The present invention relates generally to bicycles, and more specifically to bicycle seats having an adjustable stiffness.
Bicycles commonly have a seat for supporting the rider. Bicycle seats can be made from a variety of materials, such as leather, plastic, and vinyl. In order to increase the comfort to the rider, bicycle seats are often designed to be resilient. For example, the seat can include foam to allow the seat to conform to the rider. In addition, the seat can be mounted on springs to facilitate absorption of shock loads imparted to the bicycle from the riding surface.
The present invention provides a bicycle seat including a mount adapted to be coupled to a bicycle frame, a shell supported by the mount, and a tensioned element (e.g., a flexible element, such as a cable) extending from a first anchor point to a second anchor point. The shell includes a flexible portion for supporting a rider, and the tensioned element includes a support portion providing support to the flexible portion between the first and second anchor points. The bicycle seat can be mounted on a bicycle frame.
In one embodiment, the mount comprises two rails, each rail having a front end secured to a front portion of the shell and a rear end secured to a rear portion of the shell. Preferably, the first anchor point is on the front portion of the shell and the second anchor point is on the rear portion of the shell. In this regard, the flexible portion can be positioned between the front portion and the rear portion.
Tension in the tensioned element is preferably adjustable to thereby adjust the support provided by the tensioned element to the flexible portion. For example, the tensioned element can be wrapped around an adjustment dial for adjusting a tension in the flexible element. A compression member (e.g., two compression members) can be positioned between the tensioned element and the flexible portion (e.g., integrally formed into the shell).
Other aspects of the invention will become apparent by consideration of the detailed description and accompanying drawings.
Before any embodiments of the invention are explained in detail, it is to be understood that the invention is not limited in its application to the details of construction and the arrangement of components set forth in the following description or illustrated in the following drawings. The invention is capable of other embodiments and of being practiced or of being carried out in various ways.
Referring to
The compression members 125 are disposed along and extend downward from the underside of the shell 85. The illustrated compression members 125 are integrally formed with the shell 85, although the compression members 125 can be provided on the seat 75 as separate elements that are attached to the shell 85. With reference to
As illustrated, each compression member 125 takes the form of a protruding tab that has a concavity or notch 135. In some cases, elongated ribs or bars (not shown) can be coupled between the two longitudinally-arranged compression members 125 so that the elongated ribs are positioned along the flexible portion 120. For example, the seat 75 can include laterally opposed elongated ribs that are integrally formed with and extend outward from the underside of the shell 85, or elongated ribs that are separately attached to the shell 85 via the compression members 125. Furthermore, the compression members 125 can take on other forms without deviating from the scope of the invention.
The seat 75 also has a front anchor point 145 located on the front portion 95 and a rear anchor point 150 located on the rear portion 100. In some constructions, one or both of the front anchor point 145 and the rear anchor point 150 can be supported by the rails 90. The front anchor point 145 is located generally rearward of the forwardly-located rail support 105, and is defined by a post 155 that extends outward from an underside of the shell 85. The post 155 can be fastened (bolted, riveted, etc.) to the shell 85, molded into or with the shell 85, or secured to the underside of the shell 85 in other ways. With reference to
With reference to
For example, the tensioned element 190 can be arranged along the underside of the shell 85 so that the tensioned element 190 makes more than two passes under the flexible portion 120. In these arrangements, the tensioned element can be supported by anchor points (e.g., anchor points 145, 150) on each end and can wrap around or otherwise engage structure on the shell 85 between the anchor points. Other arrangements of the tensioned element 190 along the underside of the shell 85 relative to the flexible portion 120 are also possible and considered herein.
The illustrated tensioned element 190 has opposed ends 210 that are coupled to the adjustment dial 195 and a looped support portion 215 that is located between the ends 210 and engaged with the compression members 125 to support the flexible portion 120 between the front anchor point 145 and the rear anchor point 150. The support portion 215 extends forward from the rear anchor point 150 through the passageways 180, and the compression members 125 are positioned between the support portion 215 and the flexible portion 120 to form a column or pillar that is acted upon by the tensioned element 190 to stiffen or relax the flexible portion 120 based on the tension applied to the tensioned element 190. In other arrangements, the tensioned element 190 can include the compression members 125, or the tensioned element can be engaged with the flexible portion 120 in other ways (e.g., without the compression members 125).
With reference to
One such tension apparatus 185 is described and illustrated in detail in U.S. Pat. No. 8,091,182, assigned to Boa Technology, Inc. with its principal place of business in Steamboat Springs, Colorado, and which is incorporated herein by reference. The illustrated adjustment dial 195 of the tension apparatus 185 rotates in one direction (e.g., clockwise) to apply tension the tensioned element 190, and rotates in another direction (e.g., counter-clockwise) to decrease tension on the tensioned element 190. In some constructions of the tension apparatus 185, the adjustment dial 195 can rotate (either clockwise or counter-clockwise) to apply or increase tension on the tensioned element 190, and can include a pushbutton (e.g., a momentary pushbutton or a maintained pushbutton) or another mechanism that is releasable (e.g., movable inward and outward or vertically relative to the base 220) to decrease or release tension on the tensioned element 190. Another adjustment mechanism can include devices that twist, turn, push, pull, ratchet, and/or screw, etc., to increase or decrease the tension on the tensioned element 190. Although only one construction of the tension apparatus 185 is illustrated and only a few examples of tension apparatus are described herein, it will be appreciated that there are several other tension apparatus that can be used to adjust tension on the tensioned element 190.
Moreover, other types of tension apparatus can be utilized to stiffen and relax the flexible portion 120 of the shell 85. One such tension apparatus can include a lever actuator with a lever that is movable in one direction to increase tension to the tensioned element 190, and that is movable in another direction to release tension on the tensioned element 190. Another tension apparatus can include a cam actuator that increase and decrease tension on the tensioned element 190. Yet another tension apparatus can include screw or fastener mechanisms that increase and decrease tension on the tensioned element 190. Still another tension apparatus can include a ratchet mechanism that increases and decrease tensions on the tensioned element 190. Also, certain features of the tension apparatus described herein can be combined to form still other types of tension apparatus (e.g., a lever-cam tension apparatus, a lever-ratchet apparatus, etc.). Other tension apparatus and/or adjustment mechanisms that stiffen and relax the flexible portion 120 are also possible and considered herein.
The illustrated adjustment dial 195 is located at the rear anchor point 150, although the adjustment dial 195 (or another adjustment mechanism) can be located anywhere along the underside of the shell 85 and in communication with the tensioned element 190 (e.g., at the front anchor point 145, between the front and rear anchor points 145, 150, along the side of the shell 85, etc.). With reference to
The illustrated tension apparatus 185 is assembled onto the seat 75 by orienting the looped tensioned element 190 relative to the rear anchor point 150 so that the support portion 215 extends through the passageways 180. The dial 195 is then placed in the cavity 170 so that the base 220 protrudes through the aperture 175. The support portion 215 is then engaged with the compression members and is routed around the post 155 within the channel 160. The fastener 200 and flange 205, when used, can be attached to the post 155 before or after the tensioned element 190 is wrapped around the post 155. Also, the cap 225 can be attached to the base 220 before or after the tensioned element is routed around the front anchor point.
When the adjustment dial 195 is rotated in the other direction (e.g., counter-clockwise as denoted by arrow 250 in
As described, the tension in the tensioned element 190 can be incrementally or continuously adjusted using the adjustment dial 195 to increase or decrease the firmness or stiffness (i.e., support) provided by the tensioned element 190 to the flexible portion 120 to provide a desired seat stiffness for the rider. The tensioned element 190 reinforces the flexible portion 120 based on the degree of tension applied to the tensioned element 190 so that the ride characteristics and feel of the seat 75 can be customized to suit different riders. More specifically, the flex of the flexible portion 120 can be tuned using the seat tension apparatus so that the seat 75 can have the same relative stiffness for riders of different weights.
Also, the tension apparatus 185 is arranged on the seat 75 so that a user can engage the cap 225 and adjust seat stiffness before or during a ride. While a rider may prefer a relatively stiff seat 75 for short rides and a relatively soft seat 75 for longer rides, the rider can adjust the stiffness of the seat 75 dynamically during a ride simply by rotating the cap 225 in the appropriate direction. Further, a rider can customize the seat stiffness using the seat tension apparatus 185 based on whether the rider is in an early training phase or late training phase.
Various features and advantages of the invention are set forth in the following claims.