas-spring devices and other variable-volume gas-pressurized devices that operate according to the gas spring characteristics (i.e., pressure v. chamber volume) they produce during operation. For purposes of this patent application, all such devices are collectively referred to herein as adjustable-volume gas-pressurized devices. The current invention is especially directed to providing such devices with the ability to have their gas spring curves easily changed by the rider on-the-fly. The current invention is especially suitable for use with, for example:
(a) gas springs used in two-wheeled vehicles, such as: bicycle shock absorbers (e.g. our '144 application), or bicycle suspension forks (e.g. our U.S. Pat. No. 6,592,136); and
b) shock absorbers having a chamber containing a pressurized gas for controlling the pressure on a hydraulic fluid and/or controlling the effect or extent of a pressure-sensitive damping effect, as exemplified by our WO2006/054994.
Just like any other type of spring, gas springs have spring curves that define the force v. deflection characteristic for the spring. In the field of gas springs and especially those used in vehicles, it is well known that it is often advantageous for the gas spring curve of the gas spring to be able to be changed. Accordingly, our '144 application extensively describes the advantages of a gas spring performing according to a gas spring curve selected—by the rider—from a number of different spring curves (i.e., “softer” and “stiffer”). The need for a gas spring to perform according to a gas spring curve selected—by the rider—from a number of different spring curves (i.e., “softer” and “stiffer”) is also generally discussed in the prior art, such as in US Pub 2005/0116399.
It is highly desirable that the gas spring curve of the gas spring should be able to be easily changed by the rider on-the-fly. Typically, for example, in the bicycle arts, a successful “on-the-fly” adjustment should: (1) be able to made without tools; (2) require small controller manipulations (e.g. short angular knob rotations); (3) require low forces/torques to manipulate the controller; and (4) be capable of being made very quickly (for example, in one or two seconds) and without the rider having to stop or dismount.
The prior art includes a number of adjustable-volume gas-pressurized devices that, while capable of being adjusted to provide various gas spring curves, are not capable of, or conducive to, easy on-the-fly adjustment.
For example, a number of adjustable gas spring designs require rotating an adjustment cap against a significant amount of torque for a full 360.degree. or more, to change the gas chamber volume. As examples, see, e.g. Risse Racing (“Remote Adjustable Gas Chamber”); Showa (U.S. Pat. No. 5,346,236 and Showa Advertisement, Mountain Bike 22-23 (June 1994)); Berthold (U.S. Pat. No. 5,957,252); Rockshox (U.S. Pat. No. 6,095,541); and SRAM (US Pub. 2005/0116399). (For completeness, we note here that the rotation adjustment described in SRAM '399, besides changing gas chamber volume, also changes total fork travel.)
Additionally, in the DHX 5® shock absorber made by FOX FACTORY, INC., the assignee of the current invention, adjusting the independent bottom-out resistance, which operates according to a gas spring curve as generally described in paragraphs [0079]-[0080] of our WO2006/054994, requires a significant amount of torque to rotate the control knob.
It is also known to those skilled in the art that by changing the volume of the oil in the damper, the air spring response can be adjusted. See e.g. Showa Advertisement (referred to above) (referring to common prior art practice: “Have you ever changed the oil volume in your suspension? Does it take a great deal of your time?”); Rick Sieman, “Do It Yourself Tech—Dial in Your Own Forks” (www.off-road.com/dirtbike/tech/forks/); “How to Improve the Ride and Suspension Performance of Cruiser Motorcycles” (www.motorcyclecruiser.com/tech/improve_ride_suspension_performance/); “Suspension Tuning Guide—Learning the Lingo” (www.sportrider.com/tech/146.sub.—0006_lingo). With this method, depressurization of the gas spring is required before the oil may be added or removed and then re-pressurization of the gas spring is required before use.
Other methods that require depressurization and re-pressurization of the gas spring during the course of making the spring curve adjustment are: (a) rotating internal parts using an Allen-wrench (e.g. 1998 Rockshox SID); (b) adding a volume spacer (e.g. 1999-2000 Rockshox SID); and (c) re-locating an internal volume plate (Cane Creek AD-10 and AD-12 rear shocks and U.S. Pat. No. 5,775,677).
When a rider has to exert this much effort and labor to make spring curve adjustments, the gas spring curve adjustment cannot be considered an on-the-fly adjustment—no less a practical on-the-fly adjustment.
As described in our '144 application, spring curves in a gas spring can be changed by altering the initial gas chamber volume. Increasing or decreasing the initial gas chamber volume softens or stiffens, respectively, the gas spring curve. The '144 application describes the theory and formulas underlying how varying gas chamber volumes effects spring curves. Note also that gas springs are sometimes referred to air springs because the gas they use is often air.
Selectively placing main and auxiliary gas chambers in fluid communication with each other to alter the total gas volume subject to compression and therefore the gas spring curve of the gas spring has been widely used in various constructions in automobiles (U.S. Pat. Nos. 1,094,567; 4,206,934; 4,534,580; 4,592,540; 4,598,929; 4,613,116; 4,616,811; 4,635,906; 4,651,977; 4,653,735; 4,659,070; 4,697,796; 4,673,171; 4,735,401; 4,746,106; 4,768,758; 4,773,635; 5,915,674; 6,883,810; 6,698,730; 6,708,803; JP61-1135808; DE 10236621; DE 3233160; and DE 4018712). Additionally, in an automotive application, JP61-1135808 teaches that a main chamber may be used in combination with two remote gas chambers to provide for three different spring curves.
However, the bulky, motor driven, electronically controlled, multi-component, and external (to the gas spring housing) devices disclosed in much of the previously mentioned automotive prior art and used to achieve this functionality are not conducive to un-powered devices, compact and lightweight packaging, and/or incorporation into smaller adjustable-volume gas-pressurized devices, such as used in bicycle or other two-wheeled vehicle suspensions.
Indeed, as compared to the automotive solutions described above, there has been much less success in finding innovative ways to provide two-wheeled vehicle riders with the ability to easily and quickly change the gas spring curve of adjustable-volume gas-pressurized devices on-the-fly. Currently used methods remain labor or effort intensive and not are conducive to on-the-fly adjustment. As mentioned above, the most widely used current two-wheel vehicle solutions involve:
1. Rotating an external knob or nut against significant torque, e.g. Showa; Risse Racing; Rockshox ('541); SRAM ('399); Bethold (U.S. Pat. No. 5,957,252); FOX DHX (WO06/054994);
2. Adding or removing oil after depressurization of the gas spring, e.g. various sources mentioned above;
3. Rotating an internal part to increase or decrease the gas chamber size after depressurization of the gas spring and requiring use of an Allen wrench, e.g. 1998 RockShox SID;
4. Adding a “volume spacer” to increase or decrease the gas chamber size after depressurization of the gas spring, e.g., 1999-2000 RockShox SID; and
5. Re-locating an internal ‘Volume Plate’ to increase or decrease the gas chamber size after depressurization of the gas spring, e.g., Creek AD-10 and AD-12 rear shocks (See U.S. Pat. No. 5,775,677).
Accordingly, the current invention, as will be described below, provides very practical and simple ways for two-wheeled vehicle riders to have the ability to easily and quickly change the gas spring curve of adjustable-volume gas-pressurized devices on-the-fly.
Damping Forces v. Spring Forces
Recognizing the difference between spring curves and so-called gas damping is important to an appreciation of the current invention relative to the prior art. Gas damping has been defined in at least one source as a damping force that results from gas being forced through “proper” (i.e., smaller) orifices. See Jack Gieck, Riding on Air: A History of Air Suspension 222 (1999). See also U.S. Pat. No. 5,775,677 (discussing and suggesting using gas as a damping medium). However, Gieck also writes that the idea that a gas flowing through an orifice can be used to create a damping force has generally been a blind alley and that the perceived damping effect can be explained with the theory that the smaller orifices actually temporarily isolate/separate the gas volumes. See Gieck at 222. While on a purely theoretical level, there may be a question as to whether there really is such a thing as true “gas damping”, some in the industry do make reference to and apply such a phenomena. See Rockshox 1998 SID User's Manual (“Air Damping Orifice Adjuster”). Accordingly, if we accept that the term “gas damping” loosely defines a result rather than how that result is achieved, the current invention has widespread applicability, for example in applications:
(a) where large gas-flow orifices that do not introduce a so-called gas damping effect are used, and the gas flows through the valve orifices and from one gas chamber to another with little or no resistance or throttling and virtually instantaneously; or
(b) where smaller orifices that may sometimes be described as introducing a so-called gas damping effect may be preferred.
For purposes of the invention, “instantaneous” is considered on the order of milliseconds. For a typical mountain bike air fork operating under normal conditions, e.g., gas chamber volumes, pressures, and temperatures, a gas flow port on the order of about 0.050″ diameter or larger will achieve a virtually instantaneous flow. A flow of this nature probably would not be considered to introduce a gas damping effect.
On the other hand, under the same conventional conditions, a gas flow port having a diameter of approximately 0.005″, would not result in a virtually instantaneous flow. Rather, it would take, for example, approximately 0.8 seconds for the pressure between the two gas chambers to equalize when such a small flow port is used. For purposes of the invention, a flow that takes “on the order of” 0.8 seconds can be considered to be restricted, throttled and not virtually instantaneous. A flow of this nature probably would be considered to add a gas damping effect.
Therefore, as used herein when describing the various exemplary embodiments of the invention, “fluid communication” means that gas may flow from one gas chamber to another, even if that gas flow is being throttled. “Unrestricted fluid communication” as used in this application means gas flows from one gas chamber to another with little or no resistance or throttling and virtually instantaneously.
Both restricted and unrestricted fluid communication are within the scope of the invention and which is used depends on the specific performance characteristics desired by the user.
Gas Spring Curves, Travel Modes and Compression Ratios
So far, reference has only been made to different gas spring curves. However, as described in the '144 application, the stiffness (gas spring curve) of a gas spring may be associated with “travel modes” and compression ratios. For conciseness and clarity, the extensive background and exemplary calculations provided in the '144 application on these concepts will only be summarized here.
Travel modes, e.g., short travel modes and long travel modes, are generally defined by how far a spring compresses when subjected to a given force. Thus, as described in the '144 application, for a given force, when a gas spring is in short travel mode it compresses less than it would if the gas spring is in long travel mode.
Compression ratio is defined in our '144 application as initial volume of a gas spring (i.e., at full expansion) divided by the final volume of the gas spring (i.e., at full compression). For a given initial pressure, higher compression ratios produce higher pressures at any given travel distance, thus requiring larger forces for compression. Reference should be made to the '144 application for exemplary compression ratio and compressive force calculations.
In the '144 application, the long travel mode is operative and the compression ratio is lowest when the two gas chambers are in fluid communication and the short travel mode is operative and the compression ratio is highest when the two gas chambers are not in fluid communication.
As will be described below, this terminology is applicable to the current invention.
As previously mentioned, the concepts underlying the gas spring curve control valve 20 according to the various exemplary embodiments of the invention have widespread applicability. However, the concepts are especially applicable to bicycle suspension forks (e.g.
Thus,
Gas spring curve control valve 20 includes body portion 25 that may be screwed into open end 11 of housing 10 using threads 21 (
As shown in
Returning to
Focusing now on
Gas spring curve control valve 20 may include ball valves 50a, 50b for controlling fluid communication between the main gas chamber C and the auxiliary gas chambers A1, A2, respectively, by selectively preventing gas flow from the main chamber C into first auxiliary chamber A1 or second auxiliary chamber A2 through the first and second gas flow ports 40, 45, when ball valves 50a, 50b are in their closed positions, or by selectively allowing the gas flow when ball valves 50a, 50b are in their open positions. In
As shown in
A rotor 60 (see also
Hollow tubular portion 25′ of body portion 25 may receive rotor tube 62. Seal 63 (
As shown in
Referring now to
1) As seen in
2) As seen in
3) As shown in
4) As seen in
As we discussed in our '144 application, it is preferable for adjustment knobs to be capable of manipulation quickly and simply by a user, many times during a ride. Therefore, in the '144 application, the adjustment knob needed only ¼ rotation to switch between the softer and stiffer spring curves available with that design. With the current invention, quick and simple manipulation of adjustment knob 67 by a user may be achieved by designing cam 70 such that the complete range of settings for gas spring curve control valve 20 may easily be achieved in less than ½ turn of adjustment knob 67. For example, in the preferred embodiment shown in
These different gas spring curve control valve settings may be summarized as set forth in the table below.
Pressurization of the Gas Spring
As shown in
Basic Method of Use
As described in our '144 application, the gas spring curve of a gas spring is determined by the volume of the gas subject to compression. The larger the volume, the softer the spring and the smaller the volume the stiffer the spring. We now apply this principle to the current invention.
When the lowest spring curve is desired for adjustable-volume gas-pressurized device 1, adjustment knob 67 is set by the user to the setting where both ball valves 50a, 50b are open (
When a stiffer spring curve is desired for adjustable-volume gas-pressurized device 1, adjustment knob 67 is set by the user to the setting where only ball valve 50b is open (
When an even more stiff spring curve is desired for adjustable-volume gas-pressurized device 1, adjustment knob 67 is set by the user to the setting where only ball valve 50a is open (
When the stiffest spring curve is desired for adjustable-volume gas-pressurized device 1, adjustment knob 67 is set by the user to the setting at which both ball valves 50 are closed (
Applying the terminology of the '144 application as described above to this description of an exemplary embodiment of the invention, the first and second settings of gas spring control valve 20 may be associated with long travel applications and the third and fourth settings of gas spring control valve 20 may be associated with short travel applications. Furthermore, as can be seen from Table One, the exemplary compression ratios are smaller in long travel modes.
Additional Feature—Detent Assembly
As shown in
Additional Feature—Remote Control
As described so far, adjuster adjustment knob 67 is manually and directly manipulated by the user at the adjustable-volume gas-pressurized device 1. However, direct and manual manipulation by the user at the adjustable-volume gas-pressurized device 1 is not required to vary the setting of gas spring curve control valve 20. As shown in
(a) an electrical wire 252 for connecting motive source M to an externally positioned electronic remote controller 310;
(b) a mechanical cable 315 for connecting motive source M to an externally positioned mechanical remote controller 310′; and
(c) an electronic controller 330, such as a CPU, receives control signals from one or more sensors 331a-c and sends control signals to motive source M. Sensors 331a-c may detect, such exemplary conditions as, vertical acceleration, speed, and inclination.
In this configuration, body portion 25 includes first and second partitions 35a, 35b that together define three auxiliary gas chambers A1, A2, A3, of progressively larger volumes. Three check balls (
It should be noted here that, although 6 discrete settings are illustrated in
In this embodiment of the invention, first end 25a of body portion 25 has a main gas flow port 350 in fluid communication with first chamber C and ball valves 50a, 50b that are used to control the fluid communication between the main gas chamber C and the auxiliary gas chambers A1, A2.
As with prior embodiments of the invention, the opening and closing of ball valves 50a, 50b results from the rotation of rotor 60 (see other FIGS) and rotor tube 62. Rotor 60 and rotor tube 62 may be rotated by any previously described method (e.g. adjustment knob 67 or motive source M).
In this embodiment, however, rotor tube 62 has a plurality of angularly and/or longitudinally offset detents 360a, 360b on its surface 361.
To open a ball valve 50, rotor 60 is rotated to align a detent 360 with a check ball 51. This alignment allows spring 52 to partially extend and deflect check ball 51 into detent 360 and away from its valve seat/seal 53. Thus, there is two-way gas flow/communication between main gas chamber C and an auxiliary gas chamber, through main gas flow port 350. In
To close a ball valve 50, rotor 60 is rotated such that a detent 360 will not be aligned with a check ball 51. This misalignment results in check ball 51 abutting the surface 361 of rotor tube 62 and being pressed radially into sealing contract with valve seal 53, which may, for example, be an o-ring. Since rotor tube 62 is fabricated from a rigid material such as aluminum, spring 52 will not deflect check ball 51 away from its valve seal 53. Thus, gas flow between main gas chamber C and an auxiliary gas chamber, through main gas flow port 350, is prevented. In
According to this embodiment, detents 360 are aligned on the surface 361 of rotor tube 62 such that, as with the previous embodiments of the invention:
1) in a first setting, both valves are open;
2) in a second setting, one of the two valves is open;
3) in a third setting, the previously open valve is closed and the other valve is open; and
4) in a fourth setting, both valves are closed.
As with previous embodiments, more than two auxiliary gas chambers may be provided and less than one full rotation of rotor 60 by the rider allows access to all available gas spring curves. Furthermore, as with previous exemplary embodiments, both ball valves 50 should be open when the device is pressurized.
Finally, as opposed to the previous exemplary embodiments of the invention, in this exemplary embodiment, the pressure in the main gas chamber C tends to unseat check balls 51. Also, for completeness, we note here that this embodiment requires somewhat closer manufacturing tolerances than previous embodiments, in order to provide proper operation and sealing of the balls 51 with the seals 53. Whereas in the previous embodiments sealing in the valve-closed position was ensured by a positive pressure in the main chamber urging the balls into sealing contact with the seals, here proper tolerance control of the ball valve features is required to ensure mechanical contact and sealing.
In particular, rotary disc valve assembly 400 includes a valve plate 402 having multiple gas flow ports 405 angularly aligned around rotational axis Q-Q as described below. Valve plate 402 rotates with knob 67 (not shown in this set of FIGS) due to valve plate 402 being keyed to fastener extension 410, such as by valve plate 402 having a hexagonal shaped cut-out (not shown) that interacts with a hexagonal shaped fastener extension 410. Light spring 415 biases valve plate 402 against seals 53. Therefore, when none of the gas flow ports 405 are aligned with flow ports 40, 45, there is no fluid communication between main chamber C and either of the auxiliary chambers A1, A2. However, during pressurization (as described above), the incoming pressurized gas flowing through pressurization channel 82 flows throughout the unsealed areas around valve plate 402 and into the various chambers C, A1, A2.
The operation of this exemplary embodiment is similar to operation of the previous embodiment shown in
Using the convention with respect to
1) in a first setting (
2) in a second setting (
3) in a third setting (
4) in a fourth setting (
Note that, with this alternate embodiment, somewhat closer manufacturing tolerances are required for this portion of the structure than for the embodiment of
While the invention has been described with respect to certain exemplary embodiments, it is understood that many variations are apparent to one of ordinary skill in the art from a reading of the above specification and such variations are within the spirit and scope of the instant invention as defined by the following appended claims.
10′
25′
67′
This application claims priority to and is a continuation of the co-pending patent application, U.S. patent application Ser. No. 14/621,905, filed on Feb. 13, 2015, entitled “GAS SPRING CURVE CONTROL IN AN ADJUSTABLE VOLUME GAS PRESSURIZED DEVICE”, by Robert C. Fox, and assigned to the assignee of the present invention, the disclosure of which is hereby incorporated herein by reference in its entirety. The U.S. patent application Ser. No. 14/621,905 is a continuation of and claims the benefit of U.S. patent application Ser. No. 13/100,129, filed on May 3, 2011, is now issued U.S. Pat. No. 9,796,447, entitled “GAS SPRING CURVE CONTROL IN AN ADJUSTABLE VOLUME GAS PRESSURIZED DEVICE” by Robert C. Fox, and assigned to the assignee of the present invention, the disclosure of which is hereby incorporated herein by reference in its entirety. The U.S. patent application Ser. No. 13/100,129 is a continuation of and claims the benefit of U.S. patent application Ser. No. 11/560,403, filed on Nov. 16, 2006, is now issued U.S. Pat. No. 8,464,850, entitled “GAS SPRING CURVE CONTROL IN AN ADJUSTABLE VOLUME GAS-PRESSURIZED DEVICE” by Robert C. Fox, and assigned to the assignee of the present invention, the disclosure of which is hereby incorporated herein by reference in its entirety. The U.S. patent application Ser. No. 13/100,129 is a continuation-in-part of and claims the benefit of U.S. patent application Ser. No. 12/768,523, filed on Apr. 27, 2010, is now issued U.S. Pat. No. 8,752,681, entitled “INTEGRATED AND SELF-CONTAINED SUSPENSION ASSEMBLY HAVING AN ON-THE-FLY ADJUSTABLE AIR SPRING” by Robert C. Fox, and assigned to the assignee of the present invention, the disclosure of which is hereby incorporated herein by reference in its entirety. The U.S. patent application Ser. No. 12/768,523 is a continuation of and claims the benefit of U.S. patent application Ser. No. 10/237,333, filed on Sep. 5, 2002, is now issued U.S. Pat. No. 7,703,585, entitled “INTEGRATED AND SELF-CONTAINED SUSPENSION ASSEMBLY HAVING AN ON-THE-FLY ADJUSTABLE AIR SPRING” by Robert C. Fox, and assigned to the assignee of the present invention, the disclosure of which is hereby incorporated herein by reference in its entirety. The U.S. patent application Ser. No. 10/237,333 claims priority to and benefit of U.S. Provisional Patent Application No. 60/392,802, filed on Jun. 28, 2002, entitled “ON-THE-FLY ADJUSTABLE AIR SPRING”, by Robert C. Fox, which is incorporated herein, in its entirety, by reference. The U.S. patent application Ser. No. 10/237,333 claims priority to and benefit of U.S. Provisional Patent Application No. 60/392,802, filed on Jun. 28, 2002, entitled “ON-THE-FLY ADJUSTABLE AIR SPRING”, by Robert C. Fox, which is incorporated herein, in its entirety, by reference. The U.S. patent application Ser. No. 10/237,333 claims priority to and benefit of U.S. Provisional Patent Application No. 60/391,991, filed on Jun. 25, 2002, entitled “ON-THE-FLY ADJUSTABLE AIR SPRING”, by Robert C. Fox, which is incorporated herein, in its entirety, by reference.
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Number | Date | Country | |
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20180057100 A1 | Mar 2018 | US |
Number | Date | Country | |
---|---|---|---|
60392802 | Jun 2002 | US | |
60391991 | Jun 2002 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 14621905 | Feb 2015 | US |
Child | 15796564 | US | |
Parent | 13100129 | May 2011 | US |
Child | 14621905 | US | |
Parent | 11560403 | Nov 2006 | US |
Child | 12768523 | US | |
Parent | 10237333 | Sep 2002 | US |
Child | 12768523 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 12768523 | Apr 2010 | US |
Child | 13100129 | US |